PUSHING THE BOUNDARIES OF THE IMAGINABLE: …

22–26 JUNE 2015 DALLAS, TX

14-315

PUSHING THE BOUNDARIES OF THE IMAGINABLE: LEVERAGING THE AVIATION ECOSYSTEM

FINAL PROGRAM www.aiaa-aviation.org#aiaaAviation

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Welcome

Juan Alonso

Stanford University

Victoria Cox

Federal Aviation Administration (retired)

Thomas Edwards

NASA Ames Research Center

John O’Leary

Airbus Americas

Richard Wahls

NASA Langley Research Center

Todd Zarfos

Boeing Commercial Airplanes

Executive Steering Committee

AIAA AVIATION 2015

21st AIAA/CEAS Aeroacoustics Conference

31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference

33rd AIAA Applied Aerodynamics Conference

AIAA Atmospheric Flight Mechanics Conference

7th AIAA Atmospheric and Space Environments Conference

15th AIAA Aviation Technology, Integration, and Operations Conference

AIAA Balloon Systems Conference

AIAA Complex Aerospace Systems Exchange

22nd AIAA Computational Fluid Dynamics Conference

AIAA Flight Testing Conference

45th AIAA Fluid Dynamics Conference

22nd AIAA Lighter-Than-Air Systems Technology Conference

16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

AIAA Modeling and Simulation Technologies Conference

46th AIAA Plasmadynamics and Lasers Conference

45th AIAA Thermophysics Conference

AVIATION 2O15 is proud to feature the following conferences:

Welcome to Dallas and to AIAA AVIATION 2015! We are excited to share this week’s program with you as we explore recent progress and the most pressing issues facing aviation today. This year’s theme is “Pushing the Boundaries of the Imaginable: Leveraging the Aviation Ecosystem.” More than just a simple slogan, we think this theme provides a good overview of the various sessions planned for you this week.

Tom Enders will set the tone for us with his opening keynote addressing how the aviation industry can remain a dynamic player in pushing technology forward. Ed Bolton and Bill Ayer will discuss how NextGen will provide the foundation for advancing aviation in the future while engaging the myriad stakeholders that are a part of our ecosystem. Charlie Bolden will share the ways by which NASA historically has and will continue to push boundaries in aviation for the benefit of the entire community. Greg Touhill will discuss one of the more pressing issues of the day – cybersecurity and the importance of securing our ecosystem. Finally, Kurt Erbacher will look back at the design, development, and testing of the award-winning G650, one of the newest airplanes to hit the market while advancing the state of the art.

The Forum 360 sessions will provide several opportunities for our community to interact with customers, regulators, and technology leaders in focused, intimate conversations. Two sessions will allow leaders from airlines to discuss issues of importance to them with our design community. Unmanned systems continue to make headlines and we will discuss the challenges facing this sector internationally. Following Administrator Bolden’s discussion of NASA’s aeronautics strategy, we will hear from the center directors responsible for executing those plans. The challenges of widely deploying green aviation technologies to substantially reduce the environmental impact of aviation will be addressed by international experts. The future of supercomputing and particle image velocimetry will be discussed, with an emphasis on their role in advancing the future of aerospace technology. We will also have focused sessions on complex aerospace systems that will tackle the most important system development issues facing chief engineers, program managers, and systems engineers today.

As you would expect, with over 1,500 presentations, our technical program is second to none. The scope, breadth, and depth of the cutting-edge aviation and aerospace research being presented is material that you will be unable to find anywhere else. We thank the Forum Organizing and Technical Program Committees and the AIAA staff for their hard work to assemble this first-class program. We hope you will too.

AVIATION 2015 will energize, inspire, and sustain our community’s efforts to keep the aviation ecosystem on the glide path to advanced efficiency, safety, and security. We thank you for making the choice to be here with us this week, and we are confident you will find the experience to be a worthwhile one.


IntroOrganizing CommitteeGeneral ChairRichard Wahls, NASA Langley Research Center

Forum 360 ChairRobert Gregg, III, The Boeing Company

Technical Co-ChairVincent Schultz, NASA Langley Research Center

Technical Co-ChairGreg Naterer, Memorial University

InternationalKonstantinos “Kostas” Kontis, University of Glasgow

Member ServicesSarah Shull, NASA Johnson Space Center

Local RepTerry Burress, Lockheed Martin Information Systems & Global Solutions

Young ProfessionalGreg Johnson, Aerojet Rocketdyne

RecognitionDimitri Mavris, Georgia Institute of Technology

Public PolicyBob Stuever, Beechcraft Defense Company, LLC

Complex Aerospace Systems Exchange (CASE) ChairSophia Bright, The Boeing Company

Technical Program Committee

Forum Technical Co-ChairsGreg Naterer (Aerospace Sciences Group), Memorial University

Vincent Schultz (Aircraft and Atmospheric Systems Group), NASA Langley Research Center

Forum Deputy Technical Co-ChairsLaTunia Melton (Aerospace Sciences Group), NASA Langley Research Center

Cees Bil (Aircraft and Atmospheric Systems Group), RMIT University

ITAR ChairKatya M. Casper, Sandia National Laboratories

Technical Discipline Chairs

Aeroacoustics Naval Agarwal, The Boeing Company

Aerodynamic Measurement TechnologyAndrew Cutler, The George Washington University

Todd Lowe, Virginia Polytechnic Institute and State University

Air Transportation Integration & OperationsCees Bil, RMIT University

Kapil Sheth, NASA Ames Research Center

Karen Marais, Purdue University

Scot Campbell, Massachusetts Institute of Technology

Aircraft DesignHernando Jimenez, Georgia Institute of Technology

Danielle (Dani) Soban, Queen’s University Belfast

Applied AerodynamicsBrian McGrath, The Johns Hopkins University Applied Physics Laboratory

Khaled Abdol-Hamid, NASA Langley Research Center

Zifeng Yang, Wright State University

Atmospheric and Space EnvironmentsNashat Ahmad, NASA Langley Research Center

Matthew Pruis, Northwest Research Associates Inc.

Atmospheric Flight Mechanics Soumyo (Som) Dutta, NASA Langley Research Center

Kevin Cunningham, NASA Langley Research Center

Balloon SystemsDebora Fairbrother, NASA

Complex Aerospace Systems Exchange (CASE) Sophia Bright, The Boeing Company

Computational Fluid DynamicsKrzysztof (Chris) Fidkowski, University of Michigan

Flight TestingKarl Garman, Federal Aviation Administration

Fluid DynamicsJill Klentzman, Baylor University

Green EngineeringAndrew Gibson, Empirical Systems Aerospace

Ground TestingBenjamin Mills, Aerospace Testing Alliance

Lighter than Air SystemsRajkumar S. Pant, Indian Institute of Technology Bombay

Modeling and Simulation TechnologiesGano Broto Chatterji, NASA Ames Research Center

Multidisciplinary Analysis and OptimizationEliot Winer, Iowa State University

Vijay Kalivarapu, Iowa State University

Plasmadynamics and LasersAzer Yalin, Colorado State University

ThermophysicsChad Boyack, Raytheon Missile Systems

Elliott Short, Raytheon Missile Systems

Technical Discipline Group Representatives

TAC Information Systems GroupSam Adhikari, Sysoft Corporation


IntroContents

Welcome 3

Organizing Committee 4

Contents 5

Forum Overview 8

Sponsors 10

Keynote Speakers and Plenary Sessions 11

Forum 360 12

Special Sessions and Events 17

Networking Events 18

Recognition Events 19

ITAR Information 21

Exposition Hall 22

Exhibitors 24

General Information 27

Author and Session Chair Information 29

Committee Meetings 30

Sessions at a Glance 33

Session Detail Matrix 41

Author and Session Chair Index 121

Technical Zones 134

Venue Map 135

AIAA is the world’s largest aerospace professional society, serving a diverse range of more than 30,000 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA.

Join the conversation!#aiaaAviation

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IntroForum Overview

MONDAY 22 June

TUESDAY 23 June

0730 hrs Speakers’ Briefing Speakers’ Briefing

0800 hrsPlenary Keynote Plenary Panel

0830 hrs

0900 hrs Networking Break

Technical Sessions

Networking Break in Exposition Hall

Technical Sessions

Exposition Hall Open

0930 hrs

Forum 360 Forum 360

1000 hrs

1030 hrs

1100 hrs

1130 hrs

1200 hrs

1230 hrs

Networking Lunch on OwnAwards Luncheon:

Celebrating Achievements in Aerospace Sciences

Networking Lunch on Own1300 hrs

1330 hrs

1400 hrs

Technical Sessions

Forum 360 Technical Sessions

Forum 360

CFD Flow Visualization Showcase


1430 hrs

1500 hrs

1530 hrs Networking Break Networking Break in Exposition Hall

1600 hrs

1630 hrs Plasmadynamics and Lasers Award Lecture1700 hrs

1730 hrs Fluid Dynamics Award Lecture Speed Geek

Networking Event and Reception

Reception in Exposition Hall1800 hrs

1830 hrs Rising Leaders in Aerospace Reception1900 hrs

1930 hrs

2000 hrs

2030 hrs

2100 hrs

2130 hrs

2200 hrs


IntroForum Overview

WEDNESDAY 24 June

THURSDAY 25 June

FRIDAY 26 June

0730 hrs Speakers’ Briefing Speakers’ Briefing Speakers’ Briefing

0800 hrsPlenary Keynote Plenary Keynote Plenary Keynote

0830 hrs

0900 hrs Networking Break in Exposition Hall

Technical Sessions


Networking Break in Exposition Hall

Technical Sessions


Networking Break

Technical Sessions

0930 hrs

Forum 360 Forum 360

1000 hrs

1030 hrs

1100 hrs

1130 hrs

1200 hrs

1230 hrs

Luncheon in Exposition HallAwards Luncheon:

Celebrating Achievements in Aircraft and Atmospheric Systems

Networking Lunch on Own1300 hrs

1330 hrs

1400 hrs

Technical Sessions

Forum 360


Technical Sessions

Forum 360

Rising Leaders in Aerospace

Panel1430 hrs

1500 hrs

1530 hrs Networking Break in Exposition Hall Rising Leaders

in Aerospace Leadership

Exchange/Speed Networking

Networking Break

1600 hrs

1630 hrs Aerodynamics Award Lecture1700 hrs

1730 hrsAeroacoustics

LectureThermophysics Award Lecture Wright Brothers Lectureship in Aeronautics

1800 hrs

1830 hrs

1900 hrs

Aeroacoustics Awards Banquet1930 hrs

2000 hrs

2030 hrs

2100 hrs

2130 hrs

2200 hrs


IntroSponsors Premier Sponsor

Speed Geek Networking Event Sponsor

Supporting Sponsors

Media Sponsor

R

Crean & AssociatesAerospace Consultants

Rising Leaders Program SponsorSponsor


IntroKeynote Speakers and Plenary SessionsGet the big picture on aviation from the thought leaders in the field during these high-level discussions and presentations.

Monday, 22 June 0800–0900 hrs Chantilly Ballroom West

Opening Keynote: Are We Moving Fast Enough? Tom Enders, Chief Executive Officer, Airbus Group

Tuesday, 23 June0800–0900 hrs Chantilly Ballroom West

NextGen: A Model of Stakeholder Engagement Bill Ayer, Retired Chairman and CEO, Alaska Air GroupEdward L. Bolton Jr., Assistant Administrator for NextGen, Federal Aviation Administration

Wednesday, 24 June0800–0900 hrs Chantilly Ballroom West

NASA and the Future of AerospaceCharles F. Bolden Jr., Administrator, National Aeronautics and Space Administration

Thursday, 25 June0800–0900 hrs Chantilly Ballroom West

DHS’s Perspectives on Cybersecurity in Aviation Gregory J. Touhill, Deputy Assistant Secretary for Cybersecurity and Communications, Department of Homeland Security

Friday, 26 June0800–0900 hrs Chantilly Ballroom West

The G650 Design, Development, and Test Kurt Erbacher, Vice President, G650 Aircraft Program, Gulfstream Aerospace Corporation


Forum 360

Monday, 22 June0930–1200 hrs Grand Ballroom E

The Voice of the Customer — Designing the Right Aircraft Moderator: Christopher Stonehouse, Senior Vice President, Customer Services, Airbus Americas, Inc.Panelists:Jack Arehart, President of MRO Services, Delta TechOpsWilliam “Bill” Meehan, Chief Operating Officer, Frontier

Airlines, Inc.Bart Roberts, Vice President, Flight Operations, JetBlue AirwaysDavid Seymour, Senior Vice President, Technical Operations,

American Airlines

1400–1700 hrs Grand Ballroom E

Whatever Happened to the Four-Year Airplane?Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace CorporationPanelists:Catherine Ferrie Kilmain, Executive Vice President of

Engineering, Bell HelicopterEric Schrock, Deputy Director, Technology Development and

Product Integration, Lockheed Martin Corporation

Tuesday, 23 June0930–1200 hrs Grand Ballroom E

Day in the Life of Operations – Effectively Managing DisruptionModerator: Neil Planzer, Vice President, Air Traffic Management, Boeing Commercial AirplanesPanelists:Tim Campbell, Senior Vice President, Air Operations, American

AirlinesJim Crites, Executive Vice President of Operations, DFW

International AirportBrian Quigley, Managing Director Flight Operations, United

AirlinesDan Smiley, Vice President for System Operations, Federal

Aviation Administration Air Traffic Office


International UAS Integration ForumModerator: Rob Hughes, Northrop Grumman, IncPanelists:Cees Bil, Associate Professor, School of Aerospace, Mechanical

and Manufacturing Engineering, RMIT UniversityChuck Johnson, Vice President of Operations, The Padina

GroupMarty Rogers, University of Alaska-FairbanksMarshall Jackson, Project Manager – Aviation Safety

Audits, Office of Inspector General, U.S. Department of Transportation

Randy Willis, FAA, Co-Chair of ICAO RPAS (Remotely Piloted Aircraft Systems)

Dale Richards, Senior Research Fellow, Human Factors, Faculty of Engineering & Computing, Coventry University

These conversations will cover a spectrum of timely topics including programs, systems, policy, operations, applications, platforms and more!


IntroWednesday, 24 June0930–1200 hrs Grand Ballroom E

NACA to NASA: Embarking on the Next 100 Years of Excellence and Innovation in Aeronautics and BeyondModerator: Robert Pearce, Director, Strategy, Architecture & Analysis, Aeronautics Research Mission Directorate, NASA HeadquartersPanelists:David Bowles, Center Director (Acting), NASA Langley

Research CenterThomas Edwards, Deputy Center Director, NASA Ames

Research CenterJanet Kavandi, Deputy Director, NASA Glenn Research CenterDavid McBride, Center Director, NASA Armstrong Flight

Research CenterJaiwon Shin, Associate Administrator, Aeronautics Research

Mission Directorate, NASA Headquarters


Energy/Environment Panel — The Challenges of Green AviationModerator: Marty Bradley, Technical Fellow, Boeing Commercial AirplanesPanelists:Ricky Curran, Faculty of Aerospace Engineering, Delft

University of TechnologyJay E. Dryer, Director, Advanced Air Vehicles Program Office

(Acting), Aeronautics Research Mission Directorate, NASA Headquarters

Askin Isikveren, Head of Visionary Aircraft Concepts, Bauhaus Luftfahrt

Leslie Perkins, Director, Energy Office, Air Force Research Laboratory

Jeanne Yu, Environmental Director, Boeing Commercial Airplanes

1400–1730 hrs Grand Ballroom D

System Complexity: Government Needs and Practical Research Results Keynote Speaker: Kristen Baldwin, Principal Deputy DASD (SE), Department of DefenseModerators:Frank Serna, Principal Director, Strategic Imperatives, Draper

LaboratoryAnna-Marie McGowan, Aeronautics Research Directorate,

NASA Langley Research CenterPanelists:Jeffrey P. Holland, Director of Research and Development and

Chief Scientist, U.S. Army Corps of EngineersDavid Neyland, Consultant

Thursday, 25 June0930–1200 hrs Grand Ballroom E

The Impact of Particle Image Velocimetry on Aerospace TechnologyModerator: Steven Beresh, Distinguished Member of the Technical Staff, Sandia National Laboratories Panelists:Ronald J. Adrian, Regent’s Professor and Ira A. Fulton Professor

of Mechanical and Aerospace Engineering, Arizona State University

Susan Gorton, Project Manager, Revolutionary Vertical Lift Technology Project, NASA Langley Research Center

Fulvio Scarano, Full Professor and Chair of Aerodynamics, Delft University of Technology

Miguel Visbal, Principal Research Aerospace Engineer and Team Leader of Multidisciplinary Computational Aerodynamics, Aerospace Systems Directorate, Air Force Research Laboratory


Supercomputing: Roadmap and Its Future Role in Aerospace EngineeringModerator: Doug Cline, Technical Lead, High Performance Computing, Lockheed Martin AeronauticsPanelists:Jef Dawson, Applications Manager, Cray, Inc.William Gropp, Thomas M. Siebel Chair, Department of

Computer Science and Director, Parallel Computing Institute, University of Illinois at Urbana-Champaign

Brian Mitchell, Senior Principal Engineer, GE Global ResearchMark Seager, Intel Fellow, CTO, High Performance Computing

Ecosystem, Intel Corporation

Forum 360


Intro

Monday, 22 June0900–1200 hrs Batik A-B

Academic RoundtableExpanding on the theme from Sunday, this session is the second day activity of the 2015 CASE Academic Workshop. It will offer rapid-fire discussions of current research efforts in systems knowledge and competency.Facilitators:Franz-Josef Kahlen, Ph.D., Associate Professor, Department

of Mechanical Engineering, University of Cape Town, Cape Town, South Africa

Shannon Flumerfelt, Ph.D., Associate Professor, Educational Leadership, Director of Lean Thinking for Schools, Pawley Learning Institute, Oakland University, Michigan

Anabela Alves, Ph.D., Assistant Professor, Departamento de Produção e Sistemas Escola de Engenharia da Universidade do Minho, Centro Interdisciplinar de Tecnologias, da Produção e da Energia (CITPE), Campus de Azurém, Portugal


Whatever Happened to the Four-Year Airplane?This panel will explore the challenges facing aerospace professionals who are directly engaged in leading, developing, producing, and supporting the industry’s most advanced vehicles and systems in the context of a “four-year aircraft” theme. We continue to push the limits of technology to deliver greater performance in all segments of aerospace, in an environment that is increasingly risk averse. These challenges have pushed us to longer development cycles and exponential growth in budgets. In addition, new technical disciplines (e.g., cyber) are being integrated into legacy and emerging systems, while subsystems are gaining in both complexity and interdependency. In the context of this environment, our panel will address how the aerospace industry should position itself to meet the challenges of reducing the cost and schedule and approach a “four-year aircraft” cycle in our increasingly complex world.Moderator: Craig Willis, Group Head for Systems Verification, Gulfstream G500/G600 Program, Gulfstream Aerospace CorporationPanelists:Catherine Ferrie Kilmain, Executive Vice President of

Engineering, Bell HelicopterEric Schrock, Deputy Director, Technology Development and

Product Integration, Lockheed Martin Corporation

1730–1900 hrs Morocco

CASE Networking SocialSponsored by Boeing Commercial Airplanes

Tuesday, 23 June0930–1200 hrs Grand Ballroom D

Applied Complexity WorkshopParticipants can learn how to embrace and thrive within technically, socially, and organizationally complex environments. Participants will be immersed in a three-pronged approach to learning, with industry examples, applied theory, and interactive practice. Please join us for this engagement, and bring your own experiences to share and a desire to strengthen your complex systems engineering thinking. Panelists:Paul C. Lambertson, Systems Engineering & Integration Team

777X, Boeing Commercial AirplanesSteve Holt, Engineering Integrated Strategy, Airplane Level

Engineering Integration, The Boeing CompanyJim Blohowiak, 777X Airplane Level Integration Team, The

Boeing CompanyAlison Lauderbach, 777X Airplane Level Integration Team, The

Boeing Company

1400–1530 hrs Steuben

Concept Development of Complex SystemsThis panel addresses the phase of development that includes activities from the beginning of decision activities for building new systems to the transition to the product design at milestone “B” (DoD) or the end of Phase B for NASA. Session Chairs:Steven D’Urso, Program Coordinator and Lecturer, Aerospace

Systems Engineering, University of Illinois at Urbana-Champaign

Mat French, Electrical Systems Engineer, Rolls-Royce Corporation

Panelists:Rick Mange, F-35 PNR Program Manager, Lockheed Martin

AeronauticsRobert (Rob) Simons, Technical Fellow, The Boeing CompanyJason Merret, Technical Specialist, Gulfstream Aerospace

Performance Engineering, Gulfstream Aerospace Corporation

Forum 360 As the name implies, CASE is an exchange of ideas among professionals on some of the most pertinent issues of the day facing the aerospace industry and the field of systems engineering.


IntroForum 360 1545–1730 hrs Steuben

Product Design for Complex Systems Across the Supply ChainThis session will focus on the challenges and enabling technologies for product design across a supply chain. In particular, the session will address the layered chain consisting of OEM/airframer, Tier 1, Tier 2, and the approaches for designing complex systems that handle the integration aspects. Methods and model-based tool approaches will be discussed in terms of existing capabilities, gaps, and future trends.Session Chairs:Eelco Scholte, Manager, Advanced Methods – Electric Systems,

UTC Aerospace Systems Carmen Schooley, Manager, Systems Engineering and

Integration, Gulfstream Aerospace CorporationPanelists:Fernando Dones, Technical Fellow, The Boeing CompanyBernard Dion, CTO, ANSYSBrenda Nuhfer, Program Manager, UTC/Pratt & Whitney

Wednesday, 24 June0900–1045 hrs Grand Ballroom D

Integration and TestThis panel focuses on the Integration & Test phase of development. Planning for integration activities of complex systems is inherently different from traditional systems engineering integration planning activities. Decisions about the systems under development have to consider not only the technical and programmatic viewpoints but also the political, societal, operational, and economic viewpoints. Definition of performance measures, found intrinsic in the plan, with trans-disciplinary implications will be discussed. A scenario for integration of UAS in the NAS will be used as a benchmark for current views and life-cycle challenges.Session Chairs:Mat French, Electrical Systems Engineer, Rolls-Royce

CorporationHernando Jiminez, Research Engineer II at Aerospace Systems

Design Laboratory, Georgia Institute of TechnologyDavid Loda, Executive Director, NCPS Research, LLCPanelists:Jim Murphy, Project Engineer for Integrated Test and Evaluation

for the Unmanned Aircraft System Integration, NASA Ames Research Center

David Maroney, Principal Systems Engineer, The Mitre Corporation


Entry into Service/End of LifeThis panel focuses on the complexities that arise once a system enters service throughout the life of the system. If these complexities are considered and incorporated into the system development phase, more robust products can be developed and higher customer satisfaction can be achieved. Session Chair: Jeff Jepson, Senior Systems Engineer GNC / Guidance Design & Performance, Raytheon Missile SystemsPanelists:Tim Adama, Chief Engineer of Factories, Raytheon Missile

SystemsEd Dolanski, President and CEO, AviallJim Gallagher, EIS Program Manager, Gulfstream Aerospace

Corporation


System Complexity: Government Needs and Practical Research ResultsThis panel is arranged around two application domains – defense systems and unmanned air systems in the national airspace – and two engineering practice needs – rapid system development and new theory complex systems engineering. The expectation is that the audience will take away both a cogent statement of needs and challenges along with a concise description of new techniques that show promise to meet the stated needs and challenges.Keynote Speaker: Kristen Baldwin, Principal Deputy DASD (SE), Department of DefenseModerators: Frank Serna, Principal Director, Strategic Initiatives, Draper

LaboratoryAnna-Maria McGowan, Aeronautics Research Directorate,

NASA Langley Research CenterPanelists:Jeffrey P. Holland, Director of Research and Development and

Chief Scientist, U.S. Army Corps of EngineersDavid Neyland, Consultant


IntroForum 360

Program Agenda

Networking ReceptionMonday, 22 June Emerald1830–1930 hrsThe reception will kick off the Rising Leaders in Aerospace events and is a perfect opportunity for young leaders to mingle with others who will be participating in AIAA AVIATION 2015 as attendee, presenter, or veteran professional. Come meet other participants in a casual environment. You’re bound to see them again.

Leadership Exchange/Speed NetworkingWednesday, 24 June Metropolitan Ballroom1530–1700 hrsGet your questions answered! Senior Mentors will include:Russ Althof, Chief Engineer, Raytheon Missile SystemsCees Bil, Professor , Royal Melbourne Institute of TechnologyDave Bowles, Center Director (Acting), NASA Langley Research CenterEd Feltrop, Engineer Specialist , Cessna Aircraft CompanySusan Gorton, Rotary Wing Project, NASA Langley Research CenterPeter Hartwich, Engineering Manager, Boeing Defense, Space and SecurityJanice Kavandi, Deputy Director, NASA Glenn Research CenterJeff Jepson, Senior Multi-Disciplined Engineer I, Raytheon Missile SystemsSamantha A. Magill, Academic Affairs and Inclusion & Diversity, Honda Aircraft CompanySandy Magnus, Executive Director, AIAADavid McBride, Center Director, NASA Armstrong Flight Research CenterCharles Smith, Center Director (Acting), NASA Ames Research Center John Valasek, Professor/Director, Vehicle Systems & Control Laboratory, Texas A&M University

Panel Discussion: Transitioning to Leadership Thursday, 25 June Emerald1400–1530 hrsAs engineers and aerospace professionals gain experience, there is often the opportunity to do more with the company. Promotions are often a result, but so are management opportunities. As you transition from an engineer on a project to an engineer leading a project, what changes? How about when you are made manager of a department or a division, are there skill sets that you need to hone? What if you are looking to eventually become a chief officer, how can you plan for and make those transitions? This panel will address the changes that accompany moving into a management role, the different skill sets that will need to be acquired, and the changes you can expect in your daily work routine.If you have management or leadership aspirations, come and listen to advice from esteemed panelists.Moderator: Ben Marchionna, Systems Engineer, Lockheed Martin Skunk WorksPanelists:Russ Althof, Chief Engineer, Raytheon Missile SystemsDouglas Stanley, President and Executive Director, National Institute of AerospaceFrederick Wieland, Director, Air Traffic Management, Intelligent Automation Systems, Inc.

RISINGLEADERSAEROSPACEin

Sponsored by:

The multidimensional program features a leadership exchange/speed mentoring, panel session, Q&A with top industry leaders, and multiple opportunities for networking. These exciting and energetic activities will provide access to top aerospace leaders and their perspectives with subject matter relevant to your career.


IntroSpecial Sessions and EventsSpeed Geek Networking Event and ReceptionMonday, 22 June Chantilly Ballroom Foyer1730–1830 hrs, reception to follow 1830–1900 hrsThis casual, high-energy session will give you the opportunity to engage one-on-one with speakers and get a glimpse of things to come in the week ahead at AIAA AVIATION 2015. You’ll travel from speaker to speaker in small groups, listen to a 5-minute overview of their topic, and then have five minutes to have your questions answered.Open to all conference attendees, but space is limited to the first 500 participants.Sponsored by:

CFD Flow Visualization ShowcaseTuesday, 23 June Chantilly Ballroom Foyer1400–1600 hrsThe CFD Flow Visualization Showcase will be held in the foyer area outside the Exposition Hall. Authors of papers containing CFD visualizations will describe their work and the significance of their animation as it plays on a large- screen monitor. Multiple visualizations will be shown during each of the four 30-minute time slots during the event. At the conclusion of the event, awards will be presented for Most Artistic Flow Visualization Animation, Most Quantitatively Descriptive Flow Visualization Animation, and Most Comprehensive Flow Visualization Animation. The visualizations of the three winners will be displayed on a monitor in the Exposition Hall during the remainder of the exposition.

Aeroacoustics Awards Reception and BanquetWednesday, 24 June Imperial Ballroom1900 hrsThe Aeroacoustics Awards Reception and Banquet will begin with a cash bar social period at 1900 hrs, followed by the awards ceremony and banquet where the AIAA and CEAS Aeroacoustics Awards will be presented. The winner of the Aeroacoustics Student Paper Competition also will be recognized. Please join us and celebrate the achievements of your peers. Tickets will be available on site, as space is available.

See it in Dallas at the Perot Museum of Nature and Science

www.airplanesmovie.com

A MILE OF RUNWAY CAN TAKE YOU ANYWHERE.

NARRATED BY

HARRISON FORD


IntroUnderstanding the importance of networking with colleagues new and old, a series of activities have been planned that will help you connect with current colleagues and new acquaintances.

Student Welcome ReceptionSunday, 21 June Emerald1800–1930 hrs Mingle with your peers and hear from AIAA Executive Director Sandy Magnus. This reception provides you with the opportunity to meet your fellow students and learn more about the opportunities available to you as an AIAA student member.

Networking Coffee BreaksNetworking coffee breaks allow even more time for making new contacts, continuing discussions from sessions, visiting the Exposition Hall, or checking emails and voicemails to keep in touch with the office while you are at the forum. Networking coffee breaks will be held at the following locations and times:

Monday, 22 June 0900–0930 hrs and 1530–1600 hrs; Meeting Room Foyers

Tuesday, 23 June 0900–0930 hrs and 1530–1600 hrs; Exposition Hall

Wednesday, 24 June 0900–0930 hrs and 1530–1600 hrs; Exposition Hall

Thursday, 25 June 0900–0930 hrs (Exposition Hall) and 1530–1600 hrs (Meeting Room Foyers)

Friday, 26 June 0900–0930 hrs Meeting Room Foyers

Reception in the Exposition HallTuesday, 23 June Chantilly Ballroom East 1730–1900 hrsTake this opportunity to engage new contacts and refresh old ones. A ticket for the reception is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available.

Luncheon in the Exposition HallWednesday, 24 June Chantilly Ballroom East1230–1400 hrsA ticket is required and included in the registration fee where indicated.

Networking Events


Recognition EventsAIAA celebrates our industry’s discoveries and achievements from the small but brilliantly simple innovations that affect everyday life to the major discoveries and missions that fuel our collective human drive to explore and accomplish amazing things.

Monday, 22 June1730–1830 hrs Grand Ballroom D

Fluid Dynamics Award LectureSearching for Truthiness in Computational Fluid DynamicsPhilip Roe, Professor, Department of Aerospace Engineering, University of Michigan

Tuesday, 23 June1230–1400 hrs Chantilly Ballroom West

Awards Luncheon: Celebrating Achievements in Aerospace Sciences A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available. The following awards will be presented:

Aeroacoustics AwardNigel PeakeProfessor, Applied Mathematics University of Cambridge “For significant contributions to the understanding and prediction of turbomachinery noise generation and scattering.”

Aerodynamics AwardRussell M. CummingsProfessor of Aeronautics U.S. Air Force Academy “For a career devoted to predicting and understanding the vortical flowfields about aircraft at high angles of attack and during maneuvers.”

Fluid Dynamics AwardPhilip RoeProfessor, Department of Aerospace Engineering University of Michigan “For seminal contributions to the design of numerical algorithms for simulations of compressible flows.”

Plasmadynamics and Lasers AwardPhilip E. CassadySenior Technical Fellow (retired) The Boeing Company “For distinguished contributions to the development of aero-optics and high power laser fluid dynamics.”

Thermophysics AwardSumanta AcharyaRing Chair & Professor, Mechanical Engineering Department University of Memphis “For significant contributions to gas turbine heat transfer and aerodynamics, investigation of novel cooling schemes and application of emerging computational methodologies for gas turbine cooling.”

Certificates of Merit:Aerodynamic Measurement Technology Best PaperAIAA 2015-1696, “Pressure Monitoring using Hybrid fs/ps Rotational CARS,” Sean Kearney, Sandia National Laboratories, and Paul Danehy, NASA Langley Research Center.

Applied Aerodynamics Best PaperAIAA 2014-2139, “Uncertainty Quantification and Certification Prediction of Low-Boom Supersonic Aircraft Configurations,” Thomas K. West, Missouri University of Science and Technology; Bryan W. Reuter, University of Texas at Austin; Eric L. Walker, Bill Kleb, and Michael A. Park, NASA Langley Research Center.

David Weaver Best Student PaperAIAA 2014-2247, “Microscale Simulations of Porous TPS Materials: Application to Permeability,” Eric C. Stern, Ioannis Nompeli, Thomas Schwartzentruber and Graham Candler, University of Minnesota.

Fluid Dynamics Best PaperAIAA Paper 2015-1518, “Large Eddy Simulation of a Three-Dimensional Compression Ramp Shock-Turbulent Boundary Layer Interaction,” David Dawson and Sanjiva Lele, Stanford University.

Ground Testing Best PaperAIAA 2014-2800, “Skin Friction Sensor Validation for High-Speed, High-Enthalpy Flow Applications,” Ryan Meritt and Joseph Schetz, Virginia Polytechnic Institute and State University.

Modeling and Simulation Best PaperAIAA 2014-2206, “Transfer of Training on the Vertical Motion Simulator,” Peter Zaal, NASA Ames Research Center; Jeffrey Schroeder, Federal Aviation Administration; and William Chung, SAIC.

(continued)


Recognition EventsCertificates of Merit (continued)Plasmadynamics and Lasers Best PaperAIAA 2015-0935, “Electric Field Measurements in a Dielectric Barrier Nanosecond Pulse Discharge with Sub-nanosecond Time Resolution,” Benjamin Goldberg and Walter Lempert, Ohio State University; and Sean O’Byrne, University of New South Wales at the Australian Defence Force Academy.Plasmadynamics and Lasers Best Student PaperAIAA 2015-0679, “A Latency-Tolerant Architecture for Airborne Adaptive Optic Systems,” William R. Burns, Eric J. Jumper and Stanislav Gordeyev, University of Notre Dame.Thermophysics Best PaperAIAA 2015-0213, “NASA Langley Experimental Aerothermodynamic Contributions to Slender and Winged Hypersonic Vehicles,” Scott Berry and Karen Berger, NASA Langley Research Center.


Plasmadynamics and Lasers Award LectureFrom Plasmadynamics and Shock Tubes to Aero-Optics and Laser Radar: An Aerospace CareerPhilip E. Cassady, Senior Technical Fellow (retired), The Boeing Company

Wednesday, 24 June1630–1730 hrs Chantilly Ballroom West

Aerodynamics Award LectureStill Trying to Understand Aircraft VorticesRussell M. Cummings, Professor of Aeronautics, U.S. Air Force Academy


Thermophysics Award LectureAerodynamics and Heat Transfer in Gas Turbine Cooling-Recent AdvancesSumanta Acharya, Ring Chair & Professor, Mechanical Engineering Department, University of Memphis

1730–1830 hrs Chantilly Ballroom West

Aeroacoustics LectureFan Broadband Noise Generation and SuppressionEdmane Envia, Acoustics Branch, NASA Glenn Research Center

Thursday, 25 June1230–1400 hrs Chantilly Ballroom West

Awards Luncheon: Celebrating Achievements in Aircraft and Atmospheric Systems A ticket for the luncheon is required and included in the registration fee where indicated. Additional tickets for guests may be purchased on site, as space is available. The following awards will be presented:

Aircraft Design AwardDarold B. CummingsAerospace Consultant Boeing Technical Fellow (retired)“For a career demonstrating exceptional skill and creativity in the configuration and design of aircraft, and inspiring future generations of aircraft designers.”

Elmer A. Sperry AwardMichael Sinnett, Vice President, Product Development, and the Boeing 787-8 Development Team, Seattle, Washington“For pioneering engineering advances including lightweight composite wing and monolithic composite fuselage construction and advanced systems that have led to significant improvements in fuel efficiency, reduced carbon emission, reduced maintenance costs and increased passenger comfort.”

Certificates of Merit:Aircraft Design Best PaperAIAA 2014-3012, “A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase,” Imon Chakraborty, David Trawick, and Dimitri Mavris, Georgia Institute of Technology; Mathias Emeneth, PACE Americas Inc.; and Alexander Schneegans, PACE GmbH.

Multidisciplinary Design Optimization Best PaperAIAA-2014-3274, “Aerostructural Optimization of the Common Research Model Configuration,” Gaetan Kenway and Joaquim Martins, University of Michigan; and Graeme Kennedy, Georgia Institute of Technology.

1730–1830 hrs Chantilly Ballroom West

Wright Brothers Lectureship in Aeronautics Development and Testing of the X-47BPablo Gonzalez II, UCAS-D Program Manager, Northrop Grumman Aerospace Systems


IntroITAR-Restricted SessionsOn Tuesday, a limited number of oral presentations and papers will be presented in “U.S. Only” technical sessions. In addition to your forum registration, a separate registration process is required to attend these restricted sessions. Please see the detailed information on the ITAR Registration Grid below to determine your individual requirements.

Access to ITAR Sessions: Presenting a Paper, Chairing a Session, or Attending an ITAR-Restricted PresentationAdmittance to the restricted technical program is controlled by the U.S. International Traffic in Arms Regulations (ITAR). All attendees, presenters, and session chairs will need to register for the conference, and then visit the ITAR registration desk to complete the additional processes. Anyone wishing to enter the restricted session room MUST abide by the procedures and submission of verified documents mandated by the DoD. No Exceptions!

Availability of Manuscripts from ITAR-Restricted SessionsFor those who are registered to attend the sessions, a DVD containing the papers from the ITAR sessions will be available for purchase on site at the forum for $25. Those purchasing the DVD must be available to pick it up on Wednesday, 24 June 2015. All DVDs must be picked up in person. There will be no sale or distribution of these papers after the event.

ITAR Electronics PolicyNo phones, computers (other than the presenter), iPads, cameras, or other electronic devices with cameras or recording capabilities will be permitted into the ITAR session room. There will be a check-in desk in front of the room where you can check these devices.

ITAR Information

10/19/2012

Important session information for all attendees wishing to present or attend ITAR papers

AIAA Restricted Papers – ITAR Regulations Session Admittance Policy (Revised 10/19/2012)

Several papers scheduled to be presented at this conference will be restricted papers governed by ITAR (U.S. International Traffic in Arms Regulations). If you plan to attend any presentations restricted by ITAR, you must bring proof of citizenship PLUS the other verification documents as shown below. Please note that only U.S. Citizens and U.S. Resident Aliens can be considered for attendance at these restricted presentations. Admittance to restricted sessions and access to restricted technical papers is implemented and controlled by ITAR . All restricted session attendees (including speakers and session chairs for these sessions) MUST abide by the procedures and submittal of verification documents as noted below – NO EXCEPTIONS: ATTENDEE CLASSIFICATION IDENTIFICATION & PROOF OF EMPLOYMENT REQUIREMENTS U.S. Government Employees 1. Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND

2. Personal photographic identification: U.S. Government/Military Photo ID badge, such as CAC card U.S. Citizens 1. Proof of U.S. Citizenship (for example, passport, birth certificate, voters registration card, naturalization papers), AND

2. Personal photographic identification (passport, driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details)

Resident Aliens (U.S.) 1. Resident Alien Card, AND 2. Personal photographic identification (passport, driver’s license, etc.), AND 3. Certification credentials based on DD Form 2345 (see below for details)

DD Form 2345 individual certification credentials (required for U.S. & Resident Aliens) MUST be from one of the following:

1. Copy of an approved and active DD2345 for the individual, OR 2. Copy of an approved and active DD2345 for the individual’s employer PLUS evidence of current employment status with that employer (corporate ID,

business card, etc.), OR 3. A listing of the individual’s employer in the most recent DoD quarterly Qualified U.S. Contractor Access List PLUS evidence of current employment status

with that employer (corporate ID, business card, etc.). DD Form 2345 may be downloaded and completed online in order to apply for approval to be listed on the Qualified U.S. Contractor List, www.dlis.dla.mil/jcp. Allow at least 4-6 week (or longer) prior to the AIAA technical conference dates for you to receive the approval and be listed on the Qualified U.S. Contractor List. How to get your ITAR Clearance: Bring all of the above listed identification, proof of employment and certification credentials to the AIAA ITAR Registration Desk in the AIAA Registration area. Your documents will be verified and you will be provided with a stamp indicating your ITAR clearance. Photo ID will be checked against your ITAR badge before admittance is granted to any ITAR presentation.

Please be advised that all policies and procedures MUST be followed or admittance to restricted sessions will not be permitted.


IntroExposition Hall

Exhibitors by Booth Number

217 AIAA North Texas Section420 Altair213 ANSYS410 Applied Dynamics International (ADI)403 BETA CAE Systems USA, Inc.219 DARcorporation209 Desktop Aeronautics207 dSPACE408 DUNMORE Corporation208 Ennova Technologies, Inc.215 ESI North America211 ESTECO404 Exa Corporation307 G.R.A.S. Sound & Vibration412 Kamatics/RWG

314 Lockheed Martin320 MathWorks301 OPAL-RT Technologies401 Photron302 Pointwise, Inc.309 SG - Space & Ground Engineering Solutions303 Software Cradle304 Tecplot Inc.301 VectorNav Technologies416 Vision Research414 XFlow CFD

ENTRANCE

208 307 408

309 410

LoungeExhibitor

ADIDesktop

DUNMORE

30

SG

Altair

301 302

303 304

Software

MathWorks

ANSYS

dSPACE

Cradle

OPAL-RT Pointwise

Tecplot

XFlow CFD

Ennova

401

403 404

BETA CAE

Photron

G.R.A.S.

Exa Corp

Kamatics/RWG

AIAA Pavilion


IntroThe Exposition Hall is the hub of activity during this event—from seeing exhibitor displays to enjoying networking breaks and other functions. All the major networking events are held in the Exposition Hall to give attendees and exhibitors an opportunity to connect with partners, industry thought leaders, and collaborators who can help move your business forward. The Exposition Hall is located in the Chantilly Ballroom East.

Exposition Hall HoursTuesday, 23 June 0900–1230 hrs

1400–1600 hrs Reception* 1730–1900 hrs

Wednesday, 24 June 0900–1200 hrs 1230–1600 hrs

Thursday, 25 June 0900–1200 hrs

*A ticket is required and included in the registration fee where indicated

AIAA PavilionStop by the AIAA Pavilion, located in the Exposition Hall, to browse publications and merchandise, learn about your membership benefits, and meet AIAA staff.

30% Off All Books at AIAA AVIATION 2015 AIAA Publications is offering a special show discount on all titles featured at AVIATION 2015. Attendees can take advantage of a 30% discount off the list price of all books for sale at the AIAA Bookstore located in the AIAA Pavilion. This show special will only be available during the forum! Take advantage of these super savings and visit the AIAA Bookstore!

Exposition Hall


ExhibitorsAIAA North Texas Section 217

Altair 4201820 E Big Beaver Road Troy, MI [email protected]

Altair is a leader in developing simulation-driven designs for leading aerospace customers. Our world-class optimization methods provide designs that are lower weight, higher quality, and have better performance vs. traditional designs.

ANSYS, Inc. 2132600 ANSYS Drive Cannonsburg, PA 15317 [email protected]

ANSYS, Inc. develops and globally markets engineering simulation software used by designers and engineers across the aerospace and defense industry. Our open and flexible simulation solutions enable users to simulate design performance using an open platform for fast, efficient and cost-effective product development.

Applied Dynamics International 4103800 Stone School Road Ann Arbor, MI [email protected]

Applied Dynamics helps companies make better use of simulation assets through all stages of product development, verification testing, demonstration, training, and maintenance. Our user base includes more than 50% of the Fortune 500 aerospace and defense companies and extends into marine, power systems, oil & gas, and the automotive industry.

BETA CAE Systems USA, Inc. 40329800 Middlebelt Road Suite #100Farmington Hills, MI [email protected]

BETA CAE Systems is an engineering services company that distributes & supports the industry leading ANSA & META software. ANSA is CAE pre-processing tool for FE & CFD Analysis, for full-model build, from CAD to solver input file, in one integrated environment. META is a post-processor for analyzing results from ANSYS, NASTRAN, ABAQUS, LS-DYNA, PAMCRASH, RADIOSS, MADYMO, FLUENT, STAR CCM, CFD++ & other solvers.

DARcorporation 2191440 Wakarusa Drive Lawrence, KS [email protected]

DARcorporation (Design, Analysis and Research Corporation) is an aeronautical engineering firm, located in Lawrence, Kansas, that has been offering aeronautical engineering consulting services, software and books since 1991.

Desktop Aeronautics Inc. 2091900 Embarcadero Road Suite 101Palo Alto, CA [email protected]

Desktop Aeronautics is a software company that licenses tools for the aerodynamic design and analysis of aerospace vehicles. Our flagship product, GoCart, is an intuitive aerial vehicle design tool built around NASA’s renowned Cartesian Euler CFD solver, Cart3D. Our customers include major players from the aerospace industry and academia.

dSPACE 20750131 Pontiac Trail Wixom, MI [email protected]

dSPACE is the world’s leading provider of hardware and software tools for developing and testing sophisticated electronic control systems. dSPACE systems play a vital role in product innovation industries. Learn more at: www.dspaceinc.com.

DUNMORE Corporation 408145 Wharton Road

R

Bristol, PA [email protected]

DUNMORE is a manufacturer of engineered films and tapes for aerospace, supplying multilayer insulation materials to the aerospace industry for over twenty-five years. With a highly technical product base of over 400 certified products, DUNMORE is the trusted source for engineered aerospace films and tapes.


Ennova Technologies Inc 2082150 Allston Way, Suite 250

EnnovaScalable Simulation Delivered

Berkeley, CA [email protected]

Ennova Technologies delivers today’s most scalable simulation platform combining the power of cloud based computing, advanced geometry repair tools, and mixed mode meshing to create an extremely efficient pre and post processing simulation environment.

ESI North America 21532605 West Twelve Mile Road, Ste 350 Farmington Hills, MI [email protected]

ESI’s 1,000 Virtual Prototyping and Mfg Simulation specialists serve clients in over 40 countries. For over 40 years, ESI’s simulation software suite has been used to tackle the toughest Acoustics, Crash, VR, Composites, Casting, Welding, Forming, and CFD engineering challenges—earning the slogan “We get it right.” For more info: www.esi-group.com

ESTECO 21139555 Orchard Hill Place Novi, MI [email protected]

ESTECO is a pioneer in numerical optimization solutions, specializing in the research and development of engineering software for all stages of the simulation-driven design process. ESTECO’s top-class products, modeFRONTIER and SOMO, are used worldwide, helping companies increase efficiency in design simulation and accelerate product innovation.

Exa Corporation 40455 Network Drive Burlington, MA [email protected]

Exa Corporation offers a full suite of CFD/CAE simulation design optimization software applications with aerodynamic, thermal and aeroacoustic simulation capabilities in addition to engineering consulting services. Exa’s products and services enable engineers to integrate simulation early in the design process, therefore creating competitive designs, shortening product design cycles and speeding time-to-market.

G.R.A.S. Sound & Vibration 3072234 E Enterprise Parkway Twinsburg, OH [email protected]

G.R.A.S. has concentrated its efforts and expertise on the development and production of front-end acoustic products. This includes in principle all products necessary for the precise and reliable measurement, and recording of acoustic signals, from the transducer to the input of the A/D converter. The main line of instrumentation includes a broad range of standard measurement microphones and preamplifiers, all designed and manufactured in accordance with international standards.

Kamatics/RWG 4121330 Blue Hills Ave Bloomfield, CT 06002www.kaman.com/[email protected]

For decades, Kamatics (USA) and RWG have been designing, testing, and manufacturing the highest performing bearings and flight critical parts in the industry, excelling under the most demanding conditions.

Lockheed Martin Corporation 314P.O. Box 748 MZ 1500 Fort Worth, TX 76101 www.lockheedmartin.com [email protected]

Lockheed Martin is principally engaged in the research, design, development, manufacture, integration and sustainment of advance technology systems, products and services.

MathWorks 3203 Apple Hill Drive Natick, MA 01760www.mathworks.com/academia

The MATLAB and Simulink product families are fundamental applied math and computational tools at the world’s educational institutions. Adopted by more than 5000 universities and colleges, MathWorks products accelerate the pace of learning, teaching, and research in engineering and science. MathWorks products also help prepare students for careers in industry worldwide, where the tools are widely used for data analysis, mathematical modeling, and algorithm development in collaborative research and new product development.

Exhibitors


IntroOPAL-RT TECHNOLOGIES 3011751 Richardson, Suite 2525 Montreal Quebec H3K [email protected]

OPAL-RT: From Imagination… to Real-Time. OPAL-RT TECHNOLOGIES is a world leading developer of open, Real-Time Digital Simulators and Hardware-in-the-Loop testing equipment for electrical, electro-mechanical and power electronics systems. Our simulators are used by engineers and researchers at leading manufacturers, utilities, universities and research centers around the world.

Photron 4019520 Padgett Street, Suite 110 San Diego, CA [email protected]

Photron’s wide range of light sensitive high-speed cameras including systems ideally suited to PIV and DIC, mega pixel to 21,000 frames per second (fps) and 4M pixels producing HD to 2,000 fps. Photron has a slow motion camera for every application.

Pointwise, Inc. 302213 S. Jennings Avenue Fort Worth, TX [email protected]

Pointwise is solving the top problem facing engineering analysts today: grid generation and preprocessing for computational fluid dynamics. Since 1994, Pointwise has supplied meshing tools to engineers and scientists worldwide.

SG-Space & Ground Engineering Solutions 3096A Aigiidon Street Athens, Attica Greece [email protected]

SG Company provides integrated engineering solutions for air/space-based earth monitoring systems and develops special techniques for UAS (Unmanned Aerial Systems) earth observation applications in various disciplines.

Software Cradle 30370 Birch Alley, Suite 240 Beavercreek, OH [email protected]

Software Cradle is a leading provider of Computational Fluid Dynamics (CFD) software including SC/Tetra (unstructured mesh), scSTREAM (general purpose Cartesian mesh), and Heat Designer (Cartesian mesh for electronics). Since inception in 1984, Cradle has established itself as a major innovator for advancing the role of simulation in engineering design.

Tecplot, Inc 3043535 Factoria Blvd SE, Suite 550 Bellevue, WA [email protected]

Tecplot visualization tools—for simulations, analyses, and experiments—provide insight and understanding into the mechanisms inside your data. Information critical in pinpointing problems, optimizing designs, and explaining physical observations.

VectorNav Technologies 30110501 Markison Road Dallas, TX [email protected]

VectorNav specializes in high-performance inertial navigation systems using the latest MEMS sensor and GPS/GNSS technology. Since its founding in 2008, we have been providing customers worldwide fully calibrated inertial sensors with aerospace-grade filtering technology, expanding the possibilities of today’s inertial navigation technology.

Vision Research 416100 Dey Road Wayne, NJ 07470 www.visionresearch.com [email protected]

Vision Research designs and manufactures high-speed digital imaging systems with unsurpassed light-sensitivity, image resolution, acquisition speed and image quality. Marketed under the Phantom®brand,these cameras enable users to visualize and analyze physical phenomena when it’s too fast to see, and too important not to™.

XFlow CFD 41440 Chellis Street White River Junction, VT 05001 www.xflowusa.com [email protected].

XFlow™ CFD is the next-generation, meshless CFD package for modeling external aerodynamics of fixed-wing and rotorcraft aircraft. XFlow supports complex motion of complicated moving parts to model dynamic effects of control surface motion in flight, high-lift (take-off and landing) configurations and/or separation of munitions or separable stores.

Exhibitors


IntroGeneral InformationAIAA Registration and Information Center HoursThe AIAA Registration and Information Center will be located on the Ballroom Level at the Hyatt Regency. Hours are as follows:Sunday, 21 June 1500–1900 hrsMonday, 22 June – Thursday, 25 June 0700–1730 hrsFriday, 26 June 0700–1200 hrs

Wi-Fi Internet Access On SiteAIAA is providing limited Wi-Fi service for attendees to use while on site. To keep this service available and optimized for all attendees, please do not download files larger than 2MB, create multiple sessions across multiple devices, or download multiple files in one session. If you receive an error message that an AIAA server is blocking your current IP address, please inform the AIAA registration desk.

Social Media KiosksThroughout the forum, social media kiosks will display content shared by forum attendees! Look for your tweets or instagrams to be displayed on the screens. AIAA is also hosting a competition where the user who has posted the most tweets during the forum will win a prize.

Conference ProceedingsProceedings for the forum will be available online. The cost is included in the registration fee where indicated. Online proceedings will be available on 22 June 2015. Attendees who register in advance for the online proceedings will be provided with instructions on how to access them. Those registering on site will be provided with instructions at that time. Proceedings:1. To view proceedings visit

www.aiaa.org >ARC>Meeting Papers.a. Log in with the link at the top right of the page.b. Select the appropriate conference from the list.c. Search for individual papers with the Quick Search

toolbar in the upper-right corner of the page:i. By paper number: Click the “Paper Number” link,

select the conference year, and enter the paper number. ii. Use the Search textbox to find papers by author, title,

or keyword. The Advanced Search link provides additional search information and options.

2. All manuscript files submitted at least four days prior to the conference are currently in the proceedings. Files submitted after that date, both original and revised manuscripts, will not be available until the final proceedings update, which may take up to 15 business days after the last day of the conference.

3. Direct any questions concerning access to proceedings and/or ARC to [email protected].

Manuscript Revisions:1. Manuscript revision is open for all presenting authors from

0900 hrs Eastern Time, Monday, 22 June, through 2000 hrs Eastern Time, Wednesday, 8 July.

2. Revisions submitted for manuscripts already online will not refresh until after the proceedings have been updated, which may take up to 15 business days after the last day of the conference.


IntroGeneral InformationCertificate of Attendance Certificates of Attendance are available for attendees who request documentation at the forum itself. The Certificates of Attendance will be available for attendees to print at a self-service station at the registration desk starting Wednesday, 24 June. AIAA offers this service to better serve the needs of the professional community. Claims of hours or applicability toward professional education requirements are the responsibility of the participant.

Employment OpportunitiesAIAA members can post and browse resumes, browse job listings, and access other online employment resources by visiting the AIAA Career Center at http://careercenter.aiaa.org. Additionally, a message board will be available for postings in the Exposition Hall.

MembershipAIAA is your vital lifelong link to the collective creativity and brainpower of the aerospace profession and a champion for its achievements – and nonmembers who pay the full conference registration fee will receive their first year’s AIAA membership at no additional cost! Students who are not yet members may apply their registration fee toward their first year’s student member dues. (Free membership is not included in discounted group-rate registration.)

AIAA Foundation Since 1996 the AIAA Foundation has provided programs and support for educators and students. Through classroom grants, scholarships, awards, design competitions, and student conferences, the AIAA Foundation has encouraged students in grades K-12 and at the university level to discover the aerospace industry and become the next generation of scientists and engineers. Please consider making a donation so that the Foundation can continue to provide the resources needed to support aerospace education and to recognize innovation at all levels. For more information and to donate online, please visit www.aiaafoundation.org.

Young Professional Guide for Gaining Management SupportYoung professionals have the unique opportunity to meet and learn from some of the most important people in the business by attending conferences and participating in AIAA activities. A detailed online guide, published by the AIAA Young Professional Committee, is available to help you gain support and financial backing from your company. The guide explains the benefits of participation, offers recommendations, and provides an example letter for seeking management support and funding, and shows you how to get the most out of your participation. The online guide can be found on the AIAA website at www.aiaa.org/YPGuide.

Nondiscriminatory PracticesAIAA accepts registrations irrespective of race, creed, gender, color, sexual orientation, physical handicap, and national or ethnic origin.

RestrictionsPhotos, video, or audio recording of sessions or exhibits, as well as the unauthorized sale of AIAA-copyrighted material, is prohibited.

International Traffic in Arms Regulations (ITAR)AIAA speakers and attendees are reminded that some topics discussed in the conference could be controlled by the International Traffic in Arms Regulations (ITAR). U.S. nationals (U.S. citizens and permanent residents) are responsible for ensuring that technical data they present in open sessions to non-U.S. nationals in attendance or in conference proceedings are not export restricted by the ITAR. U.S. nationals are likewise responsible for ensuring that they do not discuss ITAR export-restricted information with non-U.S. nationals in attendance.


IntroGeneral Information

AIAA is the world’s largest aerospace professional society, serving a diverse range of more than 30,000 individual members from 88 countries, and 95 corporate members. AIAA members help make the world safer, more connected, more accessible, and more prosperous. For more information, visit www.aiaa.org, or follow us on Twitter @AIAA.American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500 Reston, VA 20191-4344 703.264.7500 or 800.639.AIAA (2422) Fax: 703.264.7657 [email protected] www.aiaa.org

Speakers’ Briefings in Session RoomsAuthors who are presenting papers will meet with session chairs and co-chairs in their session rooms for a short 30-minute briefing on the day of their sessions to exchange bios and review final details prior to the session. Please attend on the day of your session(s). Laptops preloaded with the Speaker Briefing preparation slides will be provided in each session room. Speaker’s Briefing schedule is as follows:Monday 22 June–Friday 26 June, 0730 hrs

Speakers’ Practice RoomSpeakers who wish to practice their presentations may do so in the Peridot room. A sign-up sheet will be posted on the door. In consideration of others, please limit practice time to 30-minute increments.

Session Chair ReportsAll session chairs are asked to complete a session chair report to evaluate their session for future planning. AIAA has partnered with Canvas Solutions to provide an electronic Session Chair Report form. You can download the FREE mobile app in your App Store, AppWorld, or Marketplace by searching for “Canvas Solutions, Inc.” The mobile app is free, so please be sure to download it. Detailed instructions will be provided in the session rooms. If you do not have a tablet or a smartphone, simply use the report form as a guide and enter your session chair report information at the session chair reporting computer station located on site near the AIAA registration area. Report data will be collected and used for future planning purposes, including session topics and room allocations. Please submit your session chair report electronically by Friday, 26 June 2015.

AudiovisualEach session room will be preset with the following: one LCD projector, one screen, one microphone and sound system (if necessitated by room size), and one laser pointer. Laptop computers will also be provided. You may also use your own computer. Any additional audiovisual equipment requested onsite will be at cost to the presenter. Please note that AIAA does not provide security in the session rooms and recommends that items of value not be left unattended

“No Paper, No Podium” and “No Podium, No Paper” PolicyIf a written paper is not submitted by the final manuscript deadline, authors will not be permitted to present the paper at the forum. Also, if the paper is not presented at the forum, it will be withdrawn from the proceedings. It is the responsibility of those authors whose papers or presentations are accepted to ensure that a representative attends the conference to present the paper. These policies are intended to improve the quality of the program for attendees..

Journal PublicationAuthors of appropriate papers are encouraged to submit them for possible publication in one of the Institute’s archival journals: AIAA Journal; Journal of Aircraft; Journal of Guidance, Control, and Dynamics; Journal of Propulsion and Power; Journal of Spacecraft and Rockets; Journal of Thermophysics and Heat Transfer; or Journal of Aerospace Information Systems (formerly Journal of Aerospace Computing, Information, and Communication). You may now submit your paper online at http://mc.manuscriptcentral.com/aiaa.

Author and Session Chair Information


IntroTime Title Location

Sunday, 21 June 20150900-1600 CASE Academics Batik A & B

1400-1500 GTTC Steering Subcommittee Miro

1400-1500 APATC New Member Orientation Dardanelles

1430-1500 APATC Liaisons Subcommittee Fleur de lis A

1500-1600 APATC Education Subcommittee Milan

1500-1600 APATC Honors and Awards Subcommittee Ming

1500-1600 APATC Membership and Nominations Subcommittee Inverness

1500-1600 APATC Planning Subcommittee Lalique

1500-1600 APATC Publicity and Publications Subcommittee Edelweiss

1500-1600 GTTC Introduction/Overview Miro

1600-1700 GTTC Program Subcommittee Miro

1600-1700 APATC Technical Activities Meeting Edelweiss

1600-1700 FDTC Higher Order Methods WG Dardanelles

1700-1800 APATC Steering Committee Ming

1700-1800 GTTC Conferences Subcommittee Miro

1730-1830 FDTC New Member Orientation Fleur de lis A

1730-2100 Atmospheric Flight Mechanics TC Dardanelles

1800-1900 GTTC Publications Subcommittee Miro

1800-2100 Applied Aerodynamics TC Metropolitan

1830-2000 FDTC Steering Committee Fleur de lis A

1900-2000 GTTC Education and Student Activities Subcommittee Miro

1900-2100 FDTC Transition DG Cardinal A

1900-2100 TAC Aircraft and Atmospheric Systems Group Cardinal B

2000-2100 GTTC Awards Subcommittee Miro

2000-2100 AMTTC Conference Subcommittee Milan

Monday, 22 June 20150800-1200 GTTC WT Model Attitude and Deformation Measurement WG Dardanelles

1100-1400 General Aviation TC Morocco

1200-1400 Aircraft Electric Propulsion Path Forward Batik B

1200-1400 Aviation MDO SPC Dardanelles

1300-1500 GTTC FoGT Experimental and Computational Aero Development Coordination

Cardinal A & B

1500-1600 FDTC Reduced Order Modeling DG Dardanelles

1600-1700 TPTC New Member Meeting Cooper

1600-1700 FDTC Flow Control - Barriers/Challenges to Tech Trans Cardinal A

1630-1800 Atmospheric and Space Environments TC Batik A

1700-1900 Computational Fluid Dynamics Committee on Standards Batik B

1730-1830 GTTC Committee on Standards Cardinal A

1730-1830 APATC Low Boom DG Cooper

1730-1900 APATC Validation of Numerical Models DG Dardanelles

1830-1930 AMTTC Awards Subcommittee Batik A

1830-2030 APATC Rotorcraft Simulations and Performance Predictions DG Cardinal B

Committee Meetings



Monday, 22 June 2015 (continued) 1900-2100 TAC Aerospace Sciences Group Batik B

1900-2100 FDTC Computational Fluid Dynamics Subcommittee Dardanelles

1900-2100 FDTC Flow Control and Fluid Applications Subcommittee Cardinal A

1900-2100 FDTC Fundamentals of Flow Phenomena Subcommittee Cooper

1900-2200 Aircraft Design TC Monte Carlo

Tuesday, 23 June 20150800-1600 GTTC Internal Balance WG Cooper

0800-1600 GTTC Dual Flow Reference Nozzle WG - Day 1 Batik A

0930-1200 DETC Subcommittee Batik B

1400-1500 Journal of Thermophysics and Heat Transfer Malta

1500-1600 TPTC Awards Subcommittee Cardinal A

1500-1600 TPTC Publications Subcommittee Dardanelles

1600-1700 TPTC Conferences Subcommittee Cardinal A

1600-1700 TPTC Best Paper Subcommittee Batik B

1700-1800 TPTC Nominations Subcommittee Cardinal A

1700-1800 TPTC Education Subcommittee Cooper

1730-1900 FDTC Low Re DG Dardanelles

1800-1900 FDTC Free Shear Layer Mixing Layer Control DG Batik A

1800-1900 TPTC Publicity Subcommittee Cooper

1800-2100 Design Engineering TC Batik B

1900-2000 APATC Low Reynolds Number Aerodynamics DG Dardanelles

1900-2200 Air Transportation Systems TC Monte Carlo

1900-2200 MVCETC Meshing 2030 Subcommittee Batik A

1900-2200 Fluid Dynamics TC Cardinal A & B

1900-2200 Thermophysics TC Monet Ballroom

1900-2200 Plasmadynamics and Lasers TC Rosetta

1930-2130 Aeroacoustics TC Miro

2000-2300 Aerodynamic Measurement Technology TC Cooper

Wednesday, 24 June 20150800-1200 GTTC Future of Ground Testing WG Cardinal A & B

0800-1200 GTTC Dual Flow Reference Nozzle WG - Day 2 Cooper

1200-1600 GTTC Uncertainty Analysis WG Cooper

1500-1600 AVIATION 2016 Technical Program Committee Dardanelles

1730-1900 GTTC Student Meet and Greet Stemmons A

1730-1830 FDTC Large Eddy Simulation DG Monte Carlo

1730-1830 Green Engineering PC Malta

1800-1900 FDTC Future of Fluids Subcommittee Cooper

1800-1900 FDTC Turbulence Model Benchmarking WG Cardinal A

1830-2000 Plasma Aerodynamics DG Cardinal B

1830-1930 AMTTC Nominations Subcommittee Edelweiss

1830-2000 FDTC Non-Equilibrium DG Dardanelles

1830-2200 Multidisciplinary Design Optimization TC Batik A & B

1900-2000 FDTC Solver Technology for Turbulent Flows Cardinal A

1900-2200 V/STOL Aircraft Systems TC Cooper

1900-2200 Meshing, Visualization and Computational Environments TC Fleur de lis B

Committee Meetings



Thursday, 25 June 20150900-1100 CASE Planning Committee Monte Carlo

0900-1700 GTTC Wind Tunnel Flow Quality WG Cooper

1600-1730 APATC Missile and Projectile Aeroprediction DG Dardanelles

1730-1830 AMTTC Conferences Subcommittee Milan

1800-2100 Ground Testing TC Cardinal A & B

1800-2100 Transformational Flight PC Batik A & B

1830-2130 Modeling and Simulation TC Cooper

1900-2200 Flight Testing TC Coral

Committee Meetings


IntroSessions at a GlanceAbbreviation Title Date Start Time Location

Aeroacoustics3-AA-1 Airframe Noise I 22-Jun 0900 hrs Fleur-de-lis A

4-AA-2 Jet Noise Prediction I 22-Jun 0900 hrs Fleur-de-lis B

5-AA-3 Jet Noise Modeling I 22-Jun 0900 hrs Inverness

6-AA-4 CAA Numerical Techniques I 22-Jun 0900 hrs Lalique

7-AA-5 Duct Acoustics I 22-Jun 0900 hrs Obelisk A

37-AA-6 Open Rotor I 22-Jun 1400 hrs Fleur-de-lis A

38-AA-7 Trailing Edge Noise I 22-Jun 1400 hrs Fleur-de-lis B

39-AA-8 Jet Noise Prediction II 22-Jun 1400 hrs Inverness

40-AA-9 Jet Noise Measurements I 22-Jun 1400 hrs Lalique

41-AA-10 CAA Sound Generation I 22-Jun 1400 hrs Obelisk A

77-AA-11 Fan Noise 23-Jun 0900 hrs Fleur-de-lis A

78-AA-12 Duct Acoustics II 23-Jun 0900 hrs Fleur-de-lis B

79-AA-13 Trailing Edge Noise II 23-Jun 0900 hrs Inverness

80-AA-14 Jet Noise Prediction III 23-Jun 0900 hrs Lalique

81-AA-15 CAA Numerical Techniques II 23-Jun 0900 hrs Obelisk A

112-AA-16 CAA Sound Generation II 23-Jun 1400 hrs Fleur-de-lis A

113-AA-17 CAA Propagation and Scattering I 23-Jun 1400 hrs Fleur-de-lis B

114-AA-18 General Acoustics I 23-Jun 1400 hrs Inverness

115-AA-19 Airframe Noise II 23-Jun 1400 hrs Lalique

116-AA-20 Duct Acoustics III 23-Jun 1400 hrs Obelisk A

151-AA-21 Turbomachinery and Core Noise 24-Jun 0900 hrs Fleur-de-lis B

152-AA-22 General Acoustics II 24-Jun 0900 hrs Inverness

153-AA-23 Jet Noise Near Field and Jet Noise Reduction 24-Jun 0900 hrs Lalique

154-AA-24 CAA Propagation and Scattering II 24-Jun 0900 hrs Obelisk A

155-AA-25 Benchmark Problems for Airframe Noise Computations III (BANC-III) Summary (Invited) 24-Jun 0900 hrs Fleur-de-lis A

185-AA-26 Combustion Noise 24-Jun 1400 hrs Fleur-de-lis B

186-AA-27 Arrays Method Panel Session 24-Jun 1400 hrs Fleur-de-lis A

187-AA-28 Open Rotor II 24-Jun 1400 hrs Inverness

188-AA-29 Airframe Noise III 24-Jun 1400 hrs Lalique

189-AA-30 Jet Noise Measurements II 24-Jun 1400 hrs Obelisk A

226-AA-31 Interior Noise 25-Jun 0900 hrs Edelweiss

227-AA-32 Jet Noise Measurements III 25-Jun 0900 hrs Fleur-de-lis A

228-AA-33 Jet Noise Modeling II 25-Jun 0900 hrs Fleur-de-lis B

229-AA-34 CAA Numerical Techniques III 25-Jun 0900 hrs Inverness

230-AA-35 Airframe Noise IV 25-Jun 0900 hrs Lalique

231-AA-36 General Acoustics III 25-Jun 0900 hrs Obelisk A

259-AA-37 Landing Gear Noise 25-Jun 1400 hrs Edelweiss

260-AA-38 Fluid-Structure Interaction 25-Jun 1400 hrs Fleur-de-lis A

261-AA-39 Fluid Acoustic Phenomena 25-Jun 1400 hrs Fleur-de-lis B

262-AA-40 Advanced Testing Techniques 25-Jun 1400 hrs Inverness

263-AA-41 CAA Numerical Techniques IV 25-Jun 1400 hrs Lalique

264-AA-42 Fan Broadband Noise Prediction 25-Jun 1400 hrs Obelisk A



Aircraft Design42-ACD-1 Aircraft Design for Environmental Impact Reduction 22-Jun 1400 hrs Miro

82-ACD-2 Aircraft Design Methods and Tools 23-Jun 0900 hrs Wyeth

117-ACD-3 Aircraft Performance Studies 23-Jun 1400 hrs Wyeth

156-ACD-4 General Aviation 24-Jun 0900 hrs Morocco

190-ACD-5 Design of Unconventional Aircraft Configurations 24-Jun 1400 hrs Morocco

232-ACD-6 Conceptual Aircraft Design Working Group (CADWG21) Panel 25-Jun 0900 hrs Wyeth

265-ACD-7 Aircraft Subsystems, Integration, and Architectures 25-Jun 1400 hrs Wyeth

293-ACD-8 Aeronautic Discipline Considerations in Aircraft Design 26-Jun 0900 hrs Miro

Atmospheric Flight Mechanics8-AFM-1 Aircraft Flight Dynamics, Control, Handling Qualities and Performance I 22-Jun 0900 hrs Plum Blossom A

9-AFM-2 Aeroservoelastic (ASE) Modeling 22-Jun 0900 hrs Plum Blossom B

43-AFM-3 Unmanned Aircraft Systems I 22-Jun 1400 hrs Plum Blossom A

44-AFM-4 Planetary Entry and Aeroassist Technology 22-Jun 1400 hrs Plum Blossom B

83-AFM-5 Aircraft Flight Dynamics, Control, Handling Qualities and Performance II 23-Jun 0900 hrs Plum Blossom A

84-AFM-6 Aeroservoelastic (ASE) and Aerodynamic Prediction Methods 23-Jun 0900 hrs Plum Blossom B

118-AFM-7 Flight Test, System Identification, and Parameter Estimation 23-Jun 1400 hrs Plum Blossom A

119-AFM-8 Launch Vehicles, Missiles, and Projectile Flight Mechanics 23-Jun 1400 hrs Plum Blossom B

157-AFM-9 Unmanned Aircraft Systems II 24-Jun 0900 hrs Plum Blossom A

Aerodynamic Measurement Technology and Ground Testing10-AMT-1/GT-1 Hap Arnold's New Horizon: The Future Role of Ground Test in High Speed System

Development22-Jun 0900 hrs Obelisk B

11-AMT-2/GT-2 Line of Sight and Density Measurement 22-Jun 0900 hrs Edelweiss

45-AMT-3/GT-3 Advances in Test Methodology and CFD Integration 22-Jun 1400 hrs Obelisk B

46-AMT-4/GT-4 Surface and Inflow Sensing 22-Jun 1400 hrs Edelweiss

85-AMT-5/GT-5 Model Attitude, Deformation, and Data Acquisition Techniques 23-Jun 0900 hrs Obelisk B

86-AMT-6/GT-6 Spatially-Resolved Spectroscopic Techniques 23-Jun 0900 hrs Edelweiss

120-AMT-7/GT-7 Design of Experiment 23-Jun 1400 hrs Obelisk B

121-AMT-8/FD-14/TP-6/GT-8

Molecular-Based Optical Diagnostics for Hypersonic Nonequilibrium Flows 23-Jun 1400 hrs Topaz

158-AMT-9/GT-9 Ground Test Facility Improvements I 24-Jun 0900 hrs Obelisk B

159-AMT-10/GT-10 Particle-Based Velocimetry Applications and Developments 24-Jun 0900 hrs Topaz

191-AMT-11/GT-11 Ground Test Facility Improvements II 24-Jun 1400 hrs Obelisk B

192-AMT-12/GT-12 The Impact of PIV on Aerospace Technology I 24-Jun 1400 hrs Edelweiss

266-AMT-13/GT-13 The Impact of PIV on Aerospace Technology II 25-Jun 1400 hrs Topaz

280-FT-2/GT-14 Optimization Techniques in Flight Test/Ground Test 25-Jun 1400 hrs Obelisk B

294-AMT-14/GT-15 Aerodynamic Measurement Systems: Calibration and Monitoring 26-Jun 0900 hrs Topaz

Applied Aerodynamics12-APA-1 Aerodynamic-Structure Dynamics Interaction 22-Jun 0900 hrs Stemmons C

13-APA-2 Aerodynamic Design Methodologies I 22-Jun 0900 hrs Carpenter Ballroom

14-APA-3 Special Session: Low Boom Activities I 22-Jun 0900 hrs Stemmons A

15-APA-4 Propeller/Rotorcraft/Wind Turbine Aerodynamics I 22-Jun 0900 hrs Stemmons B

47-APA-5 Applied CFD & Numerical Correlations with Experimental Data I 22-Jun 1400 hrs Stemmons B

48-APA-6 Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs I 22-Jun 1400 hrs Carpenter Ballroom



Applied Aerodynamics (continued)49-APA-7 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for

Flexible Wing Technology I22-Jun 1400 hrs Stemmons A

50-APA-8 Flow Control Applications & Demonstrations (Active & Passive) I 22-Jun 1400 hrs Stemmons C

87-APA-9 High Angle of Attack and High Lift Aerodynamics 23-Jun 0900 hrs Stemmons C

88-APA-10 Wind Tunnel and Flight Testing 23-Jun 0900 hrs Carpenter Ballroom

89-APA-11 Special Session: Low Boom Activities II 23-Jun 0900 hrs Stemmons A

90-APA-12 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation I 23-Jun 0900 hrs Stemmons B

122-APA-13 Applied CFD & Numerical Correlations with Experimental Data II 23-Jun 1400 hrs Stemmons B

123-APA-14 Special Session: Historically Significant/Influential Papers in Applied Aerodynamics 23-Jun 1400 hrs Carpenter Ballroom

124-APA-15 Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology II

23-Jun 1400 hrs Stemmons A

125-APA-16 Flow Control Applications & Demonstrations (Active & Passive) II 23-Jun 1400 hrs Stemmons C

160-APA-17 Special Session: Hybrid CFD Method Assessments for F-16XL Aircraft Aerodynamics 24-Jun 0900 hrs Stemmons A

161-APA-18 Aerodynamic Design Methodologies II 24-Jun 0900 hrs Carpenter Ballroom

162-APA-19 Propeller/Rotorcraft/Wind Turbine Aerodynamics II 24-Jun 0900 hrs Stemmons B

180-PDL-8/APA-20 Plasma Aerodynamics & Flow Control IV 24-Jun 0900 hrs Stemmons C

193-APA-21 Transonic & Supersonic Aerodynamics 24-Jun 1400 hrs Stemmons A

194-APA-22 VSTOL/STOL Aerodynamics 24-Jun 1400 hrs Carpenter Ballroom

195-APA-23 Weapons Aerodynamics: Missile/Projectile/Guided-Munitions, Carriage and Store Separation II 24-Jun 1400 hrs Stemmons B

233-APA-25 Applied CFD & Numerical Correlations with Experimental Data III 25-Jun 0900 hrs Stemmons B

234-APA-26 Unmanned, Bio-Inspired, Solar Powered Aerial Vehicle Designs II 25-Jun 0900 hrs Carpenter Ballroom

235-APA-27 Airfoil/Wing/Configuration Aerodynamics 25-Jun 0900 hrs Stemmons C

236-APA-28 Unsteady Aerodynamics I 25-Jun 0900 hrs Stemmons A

267-APA-29 Innovative Aerodynamic Concepts & Designs 25-Jun 1400 hrs Carpenter Ballroom

268-APA-30 Low Speed, Low Reynolds Number Aerodynamics 25-Jun 1400 hrs Grand Ballroom A

269-APA-31 Vortical/Vortex Flow 25-Jun 1400 hrs Stemmons B

270-APA-32 Unsteady Aerodynamics II 25-Jun 1400 hrs Stemmons A

271-APA-33 Flow Control Applications & Demonstrations (Active & Passive) III 25-Jun 1400 hrs Stemmons C

295-APA-34 Icing or Roughness Effects on Vehicle Aerodynamics 26-Jun 0900 hrs Stemmons C

296-APA-35 Aerodynamic Design Methodologies III 26-Jun 0900 hrs Carpenter Ballroom

297-APA-37 Propeller/Rotorcraft/Wind Turbine Aerodynamics III 26-Jun 0900 hrs Stemmons B

Atmospheric and Space Environments163-ASE-1 Numerical Weather Prediction (Invited) 24-Jun 0900 hrs Plum Blossom B

196-ASE-2 Aircraft Icing and Atmospheric Hazards 24-Jun 1400 hrs Plum Blossom B

237-ASE-3 Aircraft Wake Turbulence I (Invited) 25-Jun 0900 hrs Plum Blossom B

272-ASE-4 Aircraft Wake Turbulence II (Invited) 25-Jun 1400 hrs Plum Blossom B

273-ASE-5 Atmospheric and Space Environments 25-Jun 1400 hrs Plum Blossom A


IntroAbbreviation Title Date Start Time Location

Aviation Technology, Integration, and Operations16-ATIO-1 Terminal & Surface Operations I 22-Jun 0900 hrs Manchester

17-ATIO-2 Separation Assurance 22-Jun 0900 hrs Ming

18-ATIO-3 Trajectory Optimization 22-Jun 0900 hrs Milan

19-ATIO-4 Transformational Flight - Rapid Concept to Flight 22-Jun 0900 hrs Metropolitan Ballroom

51-ATIO-5 Terminal & Surface Operations II 22-Jun 1400 hrs Manchester

52-ATIO-6 Fleet and Route Planning 22-Jun 1400 hrs Ming

53-ATIO-7 Systems Engineering and Analysis 22-Jun 1400 hrs Milan

54-ATIO-8 Transformational Flight - Enabling the Next Billion Dollar Aviation Market through Autonomy

22-Jun 1400 hrs Metropolitan Ballroom

91-ATIO-9 Terminal & Surface Operations III 23-Jun 0900 hrs Manchester

92-ATIO-10 ATM I - Trajectory Enhancements 23-Jun 0900 hrs Milan

93-ATIO-11 Transformational Flight - On-Demand Mobility 23-Jun 0900 hrs Metropolitan Ballroom

126-ATIO-12 ATM II - Air Traffic Analysis 23-Jun 1400 hrs Milan

127-ATIO-13 Transformational Flight - Advanced Concepts 23-Jun 1400 hrs Metropolitan Ballroom

128-ATIO-14 Product Design and Support 23-Jun 1400 hrs Manchester

164-ATIO-15 ATM III - Modeling in ATM 24-Jun 0900 hrs Metropolitan Ballroom

165-ATIO-16 Transformational Flight - Autonomy I 24-Jun 0900 hrs Monet Ballroom

166-ATIO-17 Human Factors in Aviation Operations 24-Jun 0900 hrs Milan

197-ATIO-18 ATM IV - Economic/Benefits Analysis 24-Jun 1400 hrs Ming

198-ATIO-19 Terminal & Surface Operations IV 24-Jun 1400 hrs Milan

199-ATIO-20 Transformational Flight - Autonomy II 24-Jun 1400 hrs Monet Ballroom

238-ATIO-21 En Route Operations 25-Jun 0900 hrs Milan

239-ATIO-22 ATM V - Performance Assessment 25-Jun 0900 hrs Morocco

240-ATIO-23 Transformational Flight - Electric Propulsion 25-Jun 0900 hrs Monet Ballroom

274-ATIO-24 UAS Integration & Operations I 25-Jun 1400 hrs Ming

275-ATIO-25 ATM VI - Management of NAS Resources 25-Jun 1400 hrs Morocco

276-ATIO-26 Transformational Flight - Unconventional VTOL Configurations 25-Jun 1400 hrs Monet Ballroom

298-ATIO-27 ATM VII - Weather Impact 26-Jun 0900 hrs Morocco

299-ATIO-28 Future Concepts 26-Jun 0900 hrs Wyeth

300-ATIO-29 UAS Integration & Operations II 26-Jun 0900 hrs Ming

Balloon Systems167-BAL-1 Balloon Systems I 24-Jun 0900 hrs Steuben

200-BAL-2 Balloon Systems II 24-Jun 1400 hrs Steuben

Complex Aerospace Systems Exchange (CASE)20-CASE-1 Academic Roundtable 22-Jun 0900 hrs Batik

59-F360-2/CASE-2 Whatever Happened to the Four-Year Airplane? 22-Jun 1400 hrs Grand Ballroom E

72-CASE-3 CASE Networking Social 22-Jun 1730 hrs Morocco

94-CASE-4 Applied Complexity Workshop 23-Jun 0900 hrs Grand Ballroom D

129-CASE-5 CASE Session I & II 23-Jun 1400 hrs Steuben

168-CASE-6 CASE Session II & III 24-Jun 0900 hrs Grand Ballroom D

207-F360-7/CASE-7 System Complexity : Government Needs and Practical Research Results 24-Jun 1400 hrs Grand Ballroom D

Sessions at a Glance


IntroAbbreviation Title Date Start Time Location

Computational Fluid Dynamics 21-CFD-1 Unstructured High-Order Methods I 22-Jun 0900 hrs Grand Ballroom A

22-CFD-2 Unsteady Flow Simulations 22-Jun 0900 hrs Grand Ballroom B

23-CFD-3 Meshing Techniques I 22-Jun 0900 hrs Coral

24-CFD-4 LES, DNS, and Hybrid RANS-LES I 22-Jun 0900 hrs Emerald

55-CFD-5 Unstructured High-Order Methods II 22-Jun 1400 hrs Grand Ballroom A

56-CFD-6 Novel Discretizations 22-Jun 1400 hrs Grand Ballroom B

57-CFD-7 Interdisciplinary CFD I 22-Jun 1400 hrs Coral

58-CFD-8 Turbulence Modeling and Uncertainty Quantification 22-Jun 1400 hrs Emerald

95-CFD-9 Adaptive High-Order Methods 23-Jun 0900 hrs Grand Ballroom A

96-CFD-10 Turbulent Flow Simulations I 23-Jun 0900 hrs Grand Ballroom B

97-CFD-11 Meshing Techniques II 23-Jun 0900 hrs Coral

98-CFD-12 LES, DNS, and Hybrid RANS-LES II 23-Jun 0900 hrs Emerald

130-CFD-13 Flux Reconstruction Methods 23-Jun 1400 hrs Grand Ballroom A

131-CFD-14 Adjoints and Error Estimation 23-Jun 1400 hrs Grand Ballroom B

132-CFD-15 Time Integration Methods 23-Jun 1400 hrs Coral

133-CFD-16 RANS Modeling 23-Jun 1400 hrs Emerald

134-CFD-37 CFD Flow Visualization Showcase 23-Jun 1400 hrs Chantilly Ballroom Foyer

169-CFD-17 Advances in High-Order Methods 24-Jun 0900 hrs Grand Ballroom A

170-CFD-18 Current Trends in CFD Research I (Invited) 24-Jun 0900 hrs Grand Ballroom B

171-CFD-19 LES, DNS, and Hybrid RANS-LES III 24-Jun 0900 hrs Coral

172-CFD-20 Turbulence Model Validation (Invited) 24-Jun 0900 hrs Emerald

201-CFD-21 Discontinuous Galerkin Methods 24-Jun 1400 hrs Grand Ballroom A

202-CFD-22 Future of Fluids: Next Generation CFD (Invited) 24-Jun 1400 hrs Grand Ballroom B

203-CFD-23 Parallel Computing and Novel Architectures 24-Jun 1400 hrs Plum Blossom A

204-CFD-24 Design Optimization 24-Jun 1400 hrs Coral

205-CFD-25 Turbulent Flow Simulations II 24-Jun 1400 hrs Emerald

241-CFD-26 Unstructured High-Order Methods III 25-Jun 0900 hrs Grand Ballroom A

242-CFD-27 Current Trends in CFD Research II (Invited) 25-Jun 0900 hrs Grand Ballroom B

243-CFD-28 Incompressible and Low Speed Flows 25-Jun 0900 hrs Plum Blossom A

244-CFD-29 High-Speed and Reacting Flows 25-Jun 0900 hrs Coral

245-CFD-30 Inflow Turbulence for Wall-Bounded LES (Invited) 25-Jun 0900 hrs Emerald

301-CFD-31 Visualization for CFD 2030 26-Jun 0900 hrs Grand Ballroom A

302-CFD-32 Post-Processing and Model Reduction 26-Jun 0900 hrs Grand Ballroom B

303-CFD-33 Interdisciplinary CFD II 26-Jun 0900 hrs Plum Blossom A

304-CFD-34 Multiphase and Nonequilibrium Flows 26-Jun 0900 hrs Coral

305-CFD-35 Overset and Cartesian Grid Methods 26-Jun 0900 hrs Plum Blossom B

306-CFD-36 LES, DNS, and Hybrid RANS-LES IV 26-Jun 0900 hrs Emerald

Sessions at a Glance



Fluid Dynamics25-FD-1 Wing Aerodynamics 22-Jun 0900 hrs Govenors Lecture

Hall

26-FD-2 Fundamental Fluid Flows 22-Jun 0900 hrs Senators Lecture Hall

27-FD-3 Combustion and Heat Transfer 22-Jun 0900 hrs Topaz

28-FD-4 Boundary Layer Transition: Hypersonic Flows 22-Jun 0900 hrs Sapphire

33-PDL-1/FD-5 Plasma Aerodynamics & Flow Control I 22-Jun 0900 hrs Monet Ballroom

60-FD-6/PDL-2 Plasma Aerodynamics & Flow Control II 22-Jun 1400 hrs Govenors Lecture Hall

61-FD-7 Boundary Layer Transition - Progress and Challenges 22-Jun 1400 hrs Sapphire

62-FD-8 Vortex Flows 22-Jun 1400 hrs Senators Lecture Hall

63-FD-9 Active and Passive Flow Control 22-Jun 1400 hrs Topaz

99-FD-10 Boundary-Layer Transition 23-Jun 0900 hrs Sapphire

100-FD-11 Unsteady Wing Aerodynamics I 23-Jun 0900 hrs Govenors Lecture Hall

101-FD-12 Airfoil Separation Control 23-Jun 0900 hrs Senators Lecture Hall

102-FD-13 Shock-Dominated Flows 23-Jun 0900 hrs Topaz

121-AMT-8/FD-14/TP-6/GT-8


136-FD-15 Unsteady Wing Aerodynamics II 23-Jun 1400 hrs Govenors Lecture Hall

137-FD-16 Boundary Layer Transition: Crossflow 23-Jun 1400 hrs Sapphire

138-FD-17 Boundary Layer and Bluff Body Control 23-Jun 1400 hrs Senators Lecture Hall

139-FD-18 Turbulence Modeling 23-Jun 1400 hrs Edelweiss

173-FD-19 Turbomachinery - Turbines 24-Jun 0900 hrs Senators Lecture Hall

174-FD-20 Shock Wave / Boundary Layer Interactions 24-Jun 0900 hrs Edelweiss

175-FD-22 Unsteady Flows - Cavity and Shear Flows 24-Jun 0900 hrs Govenors Lecture Hall

208-FD-23 Unsteady Wing Aerodynamics III 24-Jun 1400 hrs Govenors Lecture Hall

209-FD-24 Boundary Layer Transition: Receptivity and Control 24-Jun 1400 hrs Sapphire

210-FD-25 Flow Control Technologies - Barriers/Challenges to Tech Transition 24-Jun 1400 hrs Topaz

211-FD-26 Turbulence Simulations 24-Jun 1400 hrs Senators Lecture Hall

246-FD-27 Turbulence Analysis 25-Jun 0900 hrs Govenors Lecture Hall

247-FD-28 Transition Open Forum 25-Jun 0900 hrs Sapphire

248-FD-29 Flow Control - Aerodynamics 25-Jun 0900 hrs Senators Lecture Hall

278-FD-30 Hypersonic and Chemically-Reacting Flows 25-Jun 1400 hrs Sapphire

279-FD-31 Flow Control - Vortical Flows 25-Jun 1400 hrs Senators Lecture Hall



Flight Testing249-FT-1 Flight Testing 25-Jun 0900 hrs Obelisk B

280-FT-2/GT-14 Optimization Techniques in Flight Test/Ground Test 25-Jun 1400 hrs Obelisk B

Green Engineering281-GEPC-1 Overview of NASA Advanced Air Vehicles Program 25-Jun 1400 hrs Metropolitan

Ballroom

ITAR Sessions103-ITAR-1 ITAR - Hypersonic Flow Phenomena (Invited) 23-Jun 0900 hrs Morocco

140-ITAR-2 ITAR - Aircraft Design and Modeling 23-Jun 1400 hrs Morocco

Lighter-Than-Air Systems250-LTA-1 Lighter-than-Air Systems & Technologies I 25-Jun 0900 hrs Steuben

282-LTA-2 Lighter-than-Air Systems & Technologies II 25-Jun 1400 hrs Steuben

Multidisciplinary Analysis and Optimization29-MAO-1 Vehicle Design Applications I 22-Jun 0900 hrs Madrid

64-MAO-2 Vehicle Design Applications II 22-Jun 1400 hrs Madrid

104-MAO-3 Applications I 23-Jun 0900 hrs Madrid

141-MAO-4 Applications II 23-Jun 1400 hrs Madrid

176-MAO-5 Emerging Methods I 24-Jun 0900 hrs Madrid

212-MAO-6 Emerging Methods II 24-Jun 1400 hrs Madrid

213-MAO-7 Metamodeling I 24-Jun 1400 hrs Manchester

251-MAO-8 Metamodeling II 25-Jun 0900 hrs Manchester

252-MAO-9 Shape and Topology I 25-Jun 0900 hrs Madrid

283-MAO-10 Shape and Topology II 25-Jun 1400 hrs Madrid

284-MAO-11 Uncertainty I 25-Jun 1400 hrs Manchester

307-MAO-12 Shape and Topology III 26-Jun 0900 hrs Madrid

308-MAO-13 Uncertainty II 26-Jun 0900 hrs Manchester

Modeling and Simulation Technologies30-MST-1 Unmanned Aerial Vehicle Systems 22-Jun 0900 hrs Travertine

31-MST-2 Aviation Systems Human Factors 22-Jun 0900 hrs Wyeth

65-MST-3 Air Traffic Management 22-Jun 1400 hrs Travertine

66-MST-4 Guidance, Control, and Dynamics I 22-Jun 1400 hrs Wyeth

105-MST-5 Guidance, Control, and Dynamics II 23-Jun 0900 hrs Travertine

142-MST-6 Shadow Mode Assessment using Realistic Technologies for National Airspace System (SMART NAS) Test Bed Development (Invited)

23-Jun 1400 hrs Travertine

177-MST-7 Flight Simulation 24-Jun 0900 hrs Travertine

178-MST-8 Computational Methods for Fluid Dynamics and Heat Transfer Simulations 24-Jun 0900 hrs Wyeth

214-MST-9 Airframe Damage and Health Monitoring 24-Jun 1400 hrs Travertine

215-MST-10 Sensor and Communications Systems 24-Jun 1400 hrs Wyeth

253-MST-11 Aircraft Systems Design, Verification and Validation 25-Jun 0900 hrs Travertine

285-MST-12 Propulsion Systems 25-Jun 1400 hrs Travertine



Plasmadynamics and Lasers 33-PDL-1/FD-5 Plasma Aerodynamics & Flow Control I 22-Jun 0900 hrs Monet Ballroom

60-FD-6/PDL-2 Plasma Aerodynamics & Flow Control II 22-Jun 1400 hrs Govenors Lecture Hall

67-PDL-3 Plasma Computational Methods I 22-Jun 1400 hrs Monet Ballroom

107-PDL-4 Plasma Assisted Combustion 23-Jun 0900 hrs Miro

143-PDL-6 Plasma Diagnostics I 23-Jun 1400 hrs Miro

144-PDL-7 Plasma Aerodynamics & Flow Control III 23-Jun 1400 hrs Monet Ballroom

180-PDL-8/APA-20 Plasma Aerodynamics & Flow Control IV 24-Jun 0900 hrs Stemmons C

181-PDL-9/TP-8 Plasma Diagnostics II 24-Jun 0900 hrs Miro

216-TP-10/PDL-10 Plasma Computational Methods II 24-Jun 1400 hrs Miro

255-PDL-12 Aero-Optics Plasma Diagnostics 25-Jun 0900 hrs Miro

286-PDL-13 Plasma Aerodynamics & Flow Control V 25-Jun 1400 hrs Miro

Thermophysics34-TP-1 Ablation I 22-Jun 0900 hrs Rosetta

35-TP-2 Heat Transfer I 22-Jun 0900 hrs Steuben

68-TP-3 Ablation II 22-Jun 1400 hrs Rosetta

69-TP-4 Aerothermodynamics I 22-Jun 1400 hrs Steuben

108-TP-5 Plasma and Arc Jet Testing, Diagnostics and Computational Methods 23-Jun 0900 hrs Rosetta

121-AMT-8/FD-14/TP-6/GT-8


145-TP-7 Heat Transfer II 23-Jun 1400 hrs Rosetta

181-PDL-9/TP-8 Plasma Diagnostics II 24-Jun 0900 hrs Miro

182-TP-9 Aerothermodynamics II 24-Jun 0900 hrs Rosetta

216-TP-10/PDL-10 Plasma Computational Methods II 24-Jun 1400 hrs Miro

217-TP-11 Aerothermodynamics III 24-Jun 1400 hrs Rosetta

256-TP-12 Detailed Molecular Process Modeling 25-Jun 0900 hrs Rosetta

288-TP-13 DSMC 25-Jun 1400 hrs Rosetta

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-1Ai

rfram

e Nois

e IFle

ur-d

e-lis

ACh

aired

by: D

. LOC

KARD

, NAS

A-Lan

gley R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-2

200

Aero

acou

stic a

nd A

erod

ynam

ic Pe

rform

ance

s of a

n Ae

rofo

il Su

bjecte

d to S

inuso

idal L

eadin

g Ed

ges

T. Ch

ong,

S. S

iddiqi

, Brun

el Un

iversi

ty,

Uxbri

dge,

Unite

d King

dom

0930

hrs

AIAA-2

015-2

201

Aero

dyna

mic a

nd A

eroa

cous

tic

Perfo

rman

ce of

Serra

ted A

irfoil

sX.

Liu,

M. Az

arpey

vand

, R. T

heun

issen

, Un

iversi

ty of

Brist

ol, B

ristol

, Unit

ed

Kingd

om

1000

hrs

AIAA-2

015-2

202

Broa

dban

d nois

e red

uctio

n th

roug

h lea

ding e

dge s

erra

tions

on re

alisti

c ae

rofo

ilsC.

Paruc

huri,

N. S

ubram

anian

, P.

Jose

ph, C

. Van

derw

el, J.

Kim,

B.

Gana

pathi

subra

mani,

Univ

ersity

of

South

ampto

n, So

utham

pton,

Unite

d Kin

gdom

1030

hrs

AIAA-2

015-2

203

Airfo

il nois

e pre

dictio

n fro

m 2D

3C

PIV d

ata

L. de

San

tana,

Catho

lic Un

iversi

ty of

Leuv

en, L

euve

n, Be

lgium

; C. S

chram

, vo

n Kárm

án In

stitut

e for

Fluid

Dyna

mics,

Rh

ode-S

aint-G

enès

e, Be

lgium

; W. D

esme

t, Ca

tholic

Unive

rsity

of Le

uven

, Leu

ven,

Belgi

um

1100

hrs

AIAA-2

015-2

204

Noise

gene

ratio

n by

turb

ulenc

e int

erac

ting w

ith an

aero

foil w

ith a

serra

ted le

ading

edge

J. Ma

thews

, N. P

eake

, Univ

ersity

of

Camb

ridge

, Cam

bridg

e, Un

ited K

ingdo

m

1130

hrs

AIAA-2

015-2

205

Deta

iled e

xper

imen

tal in

vesti

gatio

n of

the a

eroa

cous

tic fi

eld ar

ound

a Co

ntro

lled-

Diffu

sion

airfo

ilT.

Pado

is, P.

Laffa

y, A.

Idier,

S. M

oreau

, Un

iversi

ty of

Sherb

rooke

, She

rbroo

ke,

Cana

da

1200

hrs

AIAA-2

015-2

206

2D h

igh-li

ft air

foil n

oise

meas

urem

ents

in an

aero

dyna

mic

wind

tunn

elV.

Fleury

, J. B

ulte,

R. Da

vy, E

. Man

oha,

ONER

A, Ch

âtillo

n, Fra

nce;

M. Po

tt-Po

llens

ke, G

erman

Aeros

pace

Cente

r (D

LR),

Brau

nsch

weig,

Germ

any

Mond

ay, 2

2 Ju

ne 2

015

4-AA

-2Je

t Nois

e Pre

dictio

n I

Fleur

-de-

lis B

Chair

ed by

: P. M

ORRIS

, Pen

nsylv

ania

State

Univ

ersity

0900

hrs

AIAA-2

015-2

207

Asse

ssmen

t of J

et-pla

te In

terac

tion

Noise

Usin

g the

Latti

ce B

oltzm

ann

Meth

odF.

da S

ilva,

C. De

scham

ps, A

. da S

ilva,

Fede

ral U

nivers

ity of

San

ta Ca

tarina

, Flo

rianó

polis,

Braz

il; L.

Simõe

s, Em

braer,

Sã

o Jos

é dos

Camp

os, B

razil

0930

hrs

AIAA-2

015-2

208

Insta

llatio

n no

ise of

a tu

rbof

an je

t en

gine u

nder

an ai

rfoil

G. B

riche

t, M.

Koen

ig, S

afran

Grou

p, Mo

issy-C

ramay

el, Fr

ance

; C. B

ailly,

École

Ce

ntrale

de Ly

on, E

cully,

Fran

ce

1000

hrs

AIAA-2

015-2

209

Larg

e-ed

dy si

mulat

ion of

su

perso

nic pl

anar

jets

impin

ging

on a

flat p

late a

t an

angle

of 6

0 to

90

degr

ees

R. Go

jon, C

. Bog

ey, O

. Mars

den,

École

Ce

ntrale

de Ly

on, E

cully,

Fran

ce

1030

hrs

AIAA-2

015-2

210

Larg

e-ed

dy si

mulat

ion of

un

dere

xpan

ded r

ound

jets

impin

ging o

n a fl

at pl

ate 4

to 9

ra

dii do

wnstr

eam

from

the n

ozzle

R. Go

jon, C

. Bog

ey, O

. Mars

den,

École

Ce

ntrale

de Ly

on, E

cully,

Fran

ce

1100

hrs

AIAA-2

015-2

211

Noise

Char

acter

istics

of a

Four

-Jet

Impin

geme

nt D

evice

Insid

e a

Broa

dban

d Eng

ine N

oise S

imula

tor

C. Br

ehm,

J. H

ousm

an, C

. Kiris

, NAS

A Am

es Re

searc

h Cen

ter, M

offett

Field

, CA;

F. Hu

tches

on, N

ASA L

angle

y Res

earch

Ce

nter, H

ampto

n, VA

1130

hrs

AIAA-2

015-2

212

Simula

tion

and s

tabil

ity an

alysis

of

a su

perso

nic im

pingin

g jet

at

vary

ing n

ozzle

-to-w

all di

stanc

esN.

Hild

ebran

d, J.

Nicho

ls, U

nivers

ity of

Mi

nnes

ota, T

win C

ities,

Minn

eapo

lis, M

N

1200

hrs

AIAA-2

015-2

213

Hybr

id ap

proa

ch fo

r the

pred

iction

of

jet n

oise i

nter

actio

n an

d ins

talla

tion

effe

ctsY.

Yang

, Y. S

un, C

. Brea

rd, Co

mmerc

ial

Aircra

ft Co

rporat

ion of

China

, Ltd.

(C

OMAC

), Sh

angh

ai, Ch

ina

41

Mond

ay, 2

2 Ju

ne 2

015

5-AA

-3Je

t Nois

e Mod

eling

IIn

vern

ess

Chair

ed by

: C. B

OGEY

, Eco

le Ce

ntrale

de Ly

on09

00 hr

sAIA

A-201

5-221

4Re

al-tim

e mod

elling

of

wave

pack

ets in

turb

ulent

jets

K. Sa

saki,

Tech

nolog

ical In

stitut

e of

Aeron

autic

s (ITA

), Sã

o Jos

é dos

Camp

os,

Braz

il; S.

Pian

tanida

, Nati

onal

Cente

r for

Scie

ntific

Rese

arch (

CNRS

), Po

itiers,

Fra

nce;

A. Ca

valie

ri, Te

chno

logica

l Ins

titute

of Ae

ronau

tics (

ITA),

São J

osé

dos C

ampo

s, Br

azil;

P. Jo

rdan,

Natio

nal

Cente

r for

Scien

tific R

esea

rch (C

NRS)

, Po

itiers,

Fran

ce

0930

hrs

AIAA-2

015-2

215

Auto

matic

Opt

imize

r vs H

uman

Op

timize

r for

Low-

Orde

r Jet

Noise

Mo

dellin

gY.

Korol

ev, S

. Kara

baso

v, V.

Torop

ov,

Quee

n Mary

Univ

ersity

of Lo

ndon

, Lon

don,

Unite

d King

dom

1000

hrs

AIAA-2

015-2

216

The p

redic

tion

of th

e rad

iated

pr

essu

re sp

ectru

m pr

oduc

ed by

jet

-wing

inter

actio

nJ.

Vera,

J. La

wren

ce, R

. Self

, M. K

ingan

, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom

1030

hrs

AIAA-2

015-2

217

Stoch

astic

and n

onlin

ear f

orcin

g of

wave

pack

ets in

a Ma

ch 0

.9 je

tA.

Town

e, T.

Colon

ius, C

alifor

nia In

stitut

e of

Tech

nolog

y, Pa

sade

na, C

A; P.

Jorda

n, Na

tiona

l Cen

ter fo

r Scie

ntific

Rese

arch

(CNR

S), P

oitier

s, Fra

nce;

A. Ca

valie

ri, Te

chno

logica

l Insti

tute o

f Aero

nauti

cs (IT

A), S

ão Jo

sé do

s Cam

pos,

Braz

il; G.

Br

ès, C

asca

de Te

chno

logies

, Inc

., Pa

lo Alt

o, CA

1100

hrs

AIAA-2

015-2

218

Sens

itivity

of w

avep

acke

ts in

jets t

o no

n-line

ar ef

fects:

the r

ole of

the

critic

al lay

erG.

Tissot

, Tech

nolog

ical In

stitute

of Ae

ronau

tics

(ITA)

, São

José

dos C

ampo

s, Bra

zil; M

. Zh

ang,

Natio

nal C

enter

for S

cienti

fic Re

search

(C

NRS)

, Poit

iers,

France

; F. La

jús, A

. Cav

alieri,

Techn

ologic

al Ins

titute

of Ae

ronau

tics (I

TA),

São J

osé do

s Cam

pos,

Brazil;

P. Jor

dan,

Natio

nal C

enter

for S

cienti

fic Re

search

(C

NRS)

, Poit

iers,

France

; T. C

oloniu

s, Ca

liforni

a Ins

titute

of Tec

hnolo

gy, Pa

saden

a, CA

1130

hrs

AIAA-2

015-2

219

Sens

itivity

analy

sis fo

r sub

sonic

jet

using

adjoi

nt of

non

loca

l sta

bility

eq

uatio

nsC.

Airiau

, T. A

nsald

i, Univ

ersity

of To

ulous

e, To

ulous

e, Fra

nce

1200

hrs

AIAA-2

015-2

220

A Co

ntro

l Fra

mewo

rk fo

r Wa

vepa

ckets

in Tu

rbule

nt Je

ts Us

ing Ti

me-D

omain

Tran

sfer

Func

tions

F. Sil

vestr

e, M.

Capre

cci, A

. Cav

alieri

, Te

chno

logica

l Insti

tute o

f Aero

nauti

cs (IT

A), S

ão Jo

sé do

s Cam

pos,

Braz

il; P.

Jorda

n, Éc

ole N

ation

ale S

upéri

eure

des

Mine

s de S

aint-É

tienn

e, Po

itiers,

Fran

ce

Mond

ay, 2

2 Ju

ne 2

015

6-AA

-4CA

A Nu

meric

al Te

chniq

ues I

Laliq

ueCh

aired

by: W

. SCH

ROED

ER, R

WTH

AACH

EN, I

nstitu

te of

Aerod

ynam

ics09

00 hr

sAIA

A-201

5-222

1Ex

perim

enta

l Vali

datio

n of

Ae

ro-V

ibro-

Acou

stic A

nalys

is of

Pr

oduc

tion

Vehic

les (I

nvite

d)S.

Caro,

CD-ad

apco

, Lyo

n, Fra

nce

0930

hrs

AIAA-2

015-2

222

CAA

Study

of A

irfoil

Bro

adba

nd

Inter

actio

n No

ise U

sing S

toch

astic

Tu

rbule

nt Vo

rticit

y Sou

rces

T. Ha

inaut,

G. G

abard

, V. C

lair, U

nivers

ity

of So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1000

hrs

AIAA-2

015-2

223

CABA

RET G

PU So

lver f

or Fa

st-Tu

rn-

Arou

nd Fl

ow an

d Nois

e Calc

ulatio

nsA.

Marke

steijn

, V. S

emile

tov, S

. Kara

baso

v, Qu

een M

ary U

nivers

ity of

Lond

on, L

ondo

n, Un

ited K

ingdo

m

1030

hrs

AIAA-2

015-2

224

Asse

ssmen

t of F

lap Si

de-Ed

ge Fe

nce

Noise

usin

g SNG

R Me

thod

H. Ya

o, L.

David

son, C

halm

ers Un

iversit

y of

Techn

ology,

Göteb

org, S

wede

n; S.

Peng

, Sw

edish

Defen

se Re

search

Agen

cy (F

OI),

Stockh

olm, S

wede

n; L.

Erikss

on, C

halm

ers

Unive

rsity o

f Tech

nolog

y, Gö

teborg

, Swe

den;

M. Ba

rbarin

o, F. C

apizz

ano,

Italian

Aeros

pace

Re

search

Cente

r (CIR

A), C

apua

, Italy

; et a

l.

1100

hrs

AIAA-2

015-2

225

Verifi

catio

n of

a Vis

cous

Co

mput

ation

al Ae

roac

ousti

cs Co

de

using

Exter

nal V

erifi

catio

n An

alysis

D. In

graha

m, D

. Hixo

n, Un

iversi

ty of

Toled

o, To

ledo,

OH

1130

hrs

AIAA-2

015-2

226

Acou

stic l

oads

pred

iction

for a

co

mmer

cial t

rans

port

aircra

ft un

der

grou

nd an

d fligh

t con

dition

sY.

Sun,

Y. Ya

ng, C

. Brea

rd, Co

mmerc

ial

Aircra

ft Co

rporat

ion of

China

, Ltd.

(C

OMAC

), Sh

angh

ai, Ch

ina

Mond

ay, 2

2 Ju

ne 2

015

7-AA

-5Du

ct Ac

ousti

cs I

Obeli

sk A

Chair

ed by

: W. E

VERS

MAN,

Miss

ouri U

nivers

ity of

Scie

nce a

nd Te

chno

logy

0900

hrs

AIAA-2

015-2

227

Effe

ct of

visco

sity o

n im

peda

nce

educ

tion

and v

alida

tion

L. Zh

ou, H

. Bod

en, R

oyal

Institu

te of

Tech

nolog

y (KT

H), S

tockh

olm, S

wede

n

0930

hrs

AIAA-2

015-2

228

Impe

danc

e Edu

ction

in So

und F

ields

wi

th P

eriph

erall

y Var

ying L

iners

and F

lowW.

Wats

on, M

. Jon

es, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

1000

hrs

AIAA-2

015-2

229

The E

ffecti

ve Im

peda

nce o

f a

Finite

-Thick

ness

Visco

ther

mal

Boun

dary

Laye

r Ove

r an

Acou

stic

Lining

D. Kh

amis,

E. B

ramble

y, Un

iversi

ty of

Camb

ridge

, Cam

bridg

e, Un

ited K

ingdo

m

1030

hrs

AIAA-2

015-2

230

Acou

stic L

iner D

rag:

A Pa

rame

tric

Study

of Co

nven

tiona

l Co

nfigu

ratio

nsB.

How

erton

, M. J

ones

, NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA

1100

hrs

AIAA-2

015-2

231

Expe

rimen

tal S

tudy

of th

e Me

chan

isms o

f Sou

nd G

ener

ation

Du

e to a

n In

-duc

t Orifi

ce P

late

F. Ta

o, X.

Zhan

g, P.

Jose

ph, O

. Stal

nov,

Unive

rsity

of So

utham

pton,

South

ampto

n, Un

ited K

ingdo

m; M

. Sier

cke,

H. S

chee

l, Air

bus,

Hamb

urg, G

erman

y

1130

hrs

AIAA-2

015-2

232

Duct

spinn

ing m

ode’s

parti

cle

veloc

ity im

aging

on a

cross

plane

ou

tside

the d

uct

W. Yu

, Q. W

ei, X

. Hua

ng, P

eking

Un

iversi

ty, B

eijing

, Chin

a

1200

hrs

AIAA-2

015-2

233

In-d

uct B

eamf

ormi

ng N

oise

Sour

ce Es

timat

ion M

ode D

etecti

on

Unive

rsity

of Sã

o Pau

lo Fa

n Ri

gL.

Calda

s, L.

Bacca

la, R.

Cuen

ca,

Unive

rsity

of Sã

o Pau

lo, S

ão Pa

ulo,

Braz

il; R.

Queir

oz, E

mbrae

r, São

José

dos

Camp

os, B

razil

42

Mond

ay, 2

2 Ju

ne 2

015

8-AF

M-1

Aircr

aft F

light

Dyn

amics

, Con

trol, H

andli

ng Q

ualiti

es an

d Per

form

ance

IPlu

m Bl

osso

m A

Chair

ed by

: E. G

ILLES

PIE, U

nited

Spa

ce Al

lianc

e09

00 hr

sAIA

A-201

5-223

4Be

nefit

s of F

orma

tion F

light

of

Exten

ded D

urati

on Co

nside

ring F

uel

Burn

W. O

kolo,

A. Do

gan,

Unive

rsity o

f Tex

as,

Arling

ton, A

rlingto

n, TX

; W. B

lake,

Air Fo

rce

Resea

rch La

borat

ory, W

right-

Patte

rson

AFB,

OH

0930

hrs

AIAA-2

015-2

235

Auto

matic

Stall

/Spin

Dete

ction

in

Fixed

-Wing

Airc

raft

R. Bu

nge,

F. Mu

nera

Savin

o, I.

Kroo,

Stan

ford U

nivers

ity, S

tanfor

d, CA

1000

hrs

AIAA-2

015-2

236

Extra

cting

Airp

lane P

erfo

rman

ce

for a

Fata

l Acci

dent

in th

e Abs

ence

of

a Fli

ght D

ata R

ecor

der

T. Bu

rtch,

Natio

nal T

ransp

ortati

on S

afety

Board

, Was

hingto

n, DC

1030

hrs

AIAA-2

015-2

237

Valid

ation

of a

Mode

l Bas

ed St

ructu

ral

Load

s Mon

itorin

g Sys

tem us

ing th

e Fli

ght T

est Ai

rcraft

UW-

9 Spr

intM.

Mon

tel, F.

Thiele

cke, H

ambu

rg Un

iversit

y of

Techn

ology,

Hamb

urg, G

erman

y

1100

hrs

AIAA-2

015-2

238

Roll p

erfo

rman

ce as

sessm

ent o

f a

light

aircr

aft:

fligh

t tes

ts an

d fligh

t sim

ulatio

nF.

Nicolo

si, A.

De M

arco,

V. Sa

betta

, P.

Della

Vecch

ia, U

nivers

ity of

Nap

les

“Fed

erico

II”, N

aples

, Ital

y

Mond

ay, 2

2 Ju

ne 2

015

9-AF

M-2

Aero

serv

oelas

tic (A

SE) M

odeli

ngPlu

m Bl

osso

m B

Chair

ed by

: T. A

LEXE

EV, U

nivers

ity of

Califo

rnia D

avis

and F

. PRIO

LO, M

illenn

ium En

ginee

ring a

nd In

tegrat

ion Co

mpan

y09

00 hr

sAIA

A-201

5-223

9Co

ntro

l of a

Non

linea

r Wing

Secti

on

using

Fly-

by-Fe

el Se

nsing

V. Su

ryaku

mar, Y

. Bab

bar, T

. Strg

anac

, Te

xas A

&M U

nivers

ity, C

olleg

e Stat

ion, T

X;

A. Ma

ngala

m, Ta

o of S

ystem

s Inte

gratio

n, Inc

., Ha

mpton

, VA

0930

hrs

AIAA-2

015-2

240

Aero

elasti

c Sta

te-sp

ace M

odel

Deve

lopme

nt B

ased

on Fr

eque

ncy

Resp

onse

Iden

tifica

tion

and

Integ

ratio

n wi

th Fl

ight D

ynam

icsT.

Buttin

i, F. M

oreira

, Emb

raer, S

ão Jo

sé

dos C

ampo

s, Br

azil;

F. Sil

vestr

e, R.

A. da

Sil

va, T

echn

ologic

al Ins

titute

of Ae

ronau

tics

(ITA)

, São

José

dos C

ampo

s, Br

azil

1000

hrs

AIAA-2

015-2

241

Optim

al Siz

ing an

d Con

figur

ation

s of

the C

ontro

l Sur

face

s for

Acti

ve

Aero

elasti

c Con

trol

R. Br

own,

K. Sin

gh, M

iami U

nivers

ity,

Oxfor

d, OH

1030

hrs

AIAA-2

015-2

242

Aero

elasti

c Tail

oring

for

Maxim

izing

Sailp

lane A

vera

ge

Cros

s-Cou

ntry

Spee

dC.

Lupp

, C. C

esnik

, Univ

ersity

of M

ichiga

n, An

n Arbo

r, Ann

Arbo

r, MI

1100

hrs

AIAA-2

015-2

243

Adap

tive F

eedf

orwa

rd Co

ntro

l De

sign

for G

ust L

oads

Alle

viatio

n of

Hi

ghly

Flexib

le Ai

rcraf

tY.

Wang

, F. L

i, Chin

a Aca

demy

of

Aeros

pace

Aerod

ynam

ics, B

eijing

, Chin

a; A.

Da Ro

nch,

Unive

rsity

of So

utham

pton,

South

ampto

n, Un

ited K

ingdo

m

1130

hrs

AIAA-2

015-2

244

Delta

Ada

ptive

Flex

ible M

otion

Co

ntro

l for

the X

-56A

Airc

raft

K. Ha

shem

i, Univ

ersity

of Te

xas,

Austi

n, Au

stin,

TX; C

. Pak

, NAS

A Arm

stron

g Flig

ht Re

searc

h Cen

ter, E

dward

s, CA

; M. A

kella

, Un

iversi

ty of

Texa

s, Au

stin,

Austi

n, TX

1200

hrs

AIAA-2

015-2

245

Feed

back

Line

ariza

tion

base

d Co

ntro

l of A

eroe

lastic

Syste

ms

repr

esen

ted in

Mod

al Co

ordin

ates

H. S

hukla

, M. P

atil, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA

Mond

ay, 2

2 Ju

ne 2

015

10-A

MT-1

/GT-1

Hap A

rnold

’s Ne

w Ho

rizon

: The

Futu

re R

ole of

Gro

und T

est i

n Hi

gh Sp

eed S

ystem

Dev

elopm

ent

Obeli

sk B

Chair

ed by

: J. S

CHMI

SSEU

R and

G. L

ISTON

0900

hrs

Oral

Prese

ntatio

nEn

vision

ing th

e Fut

ure o

f the

T&E

Enter

prise

M. Le

wis,

IDA,

Wash

ington

, DC

0930

hrs

Oral

Prese

ntatio

nCh

allen

ges a

nd O

ppor

tunit

ies in

the

Deve

lopme

nt of

T&E C

apab

ilities

J. Sc

hmiss

eur, U

nivers

ity of

Tenn

esse

e, Tu

llaho

ma, T

ullah

oma,

TN

1000

hrs

Oral

Prese

ntatio

nIn

trodu

ction

to th

e AFR

L High

-Sp

eed E

xper

imen

tatio

n Br

anch

G. Li

ston,

Air Fo

rce Re

searc

h Lab

orator

y, Cle

velan

d, OH

1030

hrs

Oral

Prese

ntatio

nDe

velop

ment

of La

rge-

Scale

Quie

t Tu

nnels

Supp

ortin

g T&E

T. Ju

liano

, Notr

e Dam

e Univ

ersity

, Notr

e Da

me, I

N

1100

hrs

Pane

l Disc

usssi

onTh

e Fut

ure o

f Gro

und T

est w

ithin

T&E

J. Sc

hmiss

eur, U

nivers

ity of

Tenn

esse

e, Tu

llaho

ma, T

ullah

oma,

TN

Mond

ay, 2

2 Ju

ne 2

015

11-A

MT-2

/GT-2

Line o

f Sigh

t and

Den

sity M

easu

reme

ntEd

elweis

sCh

aired

by: S

. O’B

YRNE

, The

Univ

ersity

of N

ew S

outh

Wales

0900

hrs

AIAA-2

015-2

246

Analy

sis of

Focu

sed L

aser

Di

ffere

ntial

Inter

fero

metry

B. S

chmi

dt, J.

She

pherd

, Cali

fornia

Ins

titute

of Te

chno

logy,

Pasa

dena

, CA

0930

hrs

AIAA-2

015-2

247

Simult

aneo

us M

easu

reme

nts

of D

ensit

y Fiel

d and

Wav

efro

nt

Disto

rtion

s in

High

Spee

d Jet

Flows

J. Ge

orge,

T. Je

nkins

, C. H

ess,

J. Tro

linge

r, Me

troLa

ser, I

nc.,

Lagu

na H

ills, C

A

1000

hrs

AIAA-2

015-2

248

Optic

al Me

asur

emen

ts of

Veloc

ity,

Dens

ity, a

nd M

ass F

lux in

a Su

perso

nic W

ind Tu

nnel

D. Pl

emmo

ns, N

. Galy

en, A

erosp

ace

Testi

ng Al

lianc

e, Arn

old AF

B, TN

1030

hrs

AIAA-2

015-2

249

A Tim

e-Re

solve

d Tem

pera

ture

Me

asur

emen

t Sys

tem fo

r Fre

e-Pis

ton

Shoc

k Tu

nnels

Y. Kri

shna

, S. S

heeh

e, S.

O’B

yrne,

Unive

rsity

of Ne

w So

uth W

ales,

Canb

erra,

Austr

alia

43

Mond

ay, 2

2 Ju

ne 2

015

12-A

PA-1

Aero

dyna

mic-S

tructu

re D

ynam

ics In

terac

tion

Stemm

ons C

Chair

ed by

: J. A

ZEVE

DO an

d C. P

ASILI

AO, A

FRL/

RWW

V09

00 hr

sAIA

A-201

5-225

0Ae

rody

nami

c Dam

ping a

nd

Stiffn

ess D

eterm

inatio

n fo

r Airc

raft

Wing

Flut

ter Sp

eed A

nalys

isK.

Boo,

S. M

anso

r, A. A

bdul-

Latif,

Un

iversi

ty of

Tech

nolog

y, Jo

hor B

ahru,

Ma

laysia

0930

hrs

AIAA-2

015-2

251

Expe

rimen

tal I

nves

tigat

ion of

the

Aero

elasti

c Beh

avior

a NA

CA00

18

Cybe

r-Phy

sical

Flexib

leWing

C. Fa

gley,

J. Se

idel, T

. McLa

ughli

n, U.

S.

Air Fo

rce Ac

adem

y, Co

lorad

o Spri

ngs,

CO

1000

hrs

AIAA-2

015-2

252

Spec

tral F

ormu

lation

-Bas

ed FS

I and

Co

upled

Sens

itivity

Ana

lysis

for

Dyan

mic A

eroe

lastic

Pro

blems

S. Yi,

Korea

Adva

nced I

nstitu

te of

Scien

ce an

d Tec

hnolo

gy, Da

ejeon

, Sou

th Ko

rea; R

. Pras

ad,

S. Ch

oi, D.

Im, V

irginia

Polyt

echnic

Instit

ute

and S

tate U

nivers

ity, Bl

acksbu

rg, VA

; D. L

ee,

Korea

Adva

nced I

nstitu

te of

Scien

ce an

d Tec

hnolo

gy, Da

ejeon

, Sou

th Ko

rea

1030

hrs

AIAA-2

015-2

253

Analy

zing t

he P

itch

Agilit

y of a

n Or

nitho

pter

Und

ergo

ing P

assiv

e Co

mplia

nt El

emen

t Ind

uced

Shap

e Ch

ange

Z. Ha

snain

, J. H

ubba

rd, U

nivers

ity of

Ma

rylan

d, Co

llege

Park,

Colle

ge Pa

rk, M

D;

A. W

issa,

Unive

rsity

of Illi

nois,

Urba

na-

Cham

paign

, Urba

na, I

L

Mond

ay, 2

2 Ju

ne 2

015

13-A

PA-2

Aero

dyna

mic D

esign

Meth

odolo

gies I

Carp

enter

Ball

room

Chair

ed by

: K. K

ARA,

Khali

fa Un

iversi

ty of

Scien

ce, T

echn

ology

& Re

searc

h and

J. M

URRA

Y, Sa

ndia

Natio

nal L

abora

tories

0900

hrs

AIAA-2

015-2

254

Deve

lopme

nt of

NOV

A Ai

rcraf

t Co

nfigu

ratio

ns fo

r Lar

ge En

gine

Integ

ratio

n Stu

dies

L. W

iart,

O. At

inault

, R. G

renon

, B. P

aluch

, D.

Hue

, ONE

RA, M

eudo

n, Fra

nce

0930

hrs

AIAA-2

015-2

255

Aircr

aft d

irecti

onal

stabil

ity

pred

iction

meth

od by

CFD

P. De

lla Ve

cchia,

F. N

icolos

i, D. C

ilibert

i, Un

iversi

ty of

Naple

s “Fe

deric

o II”,

Nap

les,

Italy

1000

hrs

AIAA-2

015-2

256

Desig

n of a

Mult

i-Stag

e Axia

l Tur

bine

withi

n the

scop

e of c

omple

te Sy

stem

Desig

n, Ma

nufac

turing

and O

pera

tion

of a n

ew Tu

rbine

Prop

ulsion

Simu

lator

(TP

S)A.

Krumm

e, Ge

rman

Aeros

pace

Cente

r (DL

R),

Göttin

gen,

Germ

any;

S. He

gen,

Germ

an-Du

tch

Wind

Tunn

els, M

arkne

sse, T

he N

etherl

ands;

R.

Nahu

is, Na

tiona

l Aero

space

Labo

ratory

(NLR

), Ma

rkness

e, Th

e Neth

erlan

ds

1030

hrs

AIAA-2

015-2

257

Fuse

lage A

erod

ynam

ic Pr

edict

ion

Meth

ods

F. Nic

olosi,

P. D

ella V

ecch

ia, D

. Cilib

erti, V

. Cu

sati,

L. Att

anas

io, U

nivers

ity of

Nap

les

“Fed

erico

II”, N

aples

, Ital

y

1100

hrs

AIAA-2

015-2

258

Inve

stiga

tion

on co

ntinu

ously

de

flecta

ble H

igh-Li

ft De

vices

for a

3D

High

-Lift

Confi

gura

tion

D. Fr

anke

, Germ

an Ae

rospa

ce Ce

nter

(DLR

), Br

auns

chwe

ig, G

erman

y

1130

hrs

AIAA-2

015-2

259

Nume

rical

study

of U

AS-S

4 Éh

ecat

l aer

odyn

amic

perfo

rman

ce

impr

ovem

ent o

btain

ed w

ith th

e use

of

a mo

rphin

g wing

appr

oach

S. O

liviu,

A. Ko

reans

chi, R

. Bote

z, Un

iversi

ty of

Québ

ec, M

ontré

al, Ca

nada

Mond

ay, 2

2 Ju

ne 2

015

14-A

PA-3

Spec

ial Se

ssion

: Low

Boo

m Ac

tivitie

s ISte

mmon

s ACh

aired

by: K

. WAIT

HE, G

ulfstr

eam

Aeros

pace

Corpo

ration

and L

. BAN

GERT

, NAS

A Lan

gley R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-2

260

Unde

r-Tra

ck CF

D-Ba

sed S

hape

Op

timiza

tion

for a

Low-

Boom

De

mons

trato

r Con

cept

M. W

intze

r, Ana

lytica

l Mec

hanic

s Asso

ciates

, Inc

., Ha

mpton

, VA;

I. Orda

z, NA

SA La

ngley

Re

searc

h Cen

ter, H

ampto

n, VA

0930

hrs

AIAA-2

015-2

261

Full-

Carp

et De

sign

of a

Low-

Boom

De

mons

trato

r Con

cept

I. Or

daz,

NASA

Lang

ley Re

searc

h Cen

ter,

Hamp

ton, V

A; M.

Wint

zer, A

nalyt

ical

Mech

anics

Asso

ciates

, Inc

., Ha

mpton

, VA

; S. R

allab

hand

i, Nati

onal

Institu

te of

Aeros

pace

, Ham

pton,

VA

1000

hrs

Oral

Prese

ntatio

nSo

nic B

oom

Varia

tion

of a

Wing

-Bo

dy-Ta

il-Na

celle

Confi

gura

tion

M. Pa

rk, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1030

hrs

AIAA-2

015-2

262

Nume

rical

Simula

tions

of Sh

ock/

Plume

Inter

actio

n Us

ing St

ructu

red

Over

set G

rids

J. Ho

usma

n, C.

Kiris,

NAS

A Ame

s Res

earch

Ce

nter, M

offett

Field

, CA

1100

hrs

AIAA-2

015-2

263

Cart3

D An

alysis

of P

lume a

nd

Shoc

k In

terac

tion

Effe

cts on

Sonic

Bo

omR.

Castn

er, N

ASA G

lenn R

esea

rch Ce

nter,

Cleve

land,

OH

44

Mond

ay, 2

2 Ju

ne 2

015

15-A

PA-4

Prop

eller

/Rot

orcra

ft/Wi

nd Tu

rbine

Aer

odyn

amics

ISte

mmon

s BCh

aired

by: M

. CAL

VERT

, U.S

. Arm

y AMR

DEC a

nd D

. O’B

RIEN,

US

Army R

DECO

M09

00 hr

sAIA

A-201

5-226

4Ex

perim

ental

Evalu

ation

of O

pen

Prop

eller

Aero

dyna

mic P

erfor

manc

e an

d Aero

-acou

stic B

ehav

iorC.

Wisni

ewski

, A. B

yerle

y, W.

Heise

r, U.S.

Air

Force

Acad

emy,

Color

ado S

pring

s, CO

; K.

Van T

reuren

, T. L

iller, B

aylor

Unive

rsity,

Waco,

TX

; N. W

isniew

ski, R

ose Hu

lman

Instit

ute of

Tec

hnolo

gy, Te

rre Ha

ute, IN

0930

hrs

AIAA-2

015-2

265

Slips

tream

Mea

sure

ment

s of S

mall-

Scale

Pro

pelle

rs at

Low

Reyn

olds

Numb

ers

R. De

ters,

G. An

anda

Krish

nan,

M. S

elig,

Unive

rsity

of Illi

nois,

Urba

na-Ch

ampa

ign,

Urba

na, I

L

1000

hrs

AIAA-2

015-2

266

The I

nflue

nce o

f Airf

oil Sh

ape,

Reyn

olds N

umbe

r and

Chor

d Le

ngth

on Sm

all P

rope

ller

Perfo

rman

ce an

d Nois

eC.

Wisn

iewsk

i, A. B

yerle

y, W.

Heis

er, U

.S.

Air Fo

rce Ac

adem

y, Co

lorad

o Spri

ngs,

CO;

K. Va

n Treu

ren, T

. Lille

r, Bay

lor U

nivers

ity,

Waco

, TX

1030

hrs

AIAA-2

015-2

267

Desig

ning S

mall P

rope

llers

for

Optim

um Ef

ficien

cy an

d Low

Nois

e Fo

otpr

intC.

Wisn

iewsk

i, A. B

yerle

y, W.

Heis

er, U

.S.

Air Fo

rce Ac

adem

y, Co

lorad

o Spri

ngs,

CO;

K. Va

n Treu

ren, T

. Lille

r, Bay

lor U

nivers

ity,

Waco

, TX

1100

hrs

AIAA-2

015-2

268

A Pa

rabo

lic M

ethod

for A

ccura

te an

d Effi

cient

Wind

Farm

Simu

lation

A. Mi

ttal, K

. Sree

nivas

, W. B

riley,

L. Ta

ylor,

Unive

rsity

of Te

nnes

see,

Chatt

anoo

ga,

Chatt

anoo

ga, T

N

1130

hrs

AIAA-2

015-2

269

Blad

e Res

olved

Simu

lation

for a

Wi

nd Fa

rmW.

Has

san,

K. Sr

eeniv

as, A

. Mitta

l, L.

Taylo

r, L. H

ereth,

Univ

ersity

of Te

nnes

see,

Chatt

anoo

ga, C

hatta

noog

a, TN

Mond

ay, 2

2 Ju

ne 2

015

16-A

TIO-1

Term

inal &

Surfa

ce O

pera

tions

IMa

nche

ster

Chair

ed by

: S. C

AMPB

ELL,

MIT L

incoln

Labo

ratory

0900

hrs

AIAA-2

015-2

270

A Rob

ust a

nd Pr

actic

al De

cision

Su

ppor

t Too

l for I

ntegr

ated

Arriv

al-De

partu

re-Su

rface

Traffi

c Ma

nage

ment

A. Sa

raf, V

. Felip

e, Sa

ab Se

nsis C

orpora

tion,

Camp

bell,

CA; B

. Saw

hill, N

extGe

n Ae

roscie

nces L

LC, W

illiams

burg,

VA

0930

hrs

AIAA-2

015-2

271

Iden

tifica

tion

of Lo

cal a

nd

Prop

agat

ed Q

ueuin

g Effe

cts at

Ma

jor A

irpor

tsH.

Idris

, Eng

ility C

orpora

tion,

Biller

ica, M

A

1000

hrs

AIAA-2

015-2

272

Taxi

Time P

redic

tion

at Ch

arlot

te Ai

rpor

t Usin

g Fas

t-Tim

e Sim

ulatio

n an

d Mac

hine L

earn

ing Te

chniq

ues

H. Le

e, W.

Mali

k, Un

iversi

ty of

Califo

rnia,

Santa

Cruz

, Moff

ett Fi

eld, C

A; B.

Zhan

g, B.

Nag

arajan

, Ame

rican

Airlin

es, F

ort

Worth

, TX;

Y. Ju

ng, N

ASA A

mes R

esea

rch

Cente

r, Moff

ett Fi

eld, C

A

1030

hrs

AIAA-2

015-2

273

A Sto

chas

tic Sc

hedu

ler fo

r In

tegra

ted A

rriva

l, Dep

artu

re, a

nd

Surfa

ce O

pera

tions

in Lo

s Ang

eles

M. X

ue, U

nivers

ity of

Califo

rnia,

Santa

Cru

z, Mo

ffett

Field,

CA; S

. Zeli

nski,

NAS

A Am

es Re

searc

h Cen

ter, M

offett

Field

, CA

1100

hrs

AIAA-2

015-2

274

Optim

izatio

n of

Airp

ort S

urfa

ce

Oper

ation

s Und

er U

ncer

taint

yC.

Bosso

n, D.

Sun

, Purd

ue U

nivers

ity, W

est

Lafay

ette,

IN

Mond

ay, 2

2 Ju

ne 2

015

17-A

TIO-2

Sepa

ratio

n As

sura

nce

Ming

Chair

ed by

: M. W

ILCOX

EN, U

.S. A

ir Forc

e09

00 hr

sAIA

A-201

5-227

5Co

nflict

Dete

ction

Perfo

rman

ce

Analy

sis fo

r Fun

ction

Alloc

ation

Usin

g Tim

e-Shif

ted Re

cord

ed Tr

affic D

ataN.

Guerr

eiro,

J. Ma

ddalo

n, T.

Lewis,

G. Ha

gen,

NASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA

0930

hrs

AIAA-2

015-2

276

Strat

egic

time-

base

d mete

ring t

hat

assu

res s

epar

ation

for i

nteg

rated

op

erat

ions i

n a t

ermi

nal a

irspa

ceA.

Sado

vsky

, M. J

astrz

ebsk

i, NAS

A Ame

s Re

searc

h Cen

ter, M

offett

Field

, CA

1000

hrs

AIAA-2

015-2

277

Confl

ict A

lerts

for A

ircra

ft Co

nduc

ting V

isual

Appr

oach

esH.

Tang

, NAS

A Ame

s Res

earch

Cente

r, Mo

ffett

Field,

CA

Mond

ay, 2

2 Ju

ne 2

015

18-A

TIO-3

Trajec

tory

Opt

imiza

tion

Milan

Chair

ed by

: H. A

RNES

ON09

00 hr

sAIA

A-201

5-227

8Th

e Stri

ng St

abilit

y of a

Traje

ctory

-Ba

sed I

nter

val M

anag

emen

t Al

gorit

hm in

the M

idter

m Ai

rspac

eK.

Swier

inga,

NASA

Lang

ley Re

searc

h Ce

nter, H

ampto

n, VA

0930

hrs

AIAA-2

015-2

279

Comp

utat

ional

Appr

oach

es to

Sim

ulatio

n an

d Opt

imiza

tion

of

Glob

al Ai

rcraf

t Tra

jecto

ries

H. N

g, Un

iversi

ty of

Califo

rnia,

Santa

Cruz

, Mo

ffett

Field,

CA; B

. Srid

har, N

ASA A

mes

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1000

hrs

AIAA-2

015-2

280

Bran

ch &

Bou

nd-B

ased

Algo

rithm

fo

r Airc

raft

VNAV

Pro

file R

efer

ence

Tra

jecto

ry O

ptim

izatio

nA.

Murrie

ta Me

ndoz

a, B.

Beu

ze, L

. Te

rnisie

n, R.

Botez

, Univ

ersity

of Q

uébe

c, Mo

ntréa

l, Can

ada

1030

hrs

AIAA-2

015-2

281

Aircr

aft T

rajec

torie

s Opt

imiza

tion

By G

eneti

c Algo

rithm

s To R

educ

e Fli

ght C

ost U

sing A

Dyn

amic

Weat

her M

odel

R. Fé

lix Pa

trón,

M. S

chind

ler, R

. Bote

z, Un

iversi

ty of

Québ

ec, M

ontré

al, Ca

nada

1100

hrs

AIAA-2

015-2

282

Trajec

tory

optim

izatio

n alg

orith

m fo

r a co

nsta

nt al

titud

e cru

ise fl

ight

with

a re

quire

d tim

e of a

rriva

l co

nstra

intA.

Liv, R

. Dan

cila, R

. Bote

z, Un

iversi

ty of

Québ

ec, M

ontré

al, Ca

nada

45

Mond

ay, 2

2 Ju

ne 2

015

19-A

TIO-4

09

00 -

1100

hrs

Trans

form

ation

al Fli

ght -

Rap

id Co

ncep

t to F

light

Metro

polita

n Ba

llroo

m

Mode

rator:

Willi

am Fr

ederi

cks,

NASA

Lang

ley Re

searc

h Cen

ter

Pan

elists

:Ne

al Wi

llfor

dTe

xtron

Aviat

ionMa

rk P

age

Dzyn

e Tec

hnolo

gies

JoeB

en B

evirt

Joby

Aviat

ionSta

rr Gi

nnNA

SA Ar

mstro

ng Re

searc

h Cen

ter

Mond

ay, 2

2 Ju

ne 2

015

20-C

ASE-1

09

00 -

1200

hrs

Acad

emic

Roun

dtab

leBa

tik

Expa

nding

on th

e the

me fr

om S

unda

y, thi

s ses

sion i

s the

seco

nd da

y acti

vity o

f the

201

5 CA

SE Ac

adem

ic Wo

rksho

p. It

will o

ffer r

apid-

fire di

scussi

ons o

f curr

ent r

esea

rch ef

forts

in sy

stems

know

ledge

and c

ompe

tency.

F

acilit

ators:

Fran

z-Jos

ef K

ahlen

, Ph.

D.As

socia

te Pro

fesso

r, Dep

artme

nt of

Mech

anica

l Eng

ineeri

ngUn

iversi

ty of

Cape

Town

, Cap

e Tow

n, So

uth Af

rica

Shan

non

Flume

rfelt,

Ph.

D.As

socia

te Pro

fesso

r, Edu

catio

nal L

eade

rship,

Dire

ctor o

f Lea

n Thin

king f

or Sc

hools

, Pa

wley

Learn

ing In

stitut

e, Oa

kland

Univ

ersity

, Mich

igan

Anab

ela A

lves,

Ph.D

.As

sistan

t Prof

essor,

Depa

rtame

nto de

Prod

ução e

Siste

mas E

scola

de En

genh

aria d

a Univ

ersida

de

do M

inho,

Centr

o Inte

rdisci

plinar

de Te

cnolog

ias, d

a Prod

ução e

da En

ergia

(CITP

E)Ca

mpus

de Az

urém,

Portu

gal

Mond

ay, 2

2 Ju

ne 2

015

21-C

FD-1

Unstr

uctu

red H

igh-O

rder

Meth

ods I

Gran

d Ball

room

ACh

aired

by: S

. MUR

MAN,

NAS

A Ame

s Res

earch

Cente

r and

A. KA

TZ09

00 hr

sAIA

A-201

5-228

3Hi

gh-O

rder

Stra

nd G

rid M

ethod

s fo

r Sho

ck Tu

rbule

nce I

nter

actio

nO.

Tong

, A. K

atz, U

tah S

tate U

nivers

ity,

Loga

n, UT

; J. S

itaram

an, U

.S. A

rmy,

Moffe

tt Fie

ld, CA

0930

hrs

AIAA-2

015-2

284

High

er-o

rder

Uns

tructu

red F

inite

Volum

e Meth

ods f

or Tu

rbule

nt

Aero

dyna

mic F

lows

A. Ja

lali, C

. Olliv

ier G

ooch

, Univ

ersity

of

Britis

h Colu

mbia,

Vanc

ouve

r, Can

ada

1000

hrs

AIAA-2

015-2

285

A Sp

ectra

l-Elem

ent A

ppro

ach

for

the E

ikona

l Equ

ation

S. M

urman

, L. D

iosad

y, NA

SA Am

es

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1030

hrs

AIAA-2

015-2

286

High

orde

r sub

cell fi

nite v

olume

me

thod

in so

lving

hyp

erbo

lic

cons

erva

tion

laws

J. Pa

n, Y.

Ren,

Tsing

hua U

nivers

ity,

Beijin

g, Ch

ina

Mond

ay, 2

2 Ju

ne 2

015

22-C

FD-2

Unste

ady F

low Si

mulat

ions

Gran

d Ball

room

BCh

aired

by: Y

. WAN

G an

d D. R

EASO

R, Air

Force

Rese

arch L

abora

tory

0900

hrs

AIAA-2

015-2

287

Unste

ady S

imula

tions

of Sh

ockw

ave-

Boun

dary

Laye

r Inte

racti

on In

duced

Tra

nson

ic Sho

ckwa

ve O

scilla

tions

using

Un

struc

tured

Grid

sK.

Bham

idipati

, D. R

easor

, 412

th Tes

t Wing

, Ed

wards

AFB,

CA; C

. Pasi

liao, A

ir Forc

e Re

search

Labo

ratory

, Eglin

AFB,

FL

0930

hrs

AIAA-2

015-2

288

Effe

ct of

Cavit

y Flow

on La

nding

Ge

ar A

erod

ynam

ic Lo

ads

U. O

za, Z

. Hu,

X. Zh

ang,

Unive

rsity

of So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1000

hrs

AIAA-2

015-2

289

Nume

rical

Inve

stiga

tion

of th

e De

tach

ing Vo

rtica

l Flow

at R

otat

ing

Cylin

ders

with

Thom

Disc

sR.

Ritz,

T. Sc

homb

erg, O

. Wün

sch,

Unive

rsity

of Ka

ssel, K

asse

l, Germ

any;

M.

Ruett

en, R

. Kes

sler, G

erman

Aeros

pace

Ce

nter (

DLR)

, Gött

ingen

, Germ

any

1030

hrs

AIAA-2

015-2

290

Symm

etrica

l and

non

-symm

etrica

l 3D

wing

defo

rmat

ion of

flap

ping

micro

aeria

l veh

icles

W. Ta

y, Na

tiona

l univ

ersity

of S

ingap

ore,

Singa

pore,

Sing

apore

1100

hrs

AIAA-2

015-2

291

Nume

rical

Inve

stiga

tion

of th

e Sta

rting

Pro

cess

in a L

ong-

test-

dura

tion

Hype

rvelo

city S

hock

Tu

nnel

Y. Wa

ng, Z

. Hu,

Z. Jia

ng, C

hines

e Ac

adem

y of S

cienc

es, B

eijing

, Chin

a

46

Mond

ay, 2

2 Ju

ne 2

015

23-C

FD-3

Mesh

ing Te

chniq

ues I

Cora

lCh

aired

by: D

. THO

MPSO

N, M

ississ

ippi S

tate U

nivers

ity an

d B. J

OLLY,

US

Air Fo

rce09

00 hr

sAIA

A-201

5-229

2Co

mpar

ing A

nisot

ropic

Out

put-

Base

d Grid

Ada

ptat

ion M

ethod

s by

Deco

mpos

ition

M. Pa

rk, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA;

A. Lo

seille

, Fren

ch N

ation

al Ins

titute

for Re

searc

h in C

ompu

ter S

cienc

e an

d Con

trol (

INRIA

), Le

Ches

nay,

Franc

e; J.

Krako

s, T.

Mich

al, Th

e Boe

ing Co

mpan

y, St

. Lou

is, M

O

0930

hrs

AIAA-2

015-2

293

mesh

Curv

e: An

Aut

omat

ed

Low-

Orde

r to H

igh-O

rder

Mes

h Ge

nera

tor

J. Im

s, Z.

Duan

, Z. W

ang,

Unive

rsity

of Ka

nsas

, Law

rence

, Law

rence

, KS

1000

hrs

AIAA-2

015-2

294

Targ

et-Ed

ge B

ased

Orth

ogon

al An

isotro

pic M

esh

J. Zu

niga V

azqu

ez, C

. Olliv

ier G

ooch

, Un

iversi

ty of

Britis

h Colu

mbia,

Vanc

ouve

r, Ca

nada

1030

hrs

AIAA-2

015-2

295

Autom

ated M

assiv

ely Re

finem

ent

Techn

ique f

or M

ulti-b

lock S

tructu

red

Grids

Based

on N

URBS

Volum

eH.

Koizu

mi, S

. Tsu

tsumi

, R. T

akak

i, Jap

an

Aeros

pace

Explo

ration

Agen

cy (J

AXA)

, Sa

gami

hara,

Japa

n; K.

Yama

moto,

Japa

n Ae

rospa

ce Ex

plorat

ion Ag

ency

(JAX

A),

Mitak

a, Ja

pan;

H. It

o, M.

Abe,

Ryoy

u Sy

stems

, Nag

oya,

Japa

n; et

al.

1100

hrs

AIAA-2

015-2

296

Cons

tructi

on of

Pris

m an

d Hex

La

yers

from

Aniso

tropic

Tetra

hedr

aJ.

Stein

brenn

er, Po

intwi

se, I

nc.,

Fort

Worth

, TX

Mond

ay, 2

2 Ju

ne 2

015

24-C

FD-4

LES,

DNS,

and H

ybrid

RAN

S-LE

S IEm

erald

Chair

ed by

: A. S

ESCU

, Miss

issipp

i Stat

e Univ

ersity

and W

. MCM

ULLA

N, U

nivers

ity of

Leice

ster

0900

hrs

AIAA-2

015-2

297

High

Ord

er Nu

meric

al Me

thods

for

the D

ynam

ic SGS

Mod

el of

Turb

ulent

Flows

with

Shoc

ksD.

Kotov

, Bay

Area

Envir

onme

ntal R

esearc

h Ins

titute,

Petal

uma,

CA; H

. Yee

, A. W

ray,

NASA

Ames

Resea

rch Ce

nter, M

offett

Field

, CA

; B. S

jogree

n, La

wren

ce Liv

ermore

Nati

onal

Labo

ratory

, Live

rmore

, CA

0930

hrs

AIAA-2

015-2

298

Larg

e Edd

y Sim

ulatio

n of

Su

perso

nic Im

pingin

g Jets

by

Adap

tive,

Expli

cit Fi

lterin

gS.

Patel

, J. M

athew

, Ind

ian In

stitut

e of

Scien

ce, B

anga

lore,

India

1000

hrs

AIAA-2

015-2

299

Reso

lved S

calar

Mixi

ng in

Larg

e Ed

dy Si

mulat

ions o

f a Lo

w Re

ynold

s Num

ber P

lane M

ixing

La

yer

J. Ha

ywoo

d, A.

Sescu

, Miss

issipp

i Stat

e Un

iversi

ty, M

ississ

ippi S

tate,

MS

1030

hrs

AIAA-2

015-2

300

Reso

lved S

calar

Mixi

ng in

Larg

e Ed

dy Si

mulat

ions o

f a Lo

w Re

ynold

s Num

ber P

lane M

ixing

La

yer

S. H

ug, W

. McM

ullan

, Univ

ersity

of

Leice

ster, L

eices

ter, U

nited

King

dom

1100

hrs

AIAA-2

015-2

301

LES S

imula

tion

Inflo

w co

nditio

ns

for O

utlet

Guid

e Van

e and

Pr

ediff

user

Flow

sJ.

Li, N

anjin

g Univ

ersity

of Ae

ronau

tics

and A

stron

autic

s, Na

njing

, Chin

a; G.

Page

, J.

McGu

irk, L

ough

borou

gh U

nivers

ity,

Loug

hboro

ugh,

Unite

d King

dom

Mond

ay, 2

2 Ju

ne 2

015

25-FD

-1Wi

ng A

erod

ynam

icsGo

veno

rs Le

cture

Hall

Chair

ed by

: D. Y

OUNG

, Ray

theon

Miss

ile S

ystem

s and

U. K

AUL,

NASA

ARC

0900

hrs

AIAA-2

015-2

302

The O

rigin

of Li

ft Re

visite

d: I.

A Co

mplet

e Phy

sical

Theo

ryT.

Liu, W

ester

n Mich

igan U

nivers

ity,

Kalam

azoo

, MI;

J. W

u, J.

Zhu,

L. Liu

, Pe

king U

nivers

ity, B

eijing

, Chin

a

0930

hrs

AIAA-2

015-2

303

The O

rigin

of Li

ft Re

visite

d: II.

Ph

ysica

l Pro

cesse

s of A

irfoil

-Cir

culat

ion Fo

rmat

ion in

Star

ting

Flow

J. Zh

u, S.

Zou,

L. Liu

, J. W

u, Pe

king

Unive

rsity,

Beij

ing, C

hina;

T. Liu

, Wes

tern

Mich

igan U

nivers

ity, K

alama

zoo,

MI

1000

hrs

AIAA-2

015-2

304

The S

teady

Aer

odyn

amics

of Q

uiet

Airfo

ils w

ith P

oros

ity G

radie

nts

R. Ha

jian,

J. Ja

worsk

i, Leh

igh U

nivers

ity,

Bethl

ehem

, PA

1030

hrs

AIAA-2

015-2

305

Lift a

nd D

rag i

n Tw

o-Di

mens

ional

Stead

y Visc

ous a

nd Co

mpre

ssible

Flo

w: I.

Far-F

ield F

ormu

lae A

nalys

is an

d Num

erica

l Con

firma

tion

J. Zh

u, L.

Liu, P

eking

Univ

ersity

, Beij

ing,

China

; T. L

iu, W

ester

n Mich

igan U

nivers

ity,

Kalam

azoo

, MI;

Y. Sh

i, W. S

u, J.

Wu,

Pekin

g Univ

ersity

, Beij

ing, C

hina

1100

hrs

AIAA-2

015-2

306

Lift a

nd D

rag i

n Tw

o-Di

mens

ional

Stead

y Visc

ous a

nd Co

mpre

ssible

Flo

w: II

. Fun

dame

ntal

Solut

ion

Theo

ryL.

Liu, J

. Wu,

Pekin

g Univ

ersity

, Beij

ing,

China

; T. L

iu, W

ester

n Mich

igan U

nivers

ity,

Kalam

azoo

, MI

1130

hrs

AIAA-2

015-2

307

Effe

cts of

Per

turb

ation

on th

e Flow

ov

er N

onsle

nder

Delt

a Wing

sC.

Canp

olat,

B. Sa

hin, C

ukuro

va U

nivers

ity,

Adan

a, Tu

rkey;

S. Ya

yla, Y

uzun

cu Y

il Un

iversi

ty, Va

n, Tu

rkey;

H. Ak

illi, C

ukuro

va

Unive

rsity,

Adan

a, Tu

rkey

1200

hrs

AIAA-2

015-2

308

Inter

actio

n of

Mult

iple V

ortic

es ov

er

a Dou

ble D

elta W

ingX.

Zhan

g, Z.

Wang

, I. G

ursul,

Univ

ersity

of

Bath,

Bath

, Unit

ed Ki

ngdo

m

47

Mond

ay, 2

2 Ju

ne 2

015

26-FD

-2Fu

ndam

enta

l Flui

d Flow

sSe

nato

rs Le

cture

Hall

Chair

ed by

: G. D

ALE,

Air Fo

rce Re

searc

h Lab

orator

y and

M. G

REEN

, Syra

cuse

Univ

ersity

0900

hrs

AIAA-2

015-2

309

Evolu

tion

of St

ratifi

ed B

ound

ary-

Free

Shea

r Flow

s Und

er St

okes

-Ek

man

Forci

ngM.

Jone

s, E.

Pater

son, V

irginia

Polyt

echnic

Ins

titute

and S

tate U

nivers

ity, Bl

acksbu

rg, VA

0930

hrs

AIAA-2

015-2

310

Nume

rical

and E

xperi

menta

l Inv

estiga

tion o

f Wind

Turb

ine W

akes

X. Hu

ang,

RWTH

Aache

n Univ

ersity,

Aache

n, Ge

rman

y; S.

Vey,

Techn

ical U

nivers

ity of

Be

rlin, B

erlin,

Germ

any;

M. M

einke

, W.

Schro

eder,

RWTH

Aache

n Univ

ersity,

Aache

n, Ge

rman

y; G.

Pechl

ivano

glou,

C. Na

yeri,

Techn

ical U

nivers

ity of

Berlin

, Berl

in, Ge

rman

y; et

al.

1000

hrs

AIAA-2

015-2

311

Evide

nce o

f com

plex

flow

struc

ture

s in

a con

verg

ing-d

iverg

ing n

ozzle

ca

used

by a

rece

ssed s

tep at

the

nozz

le th

roat

M. Ca

rmine

, R. C

heli,

F. Co

zzi, A

. Sp

inelli,

M. Z

occa

, A. G

uardo

ne, T

echn

ical

Unive

rsity

of Mi

lan, M

ilan,

Italy

1030

hrs

AIAA-2

015-2

312

Nume

rical

Study

of th

e Tra

nsien

t De

forma

tion a

nd D

rag C

hara

cteris

tics

of a D

eceler

ating

Dro

plet

Q. Q

u, P.

Ma, P

. Liu,

Beih

ang U

nivers

ity,

Beijin

g, Ch

ina; S

. Li, B

eijing

Insti

tute o

f Me

chan

ical a

nd El

ectric

al En

ginee

ring,

Beijin

g, Ch

ina; R

. Aga

rwal,

Was

hingto

n Un

iversi

ty in

St. L

ouis,

St.

Louis

, MO

Mond

ay, 2

2 Ju

ne 2

015

27-FD

-3Co

mbus

tion

and H

eat T

rans

fer

Topa

zCh

aired

by: J

. CHO

I, Ge

orgia

Institu

te of

Tech

nolog

y and

I. LE

YVA

0900

hrs

AIAA-2

015-2

313

An Ex

perim

enta

l Stu

dy of

Glob

al Ch

arac

terist

ics of

Turb

ulent

Di

ffusio

n Je

t Flam

es fo

r Fue

ls of

Co

mplex

Chem

istry

A. Ra

mach

andra

n, V.

Naray

anas

wamy

, No

rth Ca

rolina

Stat

e Univ

ersity

, Rale

igh,

NC

0930

hrs

AIAA-2

015-2

314

Comp

ariso

n of T

heor

etica

l and

Semi

-Em

pirica

l Solu

tions

for D

issipa

tion

Coeffi

cient

in a L

ow Re

ynold

s Num

ber

Comp

resso

r Cas

cade

F. Ko

k, R.

Myos

e, W

ichita

Stat

e Univ

ersity

, W

ichita

, KS;

S. H

ayas

hibara

, Emb

ry-Rid

dle

Aeron

autic

al Un

iversi

ty, Pr

esco

tt, AZ

1000

hrs

AIAA-2

015-2

315

On au

toign

ition-

domi

nated

su

perso

nic co

mbus

tion

N. Cy

mbali

st, P.

Dim

otakis

, Cali

fornia

Ins

titute

of Te

chno

logy,

Pasa

dena

, CA

1030

hrs

AIAA-2

015-2

316

Flow

Fields

of M

anipu

lated

Shea

r La

yers

of a

Turb

ulent

Jet F

lame

H. N

awrot

h, C.

Pasch

ereit,

Tech

nical

Unive

rsity

of Be

rlin, B

erlin,

Germ

any

Mond

ay, 2

2 Ju

ne 2

015

28-FD

-4Bo

unda

ry La

yer T

rans

ition:

Hyp

erso

nic Fl

ows

Sapp

hire

Chair

ed by

: J. J

EWEL

L, Air

Force

Rese

arch L

abora

tory a

nd K.

CASP

ER09

00 hr

sAIA

A-201

5-231

7In

stabil

ity an

d Tra

nsitio

n Ex

perim

ents

in th

e Boe

ing/A

FOSR

Ma

ch 6

Quie

t Tun

nel

G. M

cKier

nan,

B. Ch

ynow

eth, S

. Sc

hneid

er, Pu

rdue U

nivers

ity, W

est

Lafay

ette,

IN

0930

hrs

AIAA-2

015-2

318

Nume

rical

Inves

tigati

on of

Non

linea

r Wa

ve-p

acke

ts in

a Hyp

erso

nic H

igh-

Entha

lpy B

ound

ary-

Laye

r on a

5

deg S

harp

Cone

L. Sa

lemi, H

. Fas

el, U

nivers

ity of

Arizo

na,

Tucso

n, Tu

cson,

AZ

1000

hrs

AIAA-2

015-2

319

Corre

lation

of H

IFiRE

-5 Fl

ight D

ata

With

Comp

uted

Pre

ssure

and H

eat

Trans

fer

J. Je

well,

J. Mi

ller, R

. Kim

mel, A

ir Forc

e Re

searc

h Lab

orator

y, W

right-

Patte

rson

AFB,

OH

1030

hrs

AIAA-2

015-2

320

Linea

r sta

bility

of h

igh-sp

eed

boun

dary

laye

r flow

s at v

aryin

g Pr

andt

l num

bers

A. Ra

macha

ndran

, B. S

aikia,

K. Si

nha,

Indian

Ins

titute

of Tec

hnolo

gy Bo

mbay,

Mum

bai,

India;

R. Go

vinda

rajan

, Tata

Instit

ute of

Fu

ndam

ental

Resea

rch, H

ydera

bad,

India

48

Mond

ay, 2

2 Ju

ne 2

015

29-M

AO-1

Vehic

le De

sign

Appli

catio

ns I

Madr

idCh

aired

by: R

. KOL

ONAY

, Air F

orce R

esea

rch La

borat

ory/R

QVC/

WPA

FB an

d V. K

ALIVA

RAPU

, Iow

a Stat

e Univ

ersity

0900

hrs

AIAA-2

015-2

321

Para

llel a

lloca

tion-

missi

on

optim

izatio

n of

a 12

8-ro

ute

netw

ork

J. Hw

ang,

J. Ma

rtins,

Unive

rsity

of Mi

chiga

n, An

n Arbo

r, Ann

Arbo

r, MI

0930

hrs

AIAA-2

015-2

322

Multi-

Objec

tive D

esign

and

Path

Plan

ning O

ptim

izatio

n of

Un

mann

ed A

erial

Vehic

les (U

AVs)

E. Ru

dnick

-Cohe

n, S.

Azarm

, J. H

errma

nn,

Unive

rsity

of Ma

rylan

d, Co

llege

Park,

Co

llege

Park,

MD

1000

hrs

AIAA-2

015-2

323

Cont

rol P

ower

Opt

imiza

tion

using

Ar

tificia

l Int

ellige

nce f

or H

ybrid

Wi

ng B

ody A

ircra

ftR.

Chha

bra, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA; S

. Mu

lani, U

nivers

ity of

Alab

ama,

Tusca

loosa

, Tu

scaloo

sa, A

L; R.

Kapa

nia, J

. Sch

etz,

Virgin

ia Po

lytec

hnic

Institu

te an

d Stat

e Un

iversi

ty, B

lacks

burg,

VA

1030

hrs

AIAA-2

015-2

324

Cont

rol F

ocus

ed M

ultidi

scipli

nary

De

sign

Optim

izatio

n of

Taille

ss Fig

hter

Airc

raft

C. Me

ckstr

oth, U

nivers

ity of

Day

ton,

Dayto

n, OH

; W. B

lake,

Air Fo

rce Re

searc

h La

borat

ory, W

right-

Patte

rson A

FB, O

H

1100

hrs

AIAA-2

015-2

325

Hybr

id Wi

ng B

ody (

HWB)

Airc

raft

Desig

n an

d Opt

imiza

tion

using

Sti

tched

Comp

osite

sV.

Li, Th

e Boe

ing Co

mpan

y, Hu

nting

ton

Beac

h, CA

1130

hrs

AIAA-2

015-2

326

A Mu

lti-Fid

elity,

Mult

i-Disc

iplina

ry

Analy

sis an

d Opt

imiza

tion

Fram

ewor

k fo

r the

Des

ign of

Mo

rphin

g UAV

Wing

A. Cia

rella,

C. Ts

otska

s, M.

Hahn

, Aircr

aft

Resea

rch As

sociat

ion, L

td., B

edfor

d, Un

ited

Kingd

om; N

. Wert

er, R.

De Br

euke

r, De

lft Un

iversit

y of T

echno

logy,

Delft,

The

Nethe

rland

s; C.

Beav

erstoc

k, Sw

ansea

Un

iversit

y, Sw

ansea

, Unit

ed Ki

ngdo

m; et

al.

1200

hrs

AIAA-2

015-2

327

Multi-

Disci

plina

ry an

d Mult

i-Ob

jectiv

e Opt

imiza

tion

of an

Un

conv

entio

nal A

ircra

ft Co

ncep

tS.

Gem

ma, F

. Mas

trodd

i, Univ

ersity

of

Rome

“La S

apien

za”,

Rome

, Ital

y

Mond

ay, 2

2 Ju

ne 2

015

30-M

ST-1

Unma

nned

Aer

ial Ve

hicle

Syste

msTra

verti

neCh

aired

by: B

. LAN

DRUM

and M

. PAT

IL, V

irgini

a Tec

h09

00 hr

sAIA

A-201

5-232

8Ex

perim

enta

l Cha

racte

rizat

ion of

Bu

tterfl

y in

Climb

ing Fl

ight

J. Cra

nford,

Univ

ersity

of Al

abam

a, Hu

ntsvil

le, H

untsv

ille, A

L; N.

Sleg

ers,

Georg

e Fox

Univ

ersity

, New

berg,

OR;

B. La

ndrum

, Univ

ersity

of Al

abam

a, Hu

ntsvil

le, H

untsv

ille, A

L

0930

hrs

AIAA-2

015-2

329

Nond

eterm

inisti

c Sim

ulatio

n for

Pr

obab

ility o

f Los

s of C

ontro

l Pr

edict

ion fo

r Unm

anne

d Airc

raft

Syste

msL.

Hale,

M. P

atil, C

. Roy,

Virgi

nia Po

lytech

nic

Institu

te an

d Stat

e Univ

ersity,

Black

sburg,

VA

1000

hrs

AIAA-2

015-2

330

Optim

al se

lectio

n of

UAV

for

grou

nd ta

rget

track

ingJ.

Narki

ewicz

, A. K

opyt,

P. Ra

dyisy

ewsk

i, T.

Malec

ki, W

arsaw

Univ

ersity

of

Tech

nolog

y, Wa

rsaw,

Polan

d

1030

hrs

AIAA-2

015-2

331

Dyna

mic R

esou

rce A

lloca

tion

for

Shar

ing M

ulti-U

AV Se

rvice

sB.

Kadd

ouh,

W. Cr

owthe

r, P. H

olling

swort

h, Un

iversi

ty of

Manc

heste

r, Man

ches

ter,

Unite

d King

dom

1100

hrs

AIAA-2

015-2

332

Optim

al Ob

ject L

ocat

ion by

a Fle

et of

Vario

us U

AVs

A. Ko

pyt,

J. Na

rkiew

icz, T

. Male

cki, P

. Ra

dyisy

ewsk

i, Wars

aw U

nivers

ity of

Te

chno

logy,

Warsa

w, Po

land

1130

hrs

AIAA-2

015-2

333

Mode

ling a

nd Co

ntro

l of T

ether

ed

Unma

nned

Mult

icopt

ers i

n Ho

verin

g Flig

htD.

Ferre

ira de

Castr

o, J.

Santo

s, M.

Ba

tista,

D. A

ntônio

dos S

antos

, L. G

óes,

Tech

nolog

ical In

stitut

e of A

erona

utics

(ITA)

, São

José

dos C

ampo

s, Br

azil

1200

hrs

AIAA-2

015-2

334

MAV P

ose M

easu

reme

nt al

gorit

hm

Base

d on

Visua

l Sys

tems

Q. Ze

ng, J

. Liu,

Y. W

ang,

Nanji

ng

Unive

rsity

of Ae

ronau

tics a

nd As

trona

utics,

Na

njing

, Chin

a

Mond

ay, 2

2 Ju

ne 2

015

31-M

ST-2

Aviat

ion Sy

stems

Hum

an Fa

ctors

Wyeth

Chair

ed by

: D. C

ARTM

ELL,

Boein

g Eng

ineeri

ng O

perat

ions &

Tech

nolog

y and

S. R

OBIN

SON,

UC D

avis

0900

hrs

AIAA-2

015-2

335

Form

al Ex

tensio

ns to

the I

nten

t-Ba

sed M

ode C

onfu

sion

Detec

tion

Fram

ewor

kJ.

Suraj

Nan

digan

ahall

i, I. H

wang

, Purd

ue

Unive

rsity,

Wes

t Lafa

yette

, IN

0930

hrs

AIAA-2

015-2

336

The R

apidl

y Rec

onfig

urab

le Re

sear

ch Co

ckpit

R. Jo

yce,

S. Ro

binso

n, Un

iversi

ty of

Califo

rnia,

Davis

, Dav

is, CA

1000

hrs

AIAA-2

015-2

337

Fligh

t Crew

Resp

onse

to Un

expe

cted

Even

ts: A

Simula

tor Ex

perim

ent

J. Fie

ld, N

ation

al Ae

rospa

ce La

borat

ory

(NLR

), Am

sterda

m, Th

e Neth

erlan

ds;

L. Fu

cke,

B. Co

rreia

Grác

io, Th

e Boe

ing

Comp

any,

Madri

d, Sp

ain; M

. Varn

ey,

Airbu

s, To

ulous

e, Fra

nce

1030

hrs

AIAA-2

015-2

338

Influ

ence

of co

upled

side

stick

s on

the p

ilot m

onito

ring’s

awar

enes

s du

ring fl

are

A. Ue

hara,

D. N

iederm

eier, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Brau

nsch

weig,

Ge

rman

y

1100

hrs

Oral

Prese

ntatio

nEr

gono

mic e

valua

tion

of di

ffere

nt

princ

iples

of po

sition

indic

ation

and

cont

rol p

lane i

n fie

ldM.

Zhelo

nkin,

Y. D

ubov

, V. Z

helon

kin, O

. Tk

ache

nko,

TsAGI

, Zhu

kovs

ky, R

ussia

1130

hrs

AIAA-2

015-2

339

Equa

tion-

Syste

m Re

pres

enta

tion

Mode

l for

Pne

umat

ic Se

at D

esign

Us

ed fo

r Vibr

ation

Isola

tion

In A

ir an

d Gro

und T

rans

port

E. Ay

yad,

W. Cu

lbreth

, D. R

eyno

lds,

Unive

rsity

of Ne

vada

, Las

Vega

s, La

s Ve

gas,

NV

1200

hrs

Oral

Prese

ntatio

nAn

appr

oach

to es

tabli

sh ca

se ba

se

of m

otion

s for

layo

ut op

timiza

tion

Y. Zh

ang,

Y. Su

n, L.

Liu, N

anjin

g Univ

ersity

of

Aeron

autic

s and

Astro

nauti

cs, Ya

ngzh

ou,

China

Mond

ay, 2

2 Ju

ne 2

015

32-N

W-1

0900

- 09

30 h

rsNe

twor

king C

offe

e Bre

akMe

eting

Roo

m Fo

yers

49

Mond

ay, 2

2 Ju

ne 2

015

33-P

DL-1

/FD-

5Pla

sma A

erod

ynam

ics &

Flow

Cont

rol I

Mone

t Ball

room

Chair

ed by

: M. S

TANE

K, AF

RL/R

QVI

0900

hrs

AIAA-2

015-2

340

Nume

rical

Simula

tions

of

Distu

rban

ces i

n Sh

ear F

lows

Intro

duce

d by N

S-DB

D Pla

sma

Actu

ator

sI.

Popo

v, G.

Corre

ale, S

. Huls

hoff,

Delf

t Un

iversi

ty of

Tech

nolog

y, De

lft, Th

e Ne

therla

nds

0930

hrs

AIAA-2

015-2

341

Nano

seco

nd D

ielec

tric B

arrie

r Di

schar

ge P

lasma

Actu

ator

Flow

Co

ntro

l of C

ompr

essib

le Dy

nami

c Sta

llM.

Fran

khou

ser, J

. Greg

ory, O

hio S

tate

Unive

rsity,

Colum

bus,

OH

1000

hrs

AIAA-2

015-2

342

Aero

dyna

mic C

ontro

l Effe

ct of

Su

rface

DC P

lasma

Disc

harg

e at

Mach

-7 H

yper

sonic

Flow

Y. Wa

tanab

e, Un

iversi

ty of

Toky

o, Bu

nkyo

, Ja

pan;

K. Su

zuki,

Univ

ersity

of To

kyo,

Kash

iwa,

Japa

n

1030

hrs

AIAA-2

015-2

343

Effect

of Pu

lsed P

lasma

Jets

on Bo

unda

ry La

yer R

ecove

ry

Down

strea

m of

a Refl

ected

Shoc

k Wa

ve-B

ound

ary L

ayer

Intera

ction

B. Gre

ene,

N. Cl

emen

s, Un

iversit

y of T

exas,

Au

stin, A

ustin,

TX; P.

Mag

ari, D

. Mick

a, M.

Ue

ckerm

ann,

Creare

, Inc.,

Hann

over,

NH

1100

hrs

AIAA-2

015-2

344

Single

Nan

oseco

nd D

ielect

ric Ba

rrier

Di

schar

ge an

d Puls

ed Sl

iding

Di

schar

ge Ap

plied

to Se

para

tion

Contr

ol Alo

ng a

NACA

0015

Airfo

ilK.

Bayo

da, N

. Ben

ard, E

. More

au, N

ation

al Ce

nter fo

r Scie

ntific

Resea

rch (C

NRS)

, Fu

turosc

ope,

France

1130

hrs

AIAA-2

015-2

345

Shoc

k-Tra

pping

Capa

bility

of a

Cavit

y in

a Sup

erso

nic Fl

owN.

Web

b, M.

Sam

imy,

Ohio

State

Un

iversi

ty, Co

lumbu

s, OH

1200

hrs

AIAA-2

015-2

346

Pres

sure

Inve

stiga

tions

over

a Co

nical

Fore

body

und

er D

uty-

Cycle

d Plas

ma A

ctuat

ions

J. Zh

ao, X

. Men

g, J.

Wang

, Nort

hwes

tern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

; F.

Liu, S

. Luo

, Univ

ersity

of Ca

liforni

a, Irv

ine,

Los A

ngele

s, CA

Mond

ay, 2

2 Ju

ne 2

015

34-TP

-1Ab

lation

IRo

setta

Chair

ed by

: D. K

UNTZ

, San

dia N

ation

al La

borat

ories

and D

. PYT

EL, L

ockh

eed M

artin

Spac

e Sys

tems

0900

hrs

AIAA-2

015-2

347

Evalu

ation

of Fi

nite-

Rate

Gas/

Surfa

ce In

terac

tion

Mode

ls fo

r a

Carb

on B

ased

Abla

tor

Y. Ch

en, N

ASA A

mes R

esea

rch Ce

nter,

Moffe

tt Fie

ld, CA

; T. G

okce

n, ER

C, Inc

., Mo

ffett

Field,

CA

0930

hrs

AIAA-2

015-2

348

Comp

ariso

n of

Carb

on A

blativ

e Sh

ock-

Laye

r Rad

iation

with

High

Su

rface

Temp

erat

ures

S. Lew

is, R.

Morga

n, T.

Mcint

yre, U

nivers

ity

of Qu

eensl

and,

St. Lu

cia, A

ustral

ia; C.

Alba

, R.

Green

dyke

, Air F

orce I

nstitu

te of

Techn

ology,

Wr

ight-P

atters

on AF

B, OH

1000

hrs

AIAA-2

015-2

349

Stagn

ation

-Line

Simu

lation

s of

Meteo

r Abla

tion

B. D

ias, A

. Turc

hi, T.

Mag

in, vo

n Kárm

án

Institu

te for

Fluid

Dyn

amics

, Rho

de-Sa

int-

Genè

se, B

elgium

Mond

ay, 2

2 Ju

ne 2

015

35-TP

-2He

at Tr

ansfe

r ISte

uben

Chair

ed by

: M. K

IO, N

ation

al Sp

ace R

esea

rch &

Dev

elopm

ent A

genc

y and

A. W

ILLIAM

S, Ai

r Forc

e Res

each

Labo

ratory

0900

hrs

AIAA-2

015-2

350

Diffu

sion

Pene

tratio

n Tim

e for

Tra

nsien

t Con

ducti

onR.

McMa

sters,

Virgi

nia M

ilitary

Institu

te,

Lexing

ton, V

A; F. d

e Mon

te, Un

iversit

y of

L’Aqu

ila, L’A

quila,

Italy;

J. Be

ck, S.

Na

llapan

eni, M

ichiga

n Stat

e Univ

ersity,

E.

Lansi

ng, M

I; D. A

mos,

Sand

ia Na

tiona

l La

borat

ories,

Albu

querq

ue, N

M; A.

Haji-S

heikh

, Un

iversit

y of T

exas,

Arling

ton, A

rlingto

n, TX

0930

hrs

AIAA-2

015-2

351

Comp

ariso

ns of

Comp

utat

ions

with

Expe

rimen

ts fo

r Elec

tron

Trans

pirat

ion Co

oling

at H

igh

Enth

alpies

K. Ha

nquis

t, I.

Boyd

, Univ

ersity

of

Mich

igan,

Ann A

rbor, A

nn Ar

bor, M

I

1000

hrs

AIAA-2

015-2

352

Heat

and M

ass T

rans

fer A

nalys

is of

a F

ilm Ev

apor

ative

MEM

S Tun

eable

Ar

ray T

hrus

terW.

O’N

eill, A

. Cofe

r, A. W

eave

r, A.

Alexe

enko

, Purd

ue U

nivers

ity, W

est

Lafay

ette,

IN

1030

hrs

AIAA-2

015-2

353

Ther

mal M

odel

for S

inter

ed

Cylin

drica

l Eva

pora

tors

of Lo

op

Heat

Pipe

s(215

0991

)M.

Man

telli,

J. Flo

rez M

era, F

. Mila

nese

, Fe

deral

Univ

ersity

of S

anta

Catar

ina,

Floria

nópo

lis, B

razil

1100

hrs

AIAA-2

015-2

354

Study

of th

e Mini

mum

Anti-

icing

En

ergy

Bas

ed on

Icing

Limi

t Sta

teY.

Zhao

, S. C

hang

, Y. B

o, M.

Leng

, Be

ihang

Univ

ersity

, Beij

ing, C

hina

1130

hrs

AIAA-2

015-2

355

Studie

s on

ther

mal c

ondu

ctivit

y pr

edict

ion of

fibe

r rein

force

d ma

terial

with

micr

osco

pic st

ructu

re

ident

ifica

tion

J. Hu

a, Na

njing

Univ

ersity

of Ae

ronau

tics

and A

stron

autic

s, Na

njing

, Chin

a

Mond

ay, 2

2 Ju

ne 2

015

36-F3

60-1

09

30 -

1200

hrs

The V

oice o

f the

Custo

mer -

Des

igning

the R

ight A

ircra

ftGr

and B

allro

om E

Mode

rator:

Chris

tophe

r Ston

ehou

se, S

enior

Vice

Pres

ident,

Custo

mer S

ervice

s, Air

bus A

meric

as, I

nc.

P

aneli

sts:

Jack

Are

hart

Presid

ent o

f MRO

Serv

ices

Delta

Tech

Ops

Willia

m “B

ill” M

eeha

nCh

ief O

perat

ing O

fficer

Fronti

er Air

lines

, Inc

.

Bart

Robe

rtsVic

e Pres

ident,

Fligh

t Tec

hnica

l Ope

ration

sJe

tBlue

Airw

ays

David

Seym

our

Senio

r Vice

Pres

ident,

Tech

nical

Opera

tions

Ameri

can A

irline

s

50

Mond

ay, 2

2 Ju

ne 2

015

37-A

A-6

Open

Rot

or I

Fleur

-de-

lis A

Chair

ed by

: A. L

YRIN

TZIS

1400

hrs

AIAA-2

015-2

356

Aero

dyna

mic a

nd A

eroa

cous

tic

Effe

cts of

Pylo

n Tra

iling E

dge

Blow

ing on

Pus

her P

rope

ller

Insta

llatio

nT.

Sinnig

e, K.

Lync

h, D.

Ragn

i, G.

Eitelb

erg, L

. Veld

huis,

Delf

t Univ

ersity

of

Tech

nolog

y, De

lft, Th

e Neth

erlan

ds

1430

hrs

AIAA-2

015-2

357

Hybr

id Us

e of C

FD an

d Ana

lytica

l Me

thod

s for

the P

redic

tion

of

Adva

nced

Ope

n Ro

tor T

one N

oise

C. Ek

oule,

M. K

ingan

, A. M

cAlpin

e, So

utham

pton U

nivers

ity, So

utham

pton,

Unite

d Kin

gdom

; N. S

ohon

i, Cam

bridg

e Univ

ersity,

Ca

mbrid

ge, U

nited

King

dom;

A. Pa

rry, R

olls-

Royce

Grou

p plc,

Derby

, Unit

ed Ki

ngdo

m

1500

hrs

AIAA-2

015-2

358

The E

ffects

of Sw

irl R

ecov

ery

Vane

s on

Single

-Rot

ation

Pro

pelle

r Ae

rody

nami

cs an

d Aer

oaco

ustic

sT.

Sinnig

e, J.

van K

uijk,

K. Ly

nch,

D.

Ragn

i, G. E

itelbe

rg, L.

Veldh

uis, D

elft

Unive

rsity

of Te

chno

logy,

Delft,

The

Nethe

rland

s

1530

hrs

AIAA-2

015-2

359

Aircr

aft O

pen

Roto

r Tec

hnolo

gy:

Analy

sis fr

om an

Ope

ratio

nal

Persp

ectiv

eG.

Bus

ch, M

. Has

san,

D. M

avris

, Geo

rgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1600

hrs

AIAA-2

015-2

360

Optim

al Pr

opell

er D

esign

for Q

uiet

Aircr

aft u

sing N

umer

ical A

nalys

isB.

Hum

pert,

R. G

aeta,

J. Ja

cob,

Oklah

oma

State

Univ

ersity

, Still

water

, OK

1630

hrs

AIAA-2

015-2

361

Soun

d Rad

iation

from

a Ro

tor

Parti

ally I

mmer

sed i

n a T

urbu

lent

Boun

dary

Laye

rS.

Gleg

g, A.

Buon

o, J.

Gran

t, F.

Lach

owsk

i, Flo

rida A

tlanti

c Univ

ersity

, Boc

a Rato

n, FL

; W. D

even

port,

W. A

lexan

der, V

irgini

a Po

lytec

hnic

Institu

te an

d Stat

e Univ

ersity

, Bla

cksb

urg, V

A

Mond

ay, 2

2 Ju

ne 2

015

38-A

A-7

Trailin

g Edg

e Nois

e IFle

ur-d

e-lis

BCh

aired

by: R

. EW

ERT,

DLR -

Germ

an Ae

rospa

ce Ce

nter

1400

hrs

AIAA-2

015-2

362

A Tra

iling-

Edge

Nois

e Mod

el fo

r Se

rrated

Edge

sB.

Lyu,

Unive

rsity

of Ca

mbrid

ge,

Camb

ridge

, Unit

ed Ki

ngdo

m; M

. Az

arpey

vand

, Univ

ersity

of B

ristol

, Bris

tol,

Unite

d King

dom;

S. S

inayo

ko, U

nivers

ity

of So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1430

hrs

AIAA-2

015-2

363

Effe

ct of

serra

ted tr

ailing

edge

on

boun

dary

laye

r ins

tabil

ity n

oise

J. Se

rpieri

, S. P

röbsti

ng, M

. Gup

ta, F.

Sc

arano

, Delf

t Univ

ersity

of Te

chno

logy,

Delft,

The N

etherl

ands

1500

hrs

AIAA-2

015-2

364

The E

ffects

of Su

ction

and B

lowing

on

Tona

l Nois

e Gen

erat

ion by

Blun

t Tra

iling E

dges

W. Ra

mirez

, W. W

olf, U

nivers

ity of

Ca

mpina

s, Ca

mpina

s, Br

azil

1530

hrs

AIAA-2

015-2

365

Bio-

Insp

ired T

railin

g Edg

e Nois

e Co

ntro

lI.

Clark,

W. A

lexan

der, W

. Dev

enpo

rt,

Virgin

ia Po

lytec

hnic

Institu

te an

d Stat

e Un

iversi

ty, B

lacks

burg,

VA; S

. Gleg

g, Flo

rida A

tlanti

c Univ

ersity

, Boc

a Rato

n, FL

; J.

Jawo

rski, L

ehigh

Univ

ersity

, Beth

lehem

, PA

; C. D

aly, U

nivers

ity of

Camb

ridge

, Ca

mbrid

ge, U

nited

King

dom;

et al

.

1600

hrs

AIAA-2

015-2

366

Nume

rical

and e

xper

imen

tal

inves

tigat

ion of

a be

veled

trail

ing

edge

flow

and n

oise fi

eldW.

van d

er Ve

lden,

S. Pr

öbsti

ng, A

. de

Jong

, A. v

an Zu

ijlen,

Delft

Unive

rsity

of Te

chno

logy,

Delft,

The N

etherl

ands

; Y.

Guan

, S. M

orris,

Univ

ersity

of N

otre D

ame,

Notre

Dam

e, IN

1630

hrs

AIAA-2

015-2

367

On th

e rob

ustn

ess o

f the

TNO

mode

l for

aero

foil s

elf-n

oise

pred

iction

C. Pa

ruchu

ri, O.

Stal

nov,

P. Jo

seph

, C.

Vand

erwel,

B. G

anap

athisu

brama

ni,

Unive

rsity

of So

utham

pton,

South

ampto

n, Un

ited K

ingdo

m; R.

Leun

g, De

fence

Sc

ience

and T

echn

ology

Labo

ratory

, So

utham

pton,

Unite

d King

dom

1700

hrs

AIAA-2

015-2

368

Impa

ct of

Wall

Per

meab

ility

on Tr

ailing

-Edge

Nois

e at H

igh

Reyn

olds N

umbe

rS.

Koh,

M. M

einke

, W. S

chroe

der, R

WTH

Aa

chen

Univ

ersity

, Aac

hen,

Germ

any

Mond

ay, 2

2 Ju

ne 2

015

39-A

A-8

Jet N

oise P

redic

tion

IIIn

vern

ess

Chair

ed by

: D. M

CLAU

GHLIN

, Reti

red14

00 hr

sAIA

A-201

5-236

9Re

cent

prog

ress

in nu

meric

al sim

ulatio

ns fo

r jet

noise

co

mput

ation

usin

g LES

on fu

lly

unstr

uctu

red m

eshe

sN.

Lupo

glazo

ff, F.

Vuillo

t, ON

ERA,

Châti

llon,

Franc

e

1430

hrs

AIAA-2

015-2

370

Jet N

oise P

redic

tion

with

Eddy

Re

laxat

ion So

urce

Mod

elA.

Neife

ld, N

. Reic

he, J

. Dier

ke, R

. Ew

ert, G

erman

Aeros

pace

Cente

r (DL

R),

Brau

nsch

weig,

Germ

any

1500

hrs

AIAA-2

015-2

371

Jet N

oise P

redic

tion

using

a Pe

rmea

ble FW

-H So

lver

A. We

st, CD

-adap

co, L

ondo

n, Un

ited

Kingd

om; M

. Cara

eni, C

D-ada

pco,

Leba

non,

NH

1530

hrs

AIAA-2

015-2

372

Para

metri

c Stu

dy of

Jet N

ozzle

s Us

ing a

RANS

-Bas

ed Je

t Nois

e Pr

edict

ion To

olB.

Venk

atesh

, R. S

elf, U

nivers

ity of

So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1600

hrs

AIAA-2

015-2

373

Larg

e Edd

y Sim

ulatio

n of

a Ta

ctica

l Ai

rcraf

t Exh

aust

Nozz

le wi

th Fr

ee-

strea

m an

d Wall

Turb

ulenc

eD.

Dah

l, J. N

ichols

, Univ

ersity

of

Minn

esota

, Minn

eapo

lis, M

innea

polis,

MN

51

Mond

ay, 2

2 Ju

ne 2

015

40-A

A-9

Jet N

oise M

easu

reme

nts I

Laliq

ueCh

aired

by: S

. MILL

ER, N

ASA

1400

hrs

AIAA-2

015-2

374

Noise

Red

uctio

n wi

th Fl

uidic

Inse

rts

in Su

perso

nic Je

ts Ex

haus

ting O

ver

a Sim

ulated

Airc

raft

Carri

er D

eck

R. Po

wers,

D. M

cLaug

hlin,

P. Mo

rris,

Penn

sylva

nia S

tate U

nivers

ity, S

tate

Colle

ge, P

A

1430

hrs

AIAA-2

015-2

375

Acou

stic E

missi

ons f

rom

F-35

Aircr

aft d

uring

Gro

und R

un-U

pM.

Jame

s, A.

Salto

n, J.

Down

ing, B

lue

Ridge

Rese

arch a

nd Co

nsult

ing, L

LC,

Ashe

ville,

NC;

K. Ge

e, T.

Neilse

n, B.

Re

ichma

n, Br

igham

Youn

g Univ

ersity

, Pro

vo, U

T; et

al.

1500

hrs

AIAA-2

015-2

376

Spat

iotem

pora

l Cor

relat

ion

Analy

sis of

Jet N

oise f

rom

a High

-Pe

rform

ance

Milit

ary A

ircra

ftB.

Hark

er, T.

Neil

sen,

K. Ge

e, Br

igham

Yo

ung U

nivers

ity, P

rovo,

UT; M

. Jam

es,

Blue R

idge R

esea

rch an

d Con

sultin

g, LLC

, As

hevil

le, N

C; A.

Wall,

Air Fo

rce Re

searc

h La

borat

ory, W

right-

Patte

rson A

FB, O

H

1530

hrs

AIAA-2

015-2

377

Acou

stica

l Env

ironm

ent o

f an

F-35B

Du

ring V

ertic

al La

nding

sB.

Reich

man,

Brigh

am Yo

ung U

nivers

ity,

Provo

, UT;

J. Do

wning

, M. J

ames

, Blue

Rid

ge Re

searc

h and

Cons

ulting

, LLC

, As

hevil

le, N

C; A.

Aube

rt, N

aval

Air W

arfare

Ce

nter, P

atuxe

nt Riv

er, M

D; R.

McK

inley

, A.

Wall,

Air Fo

rce Re

searc

h Lab

orator

y, W

right-

Patte

rson A

FB, O

H; et

al.

1600

hrs

AIAA-2

015-2

378

Sour

ce ch

arac

teriza

tion

of fu

ll-sca

le jet

nois

e usin

g vec

tor i

nten

sity

T. St

out,

K. Ge

e, T.

Neilse

n, A.

Wall,

Brigh

am Yo

ung U

nivers

ity, P

rovo,

UT;

M. Ja

mes,

Blue R

idge R

esea

rch an

d Co

nsult

ing, L

LC, A

shev

ille, N

C

1630

hrs

AIAA-2

015-2

379

Invest

igatio

n of m

ulti-lo

bed fi

ghter

jet

noise

sour

ces us

ing ac

ousti

cal

holog

raph

y and

parti

al fie

ld de

comp

ositio

n meth

ods

A. Wa

ll, Air

Force

Resea

rch La

borat

ory,

Wrigh

t-Patt

erson

AFB,

OH; K

. Gee

, T. N

eilsen

, Bri

gham

Youn

g Univ

ersity,

Prov

o, UT

; S.

McIne

rny, U

nivers

ity of

Louis

iana,

Lafay

ette,

Lafay

ette,

LA; M

. Jam

es, Bl

ue Ri

dge R

esearc

h an

d Con

sultin

g, LLC

, Ashe

ville,

NC

Mond

ay, 2

2 Ju

ne 2

015

41-A

A-10

CAA

Soun

d Gen

erat

ion I

Obeli

sk A

Chair

ed by

: C. T

AM, F

lorida

Stat

e Univ

eristy

1400

hrs

AIAA-2

015-2

380

Hydr

odyn

amic

insta

bility

and s

hear

lay

er ef

fect

on th

e sou

nd em

ission

of

a tu

rbule

nt je

t flam

eS.

Sch

limpe

rt, S

. Koh

, A. F

eldhu

sen,

B.

Roidl

, M. M

einke

, W. S

chroe

der, R

WTH

Aa

chen

Univ

ersity

, Aac

hen,

Germ

any

1430

hrs

AIAA-2

015-2

381

Asse

ssing

Aco

ustic

Sour

ce Fo

rcing

To

ols fo

r Lau

nch

Vehic

le Je

t Nois

e Pr

edict

ionA.

Sescu

, E. C

ollins

, Miss

issipp

i Stat

e Un

iversi

ty, M

ississ

ippi S

tate,

MS; R

. Harr

is,

CFD

Rese

arch C

orpora

tion,

Hunts

ville,

AL

; E. L

uke,

Missi

ssipp

i Stat

e Univ

ersity

, Mi

ssissi

ppi S

tate,

MS

1500

hrs

AIAA-2

015-2

382

Nume

rical

Inve

stiga

tion

of In

direc

t No

ise G

ener

ation

by A

cceler

ated

Vo

rticit

yW.

Ullri

ch, T

echn

ical U

nivers

ity of

Mun

ich,

Garch

ing, G

erman

y; F.

Bake

, Germ

an

Aeros

pace

Cente

r (DL

R), B

erlin,

Germ

any;

N. Ki

ngs,

Natio

nal C

enter

for S

cienti

fic

Rese

arch (

CNRS

), Ch

âtena

y-Mala

bry,

Franc

e; T.

Satte

lmay

er, Te

chnic

al Un

iversi

ty of

Munic

h, Ga

rching

, Germ

any

1530

hrs

AIAA-2

015-2

383

Exten

sion

of th

e Ran

dom

Parti

cle

Mesh

meth

od to

perio

dic tu

rbule

nt

flows

for f

an br

oadb

and n

oise

pred

iction

A. Wo

hlbran

dt, S

. Gue

rin, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Berl

in, G

erman

y; R.

Ewert

, Germ

an Ae

rospa

ce Ce

nter (

DLR)

, Br

auns

chwe

ig, G

erman

y

1600

hrs

AIAA-2

015-2

384

A stu

dy of

mec

hanis

ms of

soun

d ge

nera

tion

by ai

rfoils

usin

g flow

-ac

ousti

c cor

relat

ions

A. Sa

no, A

. Cav

alieri

, Tec

hnolo

gical

Institu

te of

Aeron

autic

s (ITA

), Sã

o Jos

é do

s Cam

pos,

Braz

il; W.

Wolf

, Univ

ersity

of

Camp

inas,

Camp

inas,

Braz

il

Mond

ay, 2

2 Ju

ne 2

015

42-A

CD-1

Aircr

aft D

esign

for E

nviro

nmen

tal I

mpac

t Red

uctio

nMi

roCh

aired

by: D

. WEL

LS, N

ASA L

angle

y Res

earch

Cente

r14

00 hr

sAIA

A-201

5-238

5Ef

fect

of W

ing Lo

ading

and F

uel

Type

on O

ptim

al Cr

uise A

ltitud

e for

Civ

il Airc

raft

A. Wo

rtman

n, M.

Hoo

greef,

R. Vo

s, De

lft Un

iversi

ty of

Tech

nolog

y, De

lft, Th

e Ne

therla

nds

1430

hrs

AIAA-2

015-2

386

Asse

ssing

Taxii

ng Tr

ade S

pace

s fro

m Ai

rcraf

t, Ai

rpor

t, an

d Airl

ine

Persp

ectiv

esI.

Chak

rabort

y, M.

LeVin

e, M.

Has

san,

D.

Mavri

s, Ge

orgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1500

hrs

AIAA-2

015-2

387

Utilis

ing Se

cond

ary A

irpor

ts fo

r RPT

Op

erat

ions:

A Bu

sines

s Cas

eC.

Bil, A

. Geb

reegz

iabhe

r, RMI

T Univ

ersity

, Me

lbourn

e, Au

strali

a

1530

hrs

AIAA-2

015-2

388

Gree

nhou

se G

as Im

pacts

of O

n-De

mand

Elec

tric A

ircra

ftT.

Thom

pson

, LMI

, McLe

an, V

A

1600

hrs

AIAA-2

015-2

389

Aircr

aft N

oise R

educ

tion

Tech

nolog

y an

d Airp

ort N

oise A

nalys

is fo

r Ge

nera

l Avia

tion

Revit

aliza

tion

S. M

in, D

. Lim

, D. M

avris

, Geo

rgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1630

hrs

AIAA-2

015-2

390

The C

lean

Sky p

rogr

amme

: en

viron

ment

al be

nefit

s at a

ircra

ft lev

elM.

Brun

et, S

. Aub

ry, R.

Lafag

e, ON

ERA,

Toulo

use,

Franc

e

52

Mond

ay, 2

2 Ju

ne 2

015

43-A

FM-3

Unma

nned

Airc

raft

Syste

ms I

Plum

Blos

som

ACh

aired

by: K

. HOF

FLER

, Ada

ptive

Aeros

pace

Grou

p, Inc

. and

S. D

’SOU

ZA, N

ASA-A

RC14

00 hr

sAIA

A-201

5-239

1Ev

aluat

ion of

Ener

gy R

equir

ed

for F

light

by a

UAV F

itted

with

a Va

riable

-Spa

n Wi

ng P

erfo

rming

a Gi

ven

Missi

on P

rofil

eP.

Santo

s, P.

Gamb

oa, U

nivers

ity of

Beir

a Int

erior,

Covil

ha, P

ortug

al

1430

hrs

AIAA-2

015-2

392

Attit

ude a

nd al

titud

e sta

biliza

tion

of qu

ad ro

tor u

sing p

aram

eter

estim

ation

and s

elf-tu

ning

cont

rolle

rT.

Dief,

S. Yo

shida

, Kyu

shu U

nivers

ity,

Kasu

ga, J

apan

; M. A

bdelh

ady,

Cairo

Un

iversi

ty, G

iza, E

gypt

1500

hrs

AIAA-2

015-2

393

Quick

ness

Crite

ria fo

r Lar

ge

Unma

nned

Airc

raft

in No

n-Pr

ecisi

on A

ggre

ssive

and N

on-

Aggr

essiv

e Man

euve

rsK.

Gree

ne, D

. Kun

z, Air

Force

Insti

tute o

f Te

chno

logy,

Wrig

ht-Pa

tterso

n AFB

, OH

1530

hrs

AIAA-2

015-2

394

An A

ssessm

ent o

f Unm

anne

d Ai

rcraf

t Sys

tem Le

vel-T

urn

Mane

uver

Per

form

ance

Re

quire

ment

s In

Relat

ion to

a Qu

antifi

ed W

ell-C

lear D

efinit

ionD.

Jack

, K. H

offler,

S. J

ohns

on, A

dapti

ve

Aeros

pace

Grou

p, Inc

., Ha

mpton

, VA

1600

hrs

AIAA-2

015-2

395

Objec

tive F

uncti

on D

evelo

pmen

t fo

r Opt

imize

d Pat

h Gu

idanc

e for

Ro

torcr

aft S

hipbo

ard R

ecov

ery

J. Tri

tschle

r, Nav

al Air

Sys

tems C

omma

nd,

Patux

ent R

iver, M

D; J.

Horn

, Pen

nsylv

ania

State

Univ

ersity

, Stat

e Coll

ege,

PA

1630

hrs

AIAA-2

015-2

396

Wake

Vorte

x De

tectio

n wi

th U

AV

Close

Form

ation

Fligh

tH.

Chao

, Univ

ersity

of Ka

nsas

, Law

rence

, La

wren

ce, K

S; Y.

Gu,

West

Virgin

ia Un

iversi

ty, M

organ

town,

WV;

P. Tia

n, Z.

Zhen

g, Un

iversi

ty of

Kans

as, L

awren

ce,

Lawr

ence

, KS;

M. N

apoli

tano,

West

Virgin

ia Un

iversi

ty, M

organ

town,

WV

1700

hrs

AIAA-2

015-2

397

Fligh

t Tes

t Eva

luatio

n of

Pilo

t Co

ntro

l Int

erfa

ces f

or R

emot

ely

Pilot

ed Ve

hicles

R. Ol

son,

Natio

nal T

est P

ilot S

choo

l, Mo

jave,

CA

Mond

ay, 2

2 Ju

ne 2

015

44-A

FM-4

Plane

tary

Entry

and A

eroa

ssist

Tech

nolog

yPlu

m Bl

osso

m B

Chair

ed by

: S. D

UTTA

, NAS

A Lan

gley R

esea

rch Ce

nter a

nd C.

KARL

GAAR

D, An

alytic

al Me

chan

ics As

socia

tes In

c14

00 hr

sAIA

A-201

5-239

8Im

prov

emen

ts to

Entry

Term

inal

Point

Cont

rolle

r for

Mar

s At

mosp

heric

Entry

Y. Zh

eng,

H. Cu

i, Y. T

ian, H

arbin

Institu

te of

Tech

nolog

y, Ha

rbin,

China

1430

hrs

AIAA-2

015-2

399

Optim

izatio

n of

Inter

ior P

oint C

ost

Func

tions

Usin

g Ind

irect

Meth

ods

T. An

tony,

M. G

rant,

Purdu

e Univ

ersity

, We

st La

fayett

e, IN

; M. B

olend

er, Ai

r Forc

e Re

searc

h Lab

orator

y, W

right-

Patte

rson

AFB,

OH

1500

hrs

AIAA-2

015-2

401

Rapid

, Rob

ust T

rajec

tory D

esign

Usin

g Ind

irect

Optim

izatio

n Meth

ods

M. Gr

ant, P

urdue

Unive

rsity,

West

Lafay

ette,

IN; M

. Bole

nder,

Air F

orce R

esearc

h La

borat

ory, W

right-

Patte

rson A

FB, O

H

1530

hrs

AIAA-2

015-2

402

Minim

um Te

rmina

l Ene

rgy

Optim

izatio

ns of

Hyp

erson

ic Veh

icles

Using

Indir

ect M

ethod

sM.

Gran

t, Purd

ue Un

iversit

y, We

st La

fayett

e, IN;

M. B

olend

er, Ai

r Forc

e Rese

arch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH

Mond

ay, 2

2 Ju

ne 2

015

45-A

MT-3

/GT-3

Adva

nces

in Te

st Me

thod

ology

and C

FD In

tegra

tion

Obeli

sk B

Chair

ed by

: S. D

UNN,

Jaco

bs Te

chno

logy a

nd S

. COL

E, NA

SA La

ngley

Rese

arch C

enter

1400

hrs

AIAA-2

015-2

403

Deve

lopme

nt of

a Tra

nson

ic Gu

st Ri

g for

Simu

lation

of Ve

rtica

l Gus

ts on

Half

-mod

elsN.

Allen

, M. Q

uinn,

Aircra

ft Re

searc

h As

socia

tion,

Ltd.,

Bedfo

rd, U

nited

King

dom

1430

hrs

AIAA-2

015-2

404

F-35

Conv

entio

nal M

ode J

et-Ef

fects

Te

sting

Meth

odolo

gyM.

McW

aters,

Lock

heed

Mart

in Co

rporat

ion, F

ort W

orth,

TX

1500

hrs

AIAA-2

015-2

405

Motio

n me

asur

emen

t of a

wind

tu

nnel

mode

l by s

tereo

vision

tec

hniqu

eB.

Mart

inez,

D. B

idino

, M. B

astid

e, C.

Deme

autis

, F. L

eopo

ld, P.

Wey

, Fren

ch-

Germ

an Re

searc

h Ins

titute

of Sa

int-Lo

uis

(ISL)

, Sain

t-Lou

is, Fr

ance

1530

hrs

AIAA-2

015-2

406

Expe

rimen

tal In

vesti

gatio

ns ab

out

Heat

Trans

fer Ch

arac

terist

ics of

Irr

egula

r Imp

ingem

ent J

et Ar

rays

in

Typic

al Ac

tive C

leara

nce C

ontro

l Sy

stem

F. Liu,

M. J

unku

i, Nan

jing Un

iversit

y of

Aeron

autics

and A

stron

autics

, Nan

jing, C

hina

Mond

ay, 2

2 Ju

ne 2

015

46-A

MT-4

/GT-4

Surfa

ce an

d Infl

ow Se

nsing

Edelw

eiss

Chair

ed by

: Z. Z

HANG

, Univ

ersity

of Te

nnes

see a

nd T.

IOPP

OLO,

Sou

thern

Metho

dist U

nivers

ity14

00 hr

sAIA

A-201

5-240

7Sh

ear S

tress

Sens

ing w

ith El

astic

Mi

crofe

nce S

tructu

res

A. Cis

otto,

F. Pa

lmier

i, NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA; Y

. Lin,

Na

tiona

l Insti

tute o

f Aero

spac

e, Ha

mpton

, VA

; A. S

aini, J

. Kim

, T. K

im, N

orth C

arolin

a St

ate U

nivers

ity, R

aleigh

, NC;

et al.

1430

hrs

AIAA-2

015-2

408

Deve

lopme

nt of

a So

l-Gel

Base

d Na

nopo

rous

uns

teady

Pre

ssure

Se

nsitiv

e Pain

t and

Valid

ation

in

the L

arge

Tran

sonic

One

ra S2

MA

Wind

tunn

elY.

Mich

ou, B

. Dele

glise

, F. L

ebrun

, ONE

RA,

Moda

ne, F

rance

; E. S

colan

, A. G

rivel,

R.

Steig

er, S

wiss

Cente

r for

Electr

onics

and

Micro

techn

ology

(CSE

M), N

eûch

atel,

Switz

erlan

d; et

al.

1500

hrs

AIAA-2

015-2

409

A Co

unter

-Pro

paga

ting L

aser

Air

Spee

d Sen

sor S

ystem

for A

ircra

ftJ.

Kurtz

, Univ

ersity

of N

ew S

outh

Wales

, Ca

nberr

a, Au

strali

a; S.

Witti

g, OH

B Sy

stem

HB, M

unich

, Germ

any;

S. O

’Byrn

e, Un

iversi

ty of

New

South

Wale

s, Ca

nberr

a, Au

strali

a

1530

hrs

AIAA-2

015-2

410

Comp

utat

ional

Mode

ling o

f Ra

diatio

n Ef

fects

on To

tal

Temp

erat

ure P

robe

sJ.

Reard

on, J

. Sch

etz, K

. Low

e, Vir

ginia

Polyt

echn

ic Ins

titute

and S

tate U

nivers

ity,

Black

sburg

, VA

53

Mond

ay, 2

2 Ju

ne 2

015

47-A

PA-5

Appli

ed CF

D &

Nume

rical

Corre

lation

s with

Expe

rimen

tal D

ata I

Stemm

ons B

Chair

ed by

: D. F

INLE

Y, Lo

ckhe

ed M

artin

Aeron

autic

s and

J. S

LOTN

ICK, B

oeing

Engin

eerin

g Ope

ration

s & Te

chno

logy

1400

hrs

AIAA-2

015-2

411

Supe

rsonic

Pro

jectile

Stee

ring u

sing

Micro

-Actu

ator

s: Ex

perim

enta

l and

Nu

meric

al Stu

dyM.

Libs

ig, B

. Mart

inez,

C. Re

y, T.

Gauth

ier,

P. We

y, C.

Berne

r, Fren

ch-Ge

rman

Rese

arch

Institu

te of

Saint

-Louis

(ISL

), Sa

int-Lo

uis,

Franc

e; et

al.

1430

hrs

AIAA-2

015-2

412

Effe

cts of

Tip C

leara

nce o

n Mi

niatu

re G

as Tu

rbine

s Com

pres

sor

Perfo

rman

ce: A

Num

erica

l Ap

proa

chJ.

Xiang

, J. S

chlut

er, F.

Dua

n, Na

nyan

g Te

chno

logica

l Univ

ersity

, Sing

apore

, Sin

gapo

re

1500

hrs

AIAA-2

015-2

413

Nume

rical

Simula

tion

of W

ater

Sp

ray C

ause

d by a

Roll

ing A

irplan

e Tir

eQ.

Qu,

F. Zh

ang,

P. Liu

, Beih

ang U

nivers

ity,

Beijin

g, Ch

ina; R

. Aga

rwal,

Was

hingto

n Un

iversi

ty in

St. L

ouis,

St.

Louis

, MO

Mond

ay, 2

2 Ju

ne 2

015

48-A

PA-6

Unma

nned

, Bio-

Insp

ired,

Solar

Pow

ered

Aer

ial Ve

hicle

Desig

ns I

Carp

enter

Ball

room

Chair

ed by

: L. U

KEILE

Y, Un

iversi

ty of

Florid

a14

00 hr

sAIA

A-201

5-241

4Co

mput

ation

al Stu

dies f

or th

e De

velop

ment

of a

Hybr

id UA

V/UU

VR.

Rama

murti,

J. G

eder,

D. E

dward

s, T.

Youn

g, Na

val R

esea

rch La

borat

ory,

Wash

ington

, DC

1430

hrs

AIAA-2

015-2

415

Force

Pro

ducti

on by

Wing

Flap

ping:

The R

ole of

Stro

ke A

ngle

of A

ttack

an

d Loc

al Re

ynold

s Num

ber

A. Re

ge, B

. Den

nis, K

. Sub

barao

, Un

iversi

ty of

Texa

s, Arl

ington

, Arlin

gton,

TX 15

00 hr

sAIA

A-201

5-241

6Sy

stem

Deve

lopme

nt fo

r Wild

fire

SUAS

J. Ja

cob,

D. G

abbe

rt, M

. And

alibi,

Ok

lahom

a Stat

e Univ

ersity

, Still

water

, OK

Mond

ay, 2

2 Ju

ne 2

015

49-A

PA-7

Spec

ial Se

ssion

: Aer

odyn

amic-

Struc

tura

l Mod

eling

, Opt

imiza

tion,

and T

est T

echn

iques

for F

lexibl

e Wing

Tech

nolog

y ISte

mmon

s ACh

aired

by: N

. NGU

YEN,

NAS

A-Ame

s Res

earch

Cente

r and

S. A

NDER

S14

00 hr

sAIA

A-201

5-241

7Wi

nd Tu

nnel

Invest

igatio

n of a

Flex

ible

Wing

High

-Lift

Confi

gura

tion w

ith a

Varia

ble Ca

mber

Conti

nuou

s Tra

iling

Edge

Flap

Desi

gnN.

Ngu

yen,

NASA

Ames

Resea

rch Ce

nter,

Moffe

tt Field

, CA;

N. Pr

ecup,

E. Liv

ne,

Unive

rsity o

f Wash

ington

, Sea

ttle, S

eattle

, WA

; J. U

rnes,

The B

oeing

Comp

any,

St.

Louis

, MO;

E. Di

ckey,

The B

oeing

Comp

any,

Hunti

ngton

Beach

, CA;

C. Ne

lson,

The B

oeing

Co

mpan

y, Se

attle,

WA;

et al.

1430

hrs

AIAA-2

015-2

418

Use o

f a Vi

scous

Flow

Simu

lation

Co

de fo

r Sta

tic A

eroe

lastic

Ana

lysis

of a

Wing

at H

igh-Li

ft Co

nditio

nsH.

Akay

din, S

. Moin

i-Yek

ta, J.

Hou

sman

, N.

Ngu

yen,

NASA

Ames

Rese

arch C

enter

, Mo

ffett

Field,

CA

1500

hrs

AIAA-2

015-2

419

Optim

izatio

n of

an A

eros

ervo

elasti

c Wi

ng w

ith D

istrib

uted

Mult

iple

Cont

rol S

urfa

ces

B. S

tanfor

d, NA

SA La

ngley

Rese

arch

Cente

r, Ham

pton,

VA

1530

hrs

AIAA-2

015-2

420

Adap

tive A

eroe

lastic

Wing

Sh

ape O

ptim

izatio

n fo

r High

-Lift

Confi

gura

tions

G. Fu

jiwara

, Univ

ersity

of W

ashin

gton,

Seatt

le, S

eattle

, WA;

N. N

guye

n, NA

SA

Ames

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1600

hrs

AIAA-2

015-2

421

Robu

st Op

timiza

tion

of Va

riable

-Ca

mber

Cont

inuou

s Tra

iling-

Edge

Fla

p Sys

tem A

ction

Usin

g Sto

chas

tic

Krigi

ngY.

Liu, J

. Bai,

Nort

hwes

tern P

olytec

hnica

l Un

iversi

ty, X

i’an,

China

; E. L

ivne,

Unive

rsity

of Wa

shing

ton, S

eattle

, Se

attle,

WA

1630

hrs

AIAA-2

015-2

422

A 3-

D Dr

ag O

ptim

izatio

n Stu

dy

of Va

riable

Camb

er Co

ntinu

ous

Trailin

g Edg

e Flap

(VCC

TEF)

Usin

g OV

ERFL

OWU.

Kaul,

N. N

guye

n, NA

SA Am

es Re

searc

h Ce

nter, M

offett

Field

, CA

54

Mond

ay, 2

2 Ju

ne 2

015

50-A

PA-8

Flow

Cont

rol A

pplic

ation

s & D

emon

strat

ions (

Activ

e & P

assiv

e) I

Stemm

ons C

Chair

ed by

: J. G

EORG

E, Me

trolas

er Inc

. and

K. M

ULLE

NERS

, Leib

niz U

nivers

itaet

Hann

over

1400

hrs

AIAA-2

015-2

423

Study

of sla

nted p

erfor

ated s

hape

s in

tabs f

or co

ntrol

of su

bson

ic Jets

A. Re

yaz A

hmed

, KCG

Colleg

e of T

echno

logy,

Chen

nai, I

ndia;

S. Th

aniga

iarasu

, Mad

ras

Institu

te of

Techn

ology,

Chen

nai, I

ndia;

S.

Venk

atram

an, K

CG Co

llege o

f Tech

nolog

y, Ch

enna

i, Ind

ia; E.

Sriniv

asan,

Bhara

th Un

iversit

y, Ch

enna

i, Ind

ia; E.

Ratha

krishn

an,

Indian

Instit

ute of

Techn

ology

Kanp

ur, Ka

npur,

Ind

ia

1430

hrs

AIAA-2

015-2

424

Nume

rical

Study

of th

e Int

erna

l Flo

w Str

uctu

res I

nside

the S

weep

ing

Jet A

ctuat

orK.

Kara,

Khali

fa Un

iversi

ty, Ab

u Dha

bi,

Unite

d Arab

Emira

tes

1500

hrs

AIAA-2

015-2

425

Effe

ct of

Span

wise

Jet S

pacin

g on

Sepa

ratio

n Co

ntro

l for

Swep

t and

Un

swep

t Airf

oils

M. W

alker,

K. H

ipp, S

. Ben

ton, J

. Bon

s, Oh

io St

ate U

nivers

ity, C

olumb

us, O

H

1530

hrs

AIAA-2

015-2

426

Dyna

mic F

low Co

ntro

l ove

r Ae

rody

nami

c Bod

ies u

sing P

hase

d Ar

ray V

ecto

red S

ynth

etic J

et Ac

tuat

ionZ.

Hasn

ain, R

. Wein

stein,

L. Tr

olling

er,

J. Hu

bbard

, A. F

latau

, Univ

ersity

of

Maryl

and,

Colle

ge Pa

rk, Co

llege

Park,

MD

1600

hrs

AIAA-2

015-2

427

Stoch

astic

analy

sis of

aero

dyna

mic

force

s acti

ng on

a se

lf-ad

aptiv

e ca

mber

airfo

il in

turb

ulent

inflo

wG.

Kamp

ers, C

arl vo

n Ossi

etzky

Univ

ersity

, Ol

denb

urg, G

erman

y; U.

Corde

s, C.

Trope

a, Te

chnic

al Un

iversi

ty of

Darm

stadt,

Da

rmsta

dt, G

erman

y; M.

Hoe

lling,

J. Pe

inke,

Carl v

on O

ssietz

ky U

nivers

ity,

Olde

nburg

, Germ

any

Mond

ay, 2

2 Ju

ne 2

015

51-A

TIO-5

Term

inal &

Surfa

ce O

pera

tions

IIMa

nche

ster

Chair

ed by

: A. S

ARAF

, Saa

b Sen

sis Co

rporat

ion14

00 hr

sAIA

A-201

5-242

8Sc

hedu

ling a

nd D

elive

ring A

ircra

ft to

Dep

artu

re Fi

xes i

n th

e NY

Metro

plex

with

Cont

rolle

r-Man

aged

Sp

acing

Tools

E. Ch

evall

ey, B

. Park

e, J.

Kraut,

N.

Biene

rt, F.

Oma

r, E. P

almer,

NAS

A Ame

s Re

searc

h Cen

ter, M

offett

Field

, CA

1430

hrs

AIAA-2

015-2

429

Stoch

astic

Nea

r-Opt

imal

Cont

rol

for A

ircra

ft Ar

rival

Sequ

encin

g and

Co

nflict

Res

olutio

nY.

Matsu

no, T

. Tsu

chiya

, Univ

ersity

of

Toky

o, Bu

nkyo

, Jap

an

1500

hrs

AIAA-2

015-2

430

Time B

ased

Sepa

ratio

n: A

stud

y int

o run

way c

ompr

essio

n an

d tim

e ba

sed s

epar

ation

R. Cu

rran,

F. He

rrema

, W. Z

hao,

Delft

Unive

rsity

of Te

chno

logy,

Delft,

The

Nethe

rland

s; V.

Treve

, R. G

raham

, EU

ROCO

NTRO

L, Br

etign

y, Fra

nce

1530

hrs

AIAA-2

015-2

431

Desig

ning a

nd Ev

aluat

ing A

dvan

ced

Appr

oach

Pro

cedu

res f

or th

e Co

ncep

t of S

egme

nted

Inde

pend

ent

Para

llel A

ppro

ache

sC.

Hans

es, F

. Kna

be, B

. Korn

, Germ

an

Aeros

pace

Cente

r (DL

R), B

rauns

chwe

ig,

Germ

any

1600

hrs

AIAA-2

015-2

432

Optim

al Ai

rspac

e Des

ign fo

r Co

ntinu

ous C

limb O

pera

tion

E. Kim

, S. H

ong,

K. Le

e, Ko

rea Ae

rospa

ce

Unive

rsity,

Goy

ang,

South

Korea

1630

hrs

AIAA-2

015-2

433

Asse

ssmen

t of D

elaye

d De

celer

ation

App

roac

h Op

portu

nities

at U

S Airp

orts

T. Re

ynold

s, M.

McP

artlan

d, Y.

Rodri

guez

, M.

San

dberg

, J. V

enuti

, Linc

oln La

borat

ory,

Massa

chus

etts I

nstitu

te of

Tech

nolog

y, Le

xingto

n, MA

Mond

ay, 2

2 Ju

ne 2

015

52-A

TIO-6

Fleet

and R

oute

Plann

ingMi

ngCh

aired

by: W

. CRO

SSLE

Y, Pu

rdue U

nivers

ity14

00 hr

sAIA

A-201

5-243

4Ef

fects

of Fu

el Pr

ice on

Tota

l Fue

l Bu

rn an

d Sys

tem Ca

pacit

y- A

n An

alysis

of A

dvan

ced E

ngine

and

Airfr

ame T

echn

ology

and A

irline

Re

spon

ses t

o Cha

nges

in Fu

el Pr

iceC.

Murph

y, B.

Mille

r, Metr

on Av

iation

, Inc

., Du

lles,

VA; L

. She

rry, G

eorge

Mas

on

Unive

rsity,

Fairfa

x, VA

1430

hrs

AIAA-2

015-2

435

Estim

ating

the F

uel S

aving

Po

tentia

l of C

omme

rcial

Aircr

aft

in Fu

ture

Flee

t-Dev

elopm

ent

Scen

arios

N. Ra

ndt,

L. Wa

che,

Tech

nical

Unive

rsity

of Mu

nich,

Munic

h, Ge

rman

y; C.

Jessb

erger,

K.

Ploetn

er, B

auha

us Lu

ftfah

rt e.V

., Mu

nich,

Germ

any

1500

hrs

AIAA-2

015-2

436

Enab

ling T

echn

ology

Por

tfolio

Se

lectio

n th

roug

h Qu

antit

ative

Un

certa

inty A

nalys

isK.

Gatia

n, D.

Mav

ris, G

eorgi

a Ins

titute

of Te

chno

logy,

Atlan

ta, G

A

1530

hrs

AIAA-2

015-2

437

A Ra

pid In

tegra

ted In

terde

pend

ent

Fleet-

Leve

l Env

ironm

enta

l Mod

elJ.

Berna

rdo, T

. Zaid

i, M. L

eVine

, H.

Jimen

ez, D

. Mav

ris, G

eorgi

a Ins

titute

of Te

chno

logy,

Atlan

ta, G

A

1600

hrs

AIAA-2

015-2

438

Mode

ling A

irline

Dec

ision

s on

Rout

e Pla

nning

Usin

g Disc

rete

Choic

e Mo

dels

Z. Sh

a, K.

Moolc

hand

ani, A

. Mah

eshw

ari,

J. Th

ekine

n, J.

Panc

hal, D

. DeL

auren

tis,

Purdu

e Univ

ersity

, Wes

t Lafa

yette

, IN

1630

hrs

AIAA-2

015-2

439

Land

scape

Ana

lysis

Fram

ewor

k fo

r Lo

w Ca

rbon

Ener

gyP.

Vasci

k, Ma

ssach

usett

s Ins

titute

of Te

chno

logy,

Camb

ridge

, MA;

R. Pe

arce,

NASA

Hea

dqua

rters,

Was

hingto

n, DC

; D.

Rhod

es, M

assa

chus

etts I

nstitu

te of

Tech

nolog

y, Ca

mbrid

ge, M

A

Mond

ay, 2

2 Ju

ne 2

015

53-A

TIO-7

Syste

ms En

ginee

ring a

nd A

nalys

isMi

lanCh

aired

by: P

. HOL

LINGS

WOR

TH, T

he U

nivers

ity of

Man

ches

ter14

00 hr

sAIA

A-201

5-244

0Kn

owled

ge En

ginee

ring -

Fo

rmali

zing t

he En

ginee

ring

Scien

ce D

iscipl

ineX.

Peng

, B. C

hudo

ba, U

nivers

ity of

Texa

s, Arl

ington

, Arlin

gton,

TX

1430

hrs

AIAA-2

015-2

441

Pavin

g the

Way

from

the P

ast t

o th

e Fut

ure:

AVDKB

S , a So

ftwar

e De

velop

ment

in K

nowl

edge

En

ginee

ring

X. Pe

ng, B

. Chu

doba

, Univ

ersity

of Te

xas,

Arling

ton, A

rlingto

n, TX

1500

hrs

AIAA-2

015-2

442

Para

metri

c Asse

ssmen

t of A

viatio

n En

viron

ment

al Go

als: I

mplic

ation

s on

R&D

Dec

ision

Mak

ingM.

Has

san,

A. Pa

yan,

S. O

’Sull

ivan,

H.

Pfaen

der, D

. Mav

ris, G

eorgi

a Ins

titute

of Te

chno

logy,

Atlan

ta, G

A

1530

hrs

AIAA-2

015-2

443

Selec

ted A

rray o

f Tec

hnolo

gy an

d Sy

stems

Opt

ions f

or Ec

ologic

ally

Resp

onsib

le Av

iation

A. Isi

kvere

n, D.

Empl,

U. K

ling,

K. Plo

etner,

C. Po

rnet,

Bauh

aus L

uftfah

rt e.V

., Ot

tobrun

n, Ge

rman

y

55

Mond

ay, 2

2 Ju

ne 2

015

54-A

TIO-8

14

00 -

1600

hrs

Trans

form

ation

al Fli

ght -

Enab

ling t

he N

ext B

illion

Doll

ar A

viatio

n Ma

rket

thro

ugh

Auto

nomy

Metro

polita

n Ba

llroo

m

Mode

rator:

Mark

Ball

in, N

ASA L

angle

y Res

earch

Cente

r

Pan

elists

:Da

nette

Alle

nAu

tonom

y Inc

ubato

r, NAS

A Lan

gley R

esea

rch Ce

nter

Nick

Roy

MIT

Craig

Woo

lsey

Virgin

ia Te

ch

Mond

ay, 2

2 Ju

ne 2

015

55-C

FD-5

Unstr

uctu

red H

igh-O

rder

Meth

ods I

IGr

and B

allro

om A

Chair

ed by

: H. H

UYNH

, NAS

A Glen

n Res

earch

Cente

r and

A. JA

MESO

N, Ae

ronau

tics a

nd As

trona

utics

1400

hrs

AIAA-2

015-2

444

A Su

rvey

of th

e Ise

ntro

pic Eu

ler

Vorte

x Pr

oblem

usin

g High

-Ord

er

Meth

ods

S. S

piege

l, H. H

uynh

, J. D

eBon

is, N

ASA

Glenn

Rese

arch C

enter

, Clev

eland

, OH

1430

hrs

AIAA-2

015-2

445

High

-Ord

er H

yper

bolic

Res

idual-

Distr

ibutio

n Sc

heme

s on

Arbit

rary

Tri

angu

lar G

rids

A. Ma

zahe

ri, NA

SA La

ngley

Rese

arch

Cente

r, Ham

pton,

VA; H

. Nish

ikawa

, Na

tiona

l Insti

tute o

f Aero

spac

e, Ha

mpton

, VA

1500

hrs

AIAA-2

015-2

446

High

-Ord

er M

ethod

s for

Co

nser

vatio

n La

ws Em

ployin

g Em

bedd

ed St

ructu

red E

lemen

t Me

thod

on U

nstru

cture

d He

xahe

dral

Grid

J. Ch

oi, U

nivers

ity of

Mary

land,

Colle

ge

Park,

Colle

ge Pa

rk, M

D

1530

hrs

AIAA-2

015-2

447

Stabil

izatio

n of

High

-Ord

er

Meth

ods f

or U

nstru

cture

d Grid

s wi

th Lo

cal F

ourie

r Spe

ctral

Filter

ing: h

igh-R

e Sim

ulatio

ns in

Co

arse

Mes

hes

M. Ló

pez-M

orales

, A. J

ames

on, S

tanfor

d Un

iversi

ty, S

tanfor

d, CA

1600

hrs

AIAA-2

015-2

448

A Cla

ss of

Ros

enbr

ock

Meth

ods

for a

Rec

onstr

ucted

Disc

ontin

uous

Ga

lerkin

Meth

od fo

r the

Uns

teady

Co

mpre

ssible

Flow

sX.

Liu,

H. Lu

o, No

rth Ca

rolina

Stat

e Un

iversi

ty, Ra

leigh

, NC;

Y. Xia

, Ida

ho

Natio

nal L

abora

tory,

Idaho

Falls,

ID

Mond

ay, 2

2 Ju

ne 2

015

56-C

FD-6

Nove

l Disc

retiz

ation

sGr

and B

allro

om B

Chair

ed by

: J. E

KATE

RIN, I

ACM

and M

. CHO

UDHA

RI, N

ASA-L

angle

y Res

earch

Cente

r14

00 hr

sAIA

A-201

5-244

9In

vesti

gatio

ns of

a Ne

w Sc

heme

for

Wave

Pro

paga

tion

D. Fa

n, P.

Roe,

Unive

rsity

of Mi

chiga

n, An

n Arb

or, An

n Arbo

r, MI

1430

hrs

AIAA-2

015-2

450

Activ

e Flux

for A

dvec

tion

Diffu

sion

H. N

ishika

wa, N

ation

al Ins

titute

of Ae

rospa

ce, H

ampto

n, VA

1500

hrs

AIAA-2

015-2

451

Alter

nativ

e For

mulat

ions f

or

First-

, Sec

ond-

, and

Third

-Ord

er

Hype

rboli

c Nav

ier-S

toke

s Sch

emes

H. N

ishika

wa, N

ation

al Ins

titute

of Ae

rospa

ce, H

ampto

n, VA

1530

hrs

AIAA-2

015-2

452

Rece

nt P

rogr

esse

s on

a Mes

hless

Euler

Solve

r for

Comp

ressi

ble Fl

ows

Z. Du

an, Z

. Wan

g, Un

iversi

ty of

Kans

as,

Lawr

ence

, Law

rence

, KS;

B. V

u, NA

SA

Kenn

edy S

pace

Cente

r, Cap

e Can

avera

l, FL

1600

hrs

AIAA-2

015-2

453

A Ve

rsatile

Non

linea

r Pre

dictiv

e Mo

delin

g App

roac

hM.

Liou

, NAS

A Glen

n Res

earch

Cente

r, Cle

velan

d, OH

; W. Y

ao, Q

ueen

’s Un

iversi

ty,

Belfa

st, U

nited

King

dom

1630

hrs

AIAA-2

015-2

454

Dyna

mica

l sele

ctive

filte

ring f

or th

e La

ttice

Bolt

zman

n Me

thod

S. M

arie,

Natio

nal C

onse

rvator

y of A

rts

and C

rafts,

Paris

, Fran

ce; X

. Gloe

rfelt,

Paris

Insti

tute o

f Tec

hnolo

gy, P

aris,

Franc

e

Mond

ay, 2

2 Ju

ne 2

015

57-C

FD-7

Inter

discip

linar

y CFD

ICo

ral

Chair

ed by

: L. M

ARTIN

ELLI,

Princ

eton U

nivers

ity an

d S. E

YI, M

iddle

East

Tech

nical

Unive

rsity

1400

hrs

AIAA-2

015-2

455

CFD-

base

d Gus

t Loa

d Ana

lysis

for

a Fre

e-fly

ing Fl

exibl

e Pas

seng

er

Aircr

aft i

n Co

mpar

ison

to a

DLM-

base

d App

roac

hL.

Reim

er, M

. Ritte

r, R. H

einric

h, W.

Krü

ger, G

erman

Aeros

pace

Cente

r (DL

R),

Brau

nsch

weig,

Germ

any

1430

hrs

AIAA-2

015-2

456

Influ

ence

of W

all Vi

brat

ion on

the

Aero

Per

form

ance

of Tr

anso

nic

Diffu

ser

C. Ya

o, G.

Zhan

g, F.

Xu, Z

. Liu,

Harb

in Ins

titute

of Te

chno

logy,

Harbi

n, Ch

ina

1500

hrs

AIAA-2

015-2

457

Nume

rical

Analy

sis of

Synt

hetic

Jet

in Cr

ossfl

owA.

Gupte

, A. P

radee

p, P.

Mujum

dar, I

ndian

Ins

titute

of Te

chno

logy B

omba

y, Mu

mbai,

Ind

ia

1530

hrs

AIAA-2

015-2

458

Perfo

rman

ces o

f New

ton

and

Prec

ondit

ioned

New

ton-

GMRE

S Me

thod

s in

Hype

rsonic

Flow

So

lution

sY.

Muslu

bas,

S. Ey

i, Midd

le Ea

st Te

chnic

al Un

iversi

ty, An

kara,

Turke

y

56

Mond

ay, 2

2 Ju

ne 2

015

58-C

FD-8

Turb

ulenc

e Mod

eling

and U

ncer

taint

y Qua

ntifi

catio

nEm

erald

Chair

ed by

: D. Y

ODER

, NAS

A Glen

n Res

earch

Cente

r and

K. D

URAIS

AMY,

Stan

ford U

nivers

ity14

00 hr

sAIA

A-201

5-245

9Qu

antifi

catio

n of

Turb

ulenc

e Mo

delin

g Unc

erta

inties

Usin

g Full

Fie

ld In

versi

onE.

Paris

h, K.

Durai

samy

, Univ

ersity

of

Mich

igan,

Ann A

rbor, A

nn Ar

bor, M

I

1430

hrs

AIAA-2

015-2

460

Mach

ine Le

arnin

g Meth

ods f

or

Data

-Driv

en Tu

rbule

nce M

odeli

ngZ.

Zhan

g, K.

Durai

samy

, Univ

ersity

of

Mich

igan,

Ann A

rbor, A

nn Ar

bor, M

I

1500

hrs

AIAA-2

015-2

461

Uncer

tainty

Qua

ntific

ation

of

Turb

ulenc

e Mod

el Clo

sure

Coeffi

cients

for

Tran

sonic

Wall

-Bou

nded

Flow

sJ.

Scha

efer, T

. West

, S. H

osder,

Miss

ouri

Unive

rsity o

f Scie

nce an

d Tech

nolog

y, Ro

lla,

MO; C

. Rum

sey, J

. Carl

son, W

. Kleb

, NAS

A La

ngley

Resea

rch Ce

nter, H

ampto

n, VA

1530

hrs

AIAA-2

015-2

462

A Sc

ale-A

dapt

ive Va

riant

of th

e Sp

alart-

Allm

aras

Eddy

-Visc

osity

Mo

del

J. Co

der, P

enns

ylvan

ia St

ate U

nivers

ity,

State

Colle

ge, P

A

1600

hrs

AIAA-2

015-2

463

PANS

Simu

lation

s of T

urbu

lent

Sepa

rated

Flow

over

a Wa

ll-mo

unted

Hum

pD.

Higu

era Ca

ubilla

, Univ

ersity

of To

ulous

e, To

ulous

e, Fra

nce;

P. Ra

zi, Te

xas A

&M

Unive

rsity,

Colle

ge S

tation

, TX;

S. S

ekha

r, N.

Man

sour,

NAS

A Ame

s Res

earch

Cente

r, Mo

ffett

Field,

CA; S

. Girim

aji, T

exas

A&M

Unive

rsity,

Colle

ge S

tation

, TX

1630

hrs

AIAA-2

015-2

464

A log

arith

mic f

ormu

lation

for

low-R

eyno

lds n

umbe

r tur

bulen

ce

mode

ls wi

th ad

aptiv

e wall

-func

tions

L. Fra

zza,

A. Ha

y, D.

Pelle

tier, É

cole

Polyt

echn

ique d

e Mon

tréal,

Mon

tréal,

Ca

nada

Mond

ay, 2

2 Ju

ne 2

015

59-F3

60-2

/CAS

E-2

1400

- 17

00 h

rsWh

atev

er H

appe

ned t

o the

Four

-Year

Airp

lane?

Gran

d Ball

room

E

Mode

rator:

Craig

Willi

s, Gr

oup H

ead f

or Sy

stems

Verifi

catio

n, Gu

lfstre

am G

500/

G600

Prog

ram, G

ulfstr

eam

Aeros

pace

Corpo

ration

P

aneli

sts:

Cath

erine

Ferri

e Kilm

ainEx

ecuti

ve V

ice Pr

eside

nt of

Engin

eerin

gBe

ll Heli

copte

r

Eric

Schr

ock

Depu

ty Dir

ector

, Tec

hnolo

gy D

evelo

pmen

t and

Prod

uct I

ntegra

tion

Lock

heed

Mart

in Co

rporat

ion

Mond

ay, 2

2 Ju

ne 2

015

60-FD

-6/P

DL-2

Plasm

a Aer

odyn

amics

& Fl

ow Co

ntro

l II

Gove

nors

Lectu

re H

allCh

aired

by: D

. WILL

IAMS,

Illino

is Ins

titute

of Te

chno

logy a

nd J.

LITT

LE, T

he U

nivers

ity of

Arizo

na14

00 hr

sAIA

A-201

5-246

5PI

V and

Elec

tric C

hara

cteriz

ation

of

a Plas

ma Sy

nthe

tic Je

t Actu

ator

F. La

urend

eau,

F. Ch

edev

ergne

, O. L

éon,

ONER

A, To

ulous

e, Fra

nce

1430

hrs

AIAA-2

015-2

466

Adjoi

nt O

ptim

izatio

n of

the S

patia

l Pr

ofile

of St

eady

Ener

gy D

epos

ition

for S

uper

sonic

Dra

g Red

uctio

nR.

Miles

, C. L

imba

ch, P

rince

ton U

nivers

ity,

Princ

eton,

NJ

1500

hrs

AIAA-2

015-2

467

Mode

ling o

f Saw

-toot

h DB

D Pla

sma A

ctuat

ors f

or Fl

ow Co

ntro

l Sim

ulatio

nsP.

Milan

, F. D

emers

, H. V

o, Éc

ole

Polyt

echn

ique d

e Mon

tréal,

Mon

tréal,

Ca

nada

1530

hrs

AIAA-2

015-2

468

Ns-D

BD pl

asma

actu

ator

indu

ced

dens

ity gr

adien

t on

a lam

inar

boun

dary

laye

rR.

Wink

el, G

. Corr

eale,

Delf

t Univ

ersity

of

Tech

nolog

y, De

lft, Th

e Neth

erlan

ds

1600

hrs

AIAA-2

015-2

469

Contr

ibutio

n of la

rge-s

cale

vorte

x an

d fine

-scale

turb

ulent

struc

ture i

n sep

arate

d flow

contr

ol us

ing D

BD

plasm

a actu

ator

K. As

ano,

Unive

rsity o

f Tok

yo, S

agam

ihara,

Jap

an; K

. Asad

a, Oh

io Sta

te Un

iversit

y, Co

lumbu

s, OH

; H. K

ato, U

nivers

ity of

Toky

o, Sa

gami

hara,

Japa

n; M.

Sato,

T. N

onom

ura,

K. Fu

jii, Jap

an Ae

rospa

ce Ex

plorat

ion Ag

ency

(JAXA

), Sa

gami

hara,

Japa

n

1630

hrs

AIAA-2

015-2

470

Flow

cont

rol o

ver a

back

ward

fa

cing s

tep by

ns-D

BD pl

asma

ac

tuat

orG.

Corre

ale, D

elft U

nivers

ity of

Tech

nolog

y, De

lft, Th

e Neth

erlan

ds

Mond

ay, 2

2 Ju

ne 2

015

61-FD

-7Bo

unda

ry La

yer T

rans

ition

- Pro

gres

s and

Chall

enge

sSa

pphir

eCh

aired

by: M

. MAL

IK, N

ASA-L

angle

y Res

earch

Cente

r and

M. R

OGER

S, N

ASA-A

mes R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-2

471

Rece

ptivi

ty: T

he In

spira

tion o

f Mar

k Mo

rkov

in (In

vited

)H.

Reed

, W. S

aric,

Texa

s A&M

Univ

ersity

, Co

llege

Stat

ion, T

X

1430

hrs

AIAA-2

015-2

472

Boun

dary

-Laye

r Tra

nsitio

n Pr

edict

ion fo

r Lam

inar F

low Co

ntro

l (In

vited

)J.

Crouch

, The

Boein

g Com

pany,

Seatt

le, W

A

1500

hrs

Oral

Prese

ntatio

nHy

perso

nic B

ound

ary-

Laye

r Tra

nsitio

n: To

ward

s Mec

hanis

m-Ba

sed P

redic

tion

Meth

ods (

Invit

ed)

S. S

chne

ider, P

urdue

Univ

ersity

, Wes

t La

fayett

e, IN

1530

hrs

AIAA-2

015-2

473

Rece

ptivi

ty of

Hyp

erso

nic B

ound

ary

Laye

rs to

Aco

ustic

and V

ortic

al Di

sturb

ance

s (In

vited

)P.

Balak

umar,

NAS

A Lan

gley R

esea

rch

Cente

r, Ham

pton,

VA

1600

hrs

AIAA-2

015-2

474

Exten

ding t

he G

amma

-Reth

etat

Corre

lation

base

d Tra

nsitio

n Mo

del

for C

rossfl

ow Ef

fects

(Inv

ited)

R. La

ngtry

, The

Boein

g Com

pany,

Seatt

le, W

A

1630

hrs

AIAA-2

015-2

475

CFD

Trans

ition

Mode

ling:

Blen

ding

Classi

cal M

ethod

s with

Mod

ern

Tools

(Inv

ited)

J. Co

der, M

. Mau

ghme

r, Pen

nsylv

ania

State

Univ

ersity

, Stat

e Coll

ege,

PA

1700

hrs

AIAA-2

015-2

476

Deve

lopme

nt an

d App

licat

ion of

Tra

nsitio

n Pr

edict

ion Te

chniq

ues i

n an

Uns

tructu

red C

FD Co

de (I

nvite

d)A.

Krumb

ein, N

. Krim

melbe

in, C.

Grab

e, Ge

rman

Aeros

pace

Cente

r (DL

R), C

ologn

e, Ge

rman

y

57

Mond

ay, 2

2 Ju

ne 2

015

62-FD

-8Vo

rtex

Flows

Sena

tors

Lectu

re H

allCh

aired

by: Z

. ZHE

NG, T

he U

nivers

ity of

Kans

as an

d R. G

ORDN

IER, A

ir Forc

e Res

each

Labo

ratory

1400

hrs

AIAA-2

015-2

477

Vorte

x Br

eakd

own

of Co

mpre

ssible

Sw

irling

Flow

s in

a Fini

te-Le

ngth

Str

aight

Circu

lar P

ipeZ.

Rusa

k, J.

Choi,

Rens

selae

r Poly

techn

ic Ins

titute,

Troy

, NY;

S. W

ang,

Unive

rsity

of Au

cklan

d, Au

cklan

d, Ne

w Ze

aland

1430

hrs

AIAA-2

015-2

478

Nume

rical

Study

of th

e For

matio

n of

Conc

entri

c Vor

tex R

ings

V. Sa

dri, P

. Krue

ger, S

outhe

rn Me

thodis

t Un

iversi

ty, D

allas

, TX

1500

hrs

AIAA-2

015-2

479

Rota

ting C

ylind

rical

Bodie

s at

Low

ReM.

Calle

nder,

Midd

le Te

nnes

see S

tate

Unive

rsity,

Murf

reesb

oro, T

N

1530

hrs

AIAA-2

015-2

480

Inve

stiga

tion

of th

e flow

dyna

mics

in a c

hann

el co

nstri

cted b

y per

iodic

hills

X. G

loerfe

lt, Pa

ris In

stitut

e of T

echn

ology

, Pa

ris, F

rance

; P. C

innell

a, Un

iversi

ty of

Salen

to, Le

cce, I

taly

1600

hrs

AIAA-2

015-2

481

Tempo

ral E

volut

ion of

Turb

ulent

Eddie

s in

a Com

press

ible J

et in

Crossfl

ow

Meas

ured

using

Pulse

-Bur

st PIV

S. B

eresh

, J. W

agne

r, J. H

enflin

g, R.

Spille

rs, B

. Prue

tt, S

andia

Nati

onal

Labo

ratori

es, A

lbuqu

erque

, NM

Mond

ay, 2

2 Ju

ne 2

015

63-FD

-9Ac

tive a

nd P

assiv

e Flow

Cont

rol

Topa

zCh

aired

by: K

. GRA

NLUN

D, Ai

r Forc

e Res

earch

Labo

ratory

and M

. AMI

TAY, R

ensse

laer P

olytec

hnic

Institu

te14

00 hr

sAIA

A-201

5-248

2In

terac

tions

of a

Dyna

mic V

ortex

Ge

nera

tor w

ith a

Cros

s-flow

: A

Nume

rical

Study

R. Cu

mming

s, Re

nsse

laer P

olytec

hnic

Institu

te, Tr

oy, N

Y; D.

Cling

man,

The

Boein

g Com

pany

, Sea

ttle, W

A; O.

Sah

ni,

Rens

selae

r Poly

techn

ic Ins

titute,

Troy

, NY

1430

hrs

AIAA-2

015-2

483

Inter

actio

ns of

a Dy

nami

c Vor

tex

Gene

rato

r with

a Cr

oss-fl

ow: A

n Ex

perim

enta

l Stu

dyC.

Leon

g, E.

Cruz,

Rens

selae

r Poly

techn

ic Ins

titute,

Troy

, NY;

D. Cl

ingma

n, Th

e Bo

eing C

ompa

ny, S

eattle

, WA;

M. Am

itay,

Rens

selae

r Poly

techn

ic Ins

titute,

Troy

, NY

1500

hrs

AIAA-2

015-2

484

Flow

Cont

rol in

a Di

ffuse

r at

Trans

onic

Cond

itions

J. Ga

rtner,

M. A

mitay

, Ren

sselae

r Po

lytec

hnic

Institu

te, Tr

oy, N

Y

1530

hrs

AIAA-2

015-2

485

The E

ffects

of Sw

eepin

g Jet

Actu

ator

Par

amete

rs on

Flow

Se

para

tion

Cont

rol

M. Ko

klu, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

Mond

ay, 2

2 Ju

ne 2

015

64-M

AO-2

Vehic

le De

sign

Appli

catio

ns II

Madr

idCh

aired

by: S

. CHO

I, Vir

ginia

Polyt

echn

ic Ins

titute

and S

tate U

nivers

ity an

d S. F

ERGU

SON,

Nort

h Caro

lina S

tate U

nivers

ity14

00 hr

sAIA

A-201

5-248

6Th

e Valu

e of S

emi-E

mpiri

cal

Analy

sis M

odels

in A

ircra

ft De

sign

S. B

randt,

M. P

ost,

U.S.

Air F

orce

Acad

emy,

Color

ado S

pring

s, CO

; D. H

all,

DHC E

ngine

ering

, San

Mate

o, CA

; F.

Gillia

m, Li

psco

mb U

nivers

ity, N

ashv

ille,

TN; T

. Jun

g, T.

Yech

out,

U.S.

Air F

orce

Acad

emy,

Color

ado S

pring

s, CO

1430

hrs

AIAA-2

015-2

487

Coup

led A

djoint

Aer

ostru

ctura

l Wi

ng O

ptim

izatio

n Us

ing Q

uasi-

Thre

e-Di

mens

ional

Aero

dyna

mic

Analy

sisA.

Elham

, Delf

t Univ

ersity

of Te

chno

logy,

Delft,

The N

etherl

ands

; M. v

an To

oren,

Unive

rsity

of So

uth Ca

rolina

, Colu

mbia,

Co

lumbia

, SC

1500

hrs

AIAA-2

015-2

488

Optim

al va

riable

stiff

ness

distri

butio

n fo

r a co

mpos

ite pl

ate

with

a ro

w of

hole

s sub

jected

to

tensio

n/sh

ear l

oad c

ases

M. va

n Too

ren, U

nivers

ity of

Sou

th Ca

rolina

, Colu

mbia,

Colum

bia, S

C; A.

Elham

, Delf

t Univ

ersity

of Te

chno

logy,

Delft,

The N

etherl

ands

; R. H

arik,

Unive

rsity

of So

uth Ca

rolina

, Colu

mbia,

Colum

bia, S

C

1530

hrs

AIAA-2

015-2

489

Simula

tion-

Base

d Opt

imal

Sens

or/

Actu

ator

Pos

itionin

g on

a Fin-

Like

Struc

ture

N. Pe

drama

sl, M

. Sah

in, M

iddle

East

Tech

nical

Unive

rsity,

Cank

aya,

Turke

y; E.

Acar,

TOBB

Univ

ersity

of Ec

onom

ics an

d Te

chno

logy,

Sogu

tozu,

Turke

y

1600

hrs

AIAA-2

015-2

490

Conc

urre

nt O

ptim

izatio

n of

a Fe

ed-Fo

rwar

d Gus

t Loa

ds Co

ntro

ller

and M

inimi

zatio

n of

Wing

Box

Str

uctu

ral M

ass o

n an

Airc

raft

with

Ac

tive W

inglet

sA.

Wild

schek

, Airb

us, O

ttobru

nn, G

erman

y

1630

hrs

AIAA-2

015-2

491

Free

-Form

Aer

odyn

amic

Wing

Op

timiza

tion U

sing M

athe

matic

ally-

Deriv

ed D

esign

Varia

bles

D. Po

ole, C

. Alle

n, T.

Rend

all, U

nivers

ity of

Br

istol,

Bris

tol, U

nited

King

dom

Mond

ay, 2

2 Ju

ne 2

015

65-M

ST-3

Air T

raffi

c Man

agem

ent

Trave

rtine

Chair

ed by

: J. S

MITH

1400

hrs

AIAA-2

015-2

492

Scala

ble M

ultidi

mens

ional

Unce

rtaint

y Eva

luatio

n Ap

proa

ch

to St

rateg

ic Ai

r Tra

ffic F

low

Mana

geme

ntJ.

Xie, Y

. Wan

, Univ

ersity

of N

orth T

exas

, De

nton,

TX

1430

hrs

AIAA-2

015-2

493

Unde

rstan

ding A

ir Tra

nspo

rtatio

n Ma

rket

Dyna

mics

using

a Se

arch

Alg

orith

m for

Calib

ratin

g Tra

vel

Dema

nd an

d Pric

eV.

Kuma

r, B. H

orio,

A. De

Cicco,

S. Ha

san, V

. Sto

uffer,

LMI, M

cLean

, VA;

J. Sm

ith, N

ASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA; e

t al.

1500

hrs

AIAA-2

015-2

494

Deve

lopme

nt of

an AT

C Tow

er

Simula

tor t

o Sim

ulate

Grou

nd

Oper

ation

sZ.

Chua

, Univ

ersity

of To

ulous

e, To

ulous

e, Fra

nce;

F. An

dre, M

. Cou

sy, Fr

ench

Civil

Av

iation

Univ

ersity

, Tou

louse

, Fran

ce

1530

hrs

AIAA-2

015-2

495

Multi-

Agen

t Bas

ed A

ir Tra

ffic

Simula

tion

Syste

mZ.

Yue,

D. S

ui, Y.

Lin,

J. Zh

ang,

Nanji

ng

Unive

rsity

of Ae

ronau

tics a

nd As

trona

utics,

Na

njing

, Chin

a

1600

hrs

AIAA-2

015-2

496

Estim

ating

Ben

efits

of A

viatio

n Al

terna

tive F

uels

at th

e Sys

tem,

Rout

e, an

d Airp

ort L

evel

B. M

iller, C

. Murp

hy, M

etron

Aviat

ion, I

nc.,

Dulle

s, VA

; C. V

illa, A

. Filiz

ola, N

ation

al Civ

il Avia

tion A

genc

y (AN

AC),

Bras

ilia,

Braz

il

58

Mond

ay, 2

2 Ju

ne 2

015

66-M

ST-4

Guida

nce,

Cont

rol, a

nd D

ynam

ics I

Wyeth

Chair

ed by

: R. B

OTEZ

, Eco

le de

Tech

nolog

ie Su

perie

ure14

00 hr

sAIA

A-201

5-249

7A

New

Meth

od fo

r Tun

ing P

I Gain

s fo

r Pos

ition

Cont

rol o

f BLD

C Mot

or

Base

d Wing

Mor

phing

Actu

ator

sR.

Botez

, S. K

han,

Unive

rsity

of Qu

ébec

, Mo

ntréa

l, Can

ada

1430

hrs

AIAA-2

015-2

498

Long

itudin

al Sta

bility

Aug

ment

ation

of

Seap

lanes

in P

laning

K. Ito

, Ghe

nt Un

iversi

ty, G

hent,

Belg

ium; T

. Hir

ayam

a, Yo

koha

ma N

ation

al Un

iversi

ty,

Yoko

hama

, Jap

an; T

. Sak

urai, H

iyoh

Aircra

ft Ma

nufac

turing

and D

evelo

pmen

t Co

mpan

y, To

kyo,

Japa

n; T.

Dhae

ne, G

hent

Unive

rsity,

Ghe

nt, B

elgium

1500

hrs

AIAA-2

015-2

499

Cont

rol v

alida

tion

of a

morp

hing

wing

in an

open

loop

arch

itectu

reM.

Tcha

tchue

ng Ka

mmeg

ne, D

. Ngu

yen,

R. Bo

tez, U

nivers

ity of

Qué

bec,

Montr

éal,

Cana

da

1530

hrs

AIAA-2

015-2

500

A Co

mpar

ative

Stud

y of a

Pse

udo-

Five D

egre

e of F

reed

om an

d an

Adjoi

nt M

odel

Again

st a S

ix De

gree

of

Free

dom

Mode

l for

Fide

lity

Asse

ssmen

tE.

Seze

r, M. N

alci, R

OKET

SAN

Missi

le Ind

ustrie

s, Inc

., An

kara,

Turke

y; A.

Kutay

, Mi

ddle

East

Tech

nical

Unive

rsity,

Anka

ra,

Turke

y

Mond

ay, 2

2 Ju

ne 2

015

67-P

DL-3

Plasm

a Com

puta

tiona

l Meth

ods I

Mone

t Ball

room

Chair

ed by

: M. W

HITE

, Ohio

Aeros

pace

Insti

tute

1400

hrs

AIAA-2

015-2

501

A No

n-ite

rativ

e Hyp

erbo

lic, F

irst-

orde

r Con

serv

ation

Law

Appr

oach

to

Dive

rgen

ce-fr

ee So

lution

s to

Maxw

ell’s

Equa

tions

R. Th

omps

on, T

. Moe

ller, U

nivers

ity of

Te

nnes

see,

Tulla

homa

, Tull

ahom

a, TN

1430

hrs

AIAA-2

015-2

502

Equiv

alent

Elec

trica

l Circ

uit fo

r a 1

D Pla

sma E

ngine

N. Ra

mesh

, Sri J

agad

guru

Chan

drash

ekara

natha

Swa

miji I

nstitu

te of

Tech

nolog

y, Ch

ickba

llapu

r, Ind

ia; P.

Mos

es

John

Chris

ty Ap

polo,

T. S

hesh

adri,

Indian

Ins

titute

of Sc

ience

, Ben

galur

u, Ind

ia

1500

hrs

AIAA-2

015-2

503

Inve

stiga

tions

of Fl

ow ov

er a

Hemi

sphe

re u

sing N

umer

ical

Simula

tions

C. Ta

m, T.

Mad

den,

Air Fo

rce Re

searc

h La

borat

ory, K

irtlan

d AFB

, NM;

B. T

hurow

, Au

burn

Unive

rsity,

Aubu

rn, AL

1530

hrs

AIAA-2

015-2

504

CFD

Valid

ation

of P

IV-ba

sed

Estim

ation

of D

BD P

lasma

-Ac

tuat

ion Fo

rceQ.

Zhai,

Z. Zh

ang,

J. Ca

i, Nort

hwes

tern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

; F.

Liu, S

. Luo

, Univ

ersity

of Ca

liforni

a, Irv

ine,

Los A

ngele

s, CA

Mond

ay, 2

2 Ju

ne 2

015

68-TP

-3Ab

lation

IIRo

setta

Chair

ed by

: N. D

OUGH

ERTY

, ERC

Inco

rporat

ed an

d A. H

ASHE

MI, L

ockh

eed M

artin

Spac

e Sys

tems

1400

hrs

AIAA-2

015-2

505

Effe

cts of

Wat

er P

rese

nce o

n Lo

w Te

mper

atur

e Phe

nome

non

in Po

rous

TPS M

ater

ials

D. S

mith,

A. O

midy

, H. W

eng,

Unive

rsity

of Ke

ntuck

y, Le

xingto

n, Le

xingto

n, KY

; T.

Whit

e, ER

C, Inc

., Mo

ffett

Field,

CA; A

. Ma

rtin, U

nivers

ity of

Kentu

cky,

Lexin

gton,

Lexin

gton,

KY

1430

hrs

AIAA-2

015-2

506

A Mu

lti-Di

mens

ional

Finite

Elem

ent

Base

d Solv

er fo

r Dec

ompo

sing

and N

on-D

ecom

posin

g The

rmal

Prot

ectio

n Sy

stems

M. H

oward

, B. B

lackw

ell, S

andia

Nati

onal

Labo

ratori

es, A

lbuqu

erque

, NM

1500

hrs

AIAA-2

015-2

507

Ther

mal P

rotec

tion

Syste

m Ma

ss Es

timat

ing R

elatio

nship

s For

Blun

t-Bo

dy, E

arth

Entry

Spac

ecra

ftS.

Sep

ka, E

RC, I

nc.,

Moffe

tt Fie

ld, CA

; J.

Sama

reh, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1530

hrs

AIAA-2

015-2

508

Deve

lopme

nt an

d Qua

lifica

tion

of

Light

weigh

t Abla

tor A

eros

hell B

BM

for M

artia

n Mi

ssion

K. Fu

jita, T

. Suz

uki, T

. Aok

i, T. O

gasa

wara,

Y.

Ishida

, Jap

an Ae

rospa

ce Ex

plorat

ion

Agen

cy (J

AXA)

, Cho

fu, Ja

pan

59

Mond

ay, 2

2 Ju

ne 2

015

69-TP

-4Ae

roth

ermo

dyna

mics

ISte

uben

Chair

ed by

: C. J

OHNS

TON,

NAS

A-Lan

gley R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-2

509

Mode

ling F

idelity

for O

xyge

n No

nequ

ilibriu

m Th

ermo

chem

istry

in

Refle

cted S

hock

Tube

Flow

sK.

Neitz

el, D

. And

rienk

o, I.

Boyd

, Un

iversi

ty of

Mich

igan,

Ann A

rbor, A

nn

Arbor,

MI

1430

hrs

AIAA-2

015-2

510

State

Spec

ific M

odeli

ng of

the

Ener

gy Tr

ansfe

r in

Nitro

gen

Shoc

ks

using

High

Fide

lity M

odels

T. Zh

u, Z.

Li, N

. Pars

ons,

Penn

sylva

nia

State

Univ

ersity

, Stat

e Coll

ege,

PA; D

. Le

vin, M

. Pan

esi, U

nivers

ity of

Illino

is,

Urba

na-Ch

ampa

ign, U

rbana

, IL

1500

hrs

AIAA-2

015-2

511

DSMC

Mod

eling

of N

oneq

uilibr

ium

Electr

onic

Excit

ation

and E

missi

on

for H

yper

sonic

Sens

or A

pplic

ation

sJ.

Burt,

E. Jo

syula

, Air F

orce R

esea

rch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH

1530

hrs

AIAA-2

015-2

512

Meas

urem

ent o

f Ultr

aviol

et Ra

diativ

e Hea

ting A

ugme

ntat

ion in

HI

EST R

eflec

ted Sh

ock

Tunn

elB.

Crud

en, A

. Bran

dis, E

RC, I

nc.,

Moffe

tt Fie

ld, CA

; J. G

rinste

ad, J

. Olej

nicza

k, NA

SA

Ames

Rese

arch C

enter

, Moff

ett Fi

eld, C

A; L.

Kirk,

R. Lil

lard,

NASA

John

son S

pace

Ce

nter, H

ousto

n, TX

; et a

l.

1600

hrs

AIAA-2

015-2

513

Comp

ariso

n of

Two H

ybrid

RC

-Mod

els fo

r Pre

dictio

n of

No

nequ

ilibriu

m Ra

diatio

n fro

m Str

ong S

hock

Wav

esS.

Surz

hikov

, Rus

sian A

cade

my of

Sc

ience

s, Mo

scow,

Russi

a

1630

hrs

AIAA-2

015-2

514

Radia

tive H

eat F

lux fr

om M

etallic

Sp

ecies

in Fr

ee P

iston

Shoc

k Tu

nnel

HIES

TS.

Nom

ura, H

. Tak

ayan

agi, K

. Fuji

ta,

H. Ta

nno,

Japa

n Aero

spac

e Exp

lorati

on

Agen

cy (J

AXA)

, Cho

fu, Ja

pan

Mond

ay, 2

2 Ju

ne 2

015

70-N

W-2

1530

- 16

00 h

rsNe

twor

king C

offe

e Bre

akMe

eting

Roo

m Fo

yers

Mond

ay, 2

2 Ju

ne 2

015

71-A

IAA-

1 17

30 -

1900

hrs

Spee

d Gee

k Ne

twor

king E

vent

and R

ecep

tion

Chan

tilly B

allro

om Fo

yer

This

casu

al, hi

gh-en

ergy s

essio

n will

give y

ou th

e opp

ortun

ity to

enga

ge on

e-on-o

ne w

ith sp

eake

rs an

d get

a glim

pse o

f thin

gs to

come

in th

e wee

k ahe

ad at

AIAA

AVIAT

ION

2015

. Yo

u’ll tr

avel

from

spea

ker t

o spe

aker

in sm

all gr

oups

, liste

n to a

5-m

inute

overv

iew of

their

topic

, and

then

have

five m

inutes

to ha

ve yo

ur qu

estio

ns an

swere

d.Op

en to

all c

onfer

ence

atten

dees

, but

spac

e is l

imite

d to t

he fir

st 50

0 pa

rticipa

nts.

Spon

sored

by: L

ockh

eed M

artin

Mond

ay, 2

2 Ju

ne 2

015

72-C

ASE-3

17

30 -

1900

hrs

CASE

Netw

orkin

g Soc

ialMo

rocco

Spon

sored

by B

oeing

Comm

ercial

Airpl

anes

Mond

ay, 2

2 Ju

ne 2

015

73-LE

C-1

1730

- 18

30 h

rsFlu

id Dy

nami

cs Aw

ard L

ectu

reGr

and B

allro

om D

Searc

hing f

or Tru

thine

ss in

Comp

utatio

nal F

luid D

ynam

icsPh

ilip R

oePro

fesso

r, Dep

artme

nt of

Aeros

pace

Engin

eerin

gUn

iversi

ty of

Mich

igan

Mond

ay, 2

2 Ju

ne 2

015

74-R

LA-1

18

30 -

1930

hrs

Risin

g Lea

ders

in Ae

rosp

ace N

etwor

king R

ecep

tion

Emer

ald

The r

ecep

tion w

ill kic

k off

the Ri

sing L

eade

rs in

Aeros

pace

even

ts an

d is a

perfe

ct op

portu

nity f

or yo

ung l

eade

rs to

ming

le wi

th oth

ers w

ho w

ill be

partic

ipatin

g in A

IAA AV

IATIO

N 20

15 as

atten

dee,

prese

nter, o

r vete

ran pr

ofessi

onal

Come

mee

t othe

r part

icipan

ts in

a cas

ual e

nviro

nmen

t. Yo

u’re b

ound

to se

e the

m ag

ain.

60

Tues

day

Tues

day,

23 Ju

ne 2

015

75-S

B-2

0730

- 08

00 h

rsSp

eake

rs’ B

riefin

gSe

ssion

Roo

ms

Tues

day,

23 Ju

ne 2

015

76-P

LNRY

-2

0800

- 09

00 h

rsPle

nary

Pan

elCh

antill

y Ball

room

Wes

t

NextG

en: A

Mod

el of

Stake

holde

r Eng

agem

ent

Bill A

yer

Retire

d Cha

irman

and C

EOAla

ska A

ir Grou

p

Edwa

rd L.

Bolt

on Jr

.As

sistan

t Adm

inistr

ator f

or Ne

xtGen

Fede

ral Av

iation

Admi

nistra

tion

Tues

day,

23 Ju

ne 2

015

77-A

A-11

Fan

Noise

Fleur

-de-

lis A

Chair

ed by

: S. G

LEGG

, Flor

ida At

lantic

Univ

ersity

0900

hrs

AIAA-2

015-2

515

Extra

polat

ion of

RAN

S flow

data

fo

r imp

rove

d ana

lytica

l fan

tone

pr

edict

ionR.

Jaron

, A. M

oreau

, S. G

uerin

, Germ

an

Aeros

pace

Cente

r (DL

R), B

erlin,

Germ

any

0930

hrs

AIAA-2

015-2

516

Syste

m No

ise P

redic

tion

of th

e DG

EN 3

80 Tu

rbof

an En

gine

J. Be

rton,

NASA

Glen

n Res

earch

Cente

r, Cle

velan

d, OH

1000

hrs

AIAA-2

015-2

517

Fan n

oise s

calin

g of s

tatic d

ata

using

semi

-analy

tical

metho

ds an

d as

sessm

ent a

gains

t exp

erime

ntal d

ataV.

Bland

eau,

V. Pa

storel

li, Air

bus,

Toulo

use,

Franc

e; A.

Morea

u, S.

Gue

rin, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Berl

in, G

erman

y

1030

hrs

AIAA-2

015-2

518

Valid

ation

of a

Movin

g-Bo

dy H

igh-

Orde

r Imm

erse

d Bou

ndar

y Meth

od

for t

he M

ultipl

e Pur

e Ton

e Nois

e Ge

nera

ted by

Supe

rsonic

Rot

or

Casca

des

B. Pi

menta

, R. B

oben

rieth

Mise

rda,

Unive

rsity

of Br

asília

, Bras

ília, B

razil

1100

hrs

AIAA-2

015-2

519

Effe

ct of

Stat

or Va

ne Sw

eep o

n Hi

gh Fr

eque

ncy F

an N

oise a

nd

Comp

ariso

n wi

th Ex

perim

ent

A. Ko

zlov,

H. At

assi,

Univ

ersity

of N

otre

Dame

, Notr

e Dam

e, IN

Tues

day,

23 Ju

ne 2

015

78-A

A-12

Duct

Acou

stics

IIFle

ur-d

e-lis

BCh

aired

by: C

. YEN

, Jac

obs T

echn

ology

0900

hrs

AIAA-2

015-2

520

Aero

-Aco

ustic

Per

form

ance

of

Adap

tive N

acell

e Inle

tF.

Majić

, G. E

fraim

sson,

C. O’

Reilly

, Roy

al Ins

titute

of Te

chno

logy (

KTH)

, Stoc

kholm

, Sw

eden

0930

hrs

AIAA-2

015-2

521

Theo

retic

al Stu

dy of

Soun

d Pr

opag

ation

in Li

ned D

uct w

ith

Rigid

Splic

es U

sing W

iener

-Hop

f Me

thod

X. Li

u, H.

Jian

g, X.

Hua

ng, P

eking

Un

iversi

ty, B

eijing

, Chin

a

1000

hrs

AIAA-2

015-2

522

Soun

d Pro

paga

tion i

n Line

d Ann

ular

Ducts

with

Mea

n Swi

rling F

lowA.

Maldo

nado

, R. A

stley,

J. Co

uplan

d, G.

Gaba

rd, Un

iversit

y of S

outha

mpton

, So

utham

pton,

Unite

d King

dom;

D. Su

tliff,

NASA

Glen

n Rese

arch C

enter

, Clev

eland

, OH

1030

hrs

AIAA-2

015-2

523

Upstr

eam

Radia

tion

from

Supe

rsonic

Bur

ied-n

ozzle

Jets

via

Scat

tering

at th

e Shr

oud E

dge

A. Sa

manta

, Ind

ian In

stitut

e of S

cienc

e, Ba

ngalo

re, In

dia; J

. Freu

nd, U

nivers

ity of

Illi

nois,

Urba

na-Ch

ampa

ign, U

rbana

, IL

1100

hrs

AIAA-2

015-2

524

Nume

rical

Pred

iction

s of M

ode

Refle

ction

s in

an O

pen

Circu

lar

Duct:

Comp

ariso

n wi

th Th

eory

M. D

ahl, N

ASA G

lenn R

esea

rch Ce

nter,

Cleve

land,

OH; D

. Hixo

n, Un

iversi

ty of

Toled

o, To

ledo,

OH

Tues

day,

23 Ju

ne 2

015

79-A

A-13

Trailin

g Edg

e Nois

e II

Inve

rnes

sCh

aired

by: J

. GAL

LMAN

, Gulf

strea

m Ae

rospa

ce Co

rporat

ion09

00 hr

sAIA

A-201

5-252

5Pr

edict

ion of

Por

ous T

railin

g Edg

e No

ise R

educ

tion

via A

cous

tic

Pertu

rbat

ion Eq

uatio

ns an

d Volu

me

Aver

aging

B. Fa

ssman

n, C.

Rautm

ann,

R. Ew

ert, J

. De

lfs, G

erman

Aeros

pace

Cente

r (DL

R),

Brau

nsch

weig,

Germ

any

0930

hrs

AIAA-2

015-2

526

Pred

iction

of B

road

band

Trail

ing-

Edge

Nois

e Bas

ed on

Blak

e Mod

el an

d Ami

et Th

eory

O. S

talno

v, C.

Paruc

huri,

P. Jo

seph

, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom

1000

hrs

AIAA-2

015-2

527

Para

metri

c Inv

estig

ation

s of T

onal

Trailin

g-Ed

ge N

oise G

ener

ation

by

Low-

Reyn

olds N

umbe

r Airf

oils.

Part

I - Ex

perim

enta

l Stu

dies

G. Ya

khina

, M. R

oger,

École

Centr

ale de

Ly

on, L

yon,

Franc

e; L.

Nguy

en, V

. Golu

bev,

Embry

-Ridd

le Ae

ronau

tical

Unive

rsity,

Da

ytona

Bea

ch, F

L

1030

hrs

AIAA-2

015-2

528

Para

metri

c Inv

estiga

tions

of To

nal

Trailin

g-Edg

e Nois

e Gen

eratio

n by

Low-

Reyn

olds N

umbe

r Airf

oils.

Part

II - N

umeri

cal S

tudies

L. Ng

uyen

, W. H

iner, S

. Sale

hian,

V. Go

lubev,

R.

Mank

badi,

Embry

-Ridd

le Ae

ronau

tical

Unive

rsity,

Dayto

na Be

ach, F

L; G.

Yakh

ina,

École

Centr

ale de

Lyon

, Lyo

n, Fra

nce; e

t al.

1100

hrs

AIAA-2

015-2

529

A Mo

del f

or Je

t-Sur

face

Inter

actio

n No

ise U

sing P

hysic

ally R

ealiz

able

Upstr

eam

Turb

ulenc

e Con

dition

sM.

Afsa

r, Imp

erial

Colle

ge Lo

ndon

, Lon

don,

Unite

d King

dom;

S. L

eib, O

hio Ae

rospa

ce

Institu

te, Cl

evela

nd, O

H

1130

hrs

AIAA-2

015-2

530

On th

e Adjo

int-b

ased

Cont

rol o

f Tra

iling-

Edge

Turb

ulenc

e and

Nois

e Mi

nimiza

tion

via P

orou

s Mat

erial

B. Zh

ou, N

. Gau

ger, T

echn

ical U

nivers

ity of

Ka

isersl

auter

n, Ka

isersl

auter

n, Ge

rman

y; S.

Koh,

M. M

einke

, W. S

chroe

der, R

WTH

Aa

chen

Univ

ersity

, Aac

hen,

Germ

any

1200

hrs

AIAA-2

015-2

531

Expe

rimen

tal Va

lidati

on of

a Se

mi-

Analy

tical

Trailin

g-Edg

e Nois

e Mod

el Inc

luding

Broa

dban

d Sca

tterin

gK.

Kucuk

cosku

n, J.

Christ

ophe

, C. S

chram

, von

Ká

rmán

Instit

ute fo

r Fluid

Dyna

mics,

Rhod

e-Sa

int-Ge

nèse,

Belgiu

m; S.

More

au, U

nivers

ity

of Sh

erbroo

ke, S

herbr

ooke

, Can

ada

61

Tues

day,

23 Ju

ne 2

015

80-A

A-14

Jet N

oise P

redic

tion

IIILa

lique

Chair

ed by

: N. M

URRA

Y, Th

e Univ

ersity

of M

ississ

ippi

0900

hrs

AIAA-2

015-2

532

Analy

sis of

Inter

mitte

ncy o

f Su

perso

nic Je

t Nois

e with

Sy

nchr

onize

d LES

U. Sa

sidha

ran N

air, L

. Ago

stini, D

. Gait

onde

, Oh

io Sta

te Un

iversit

y, Co

lumbu

s, OH

0930

hrs

AIAA-2

015-2

533

Aero

acou

stic A

nalys

is of

a He

licop

ter En

gine J

et In

cludin

g a

Reali

stic N

ozzle

Geo

metry

M. Ce

tin, S

. Koh

, M. M

einke

, W.

Schro

eder,

RWTH

Aach

en U

nivers

ity,

Aach

en, G

erman

y

1000

hrs

AIAA-2

015-2

534

Larg

e-sca

le str

uctu

re ev

olutio

n an

d so

und g

ener

ation

in a

hotje

tF.

Feng

, Q. W

ang,

China

Acad

emy o

f Ae

rospa

ce Ae

rodyn

amics

, Beij

ing, C

hina

1030

hrs

AIAA-2

015-2

535

Larg

e edd

y sim

ulatio

n for

jet n

oise:

the im

porta

nce o

f gett

ing th

e bo

unda

ry la

yer r

ight

G. Brè

s, Ca

scade

Techn

ologie

s, Inc

., Palo

Alto,

CA

; V. J

aune

t, M. L

e Ralli

c, P. J

ordan

, Nati

onal

Cente

r for S

cienti

fic Re

search

(CNR

S), P

oitier

s, Fra

nce; T

. Colo

nius,

Califo

rnia I

nstitu

te of

Techn

ology,

Pasad

ena,

CA; S

. Lele

, Stan

ford

Unive

rsity,

Stanfo

rd, CA

1100

hrs

AIAA-2

015-2

536

Empir

icism

-free

nois

e calc

ulatio

n fro

m LE

S solu

tion

base

d on

Golds

tein

gene

raliz

ed ac

ousti

c an

alogy

: volu

me n

oise s

ource

s and

me

anflo

w ef

fects

V. Se

milet

ov, S

. Kara

baso

v, A.

Chint

agun

ta, A.

Mark

estei

jn, Q

ueen

Mary

Un

iversi

ty of

Lond

on, L

ondo

n, Un

ited

Kingd

om

1130

hrs

AIAA-2

015-2

537

Spat

ial st

abilit

y cha

racte

ristic

s of

non-

circu

lar je

tsF.

Lajús

, Fed

eral U

nivers

ity of

San

ta Ca

tarina

, Flor

ianóp

olis,

Braz

il; A.

Cava

lieri,

Tech

nolog

ical In

stitut

e of A

erona

utics

(ITA)

, São

José

dos C

ampo

s, Br

azil;

C. De

scham

ps, F

edera

l Univ

ersity

of S

anta

Catar

ina, F

lorian

ópoli

s, Br

azil

Tues

day,

23 Ju

ne 2

015

81-A

A-15

CAA

Nume

rical

Tech

nique

s II

Obeli

sk A

Chair

ed by

: X. L

I, Be

ihang

Univ

ersity

0900

hrs

AIAA-2

015-2

538

Coup

led O

verse

t Uns

tructu

red

Disco

ntinu

ous G

alerk

in Me

thod

fo

r Lau

nch

Envir

onme

nt A

cous

tics

Pred

iction

(Inv

ited)

R. Ha

rris, C

FD Re

searc

h Corp

oratio

n, Hu

ntsvil

le, AL

; E. C

ollins

, A. S

escu

, E.

Luke

, Miss

issipp

i Stat

e Univ

ersity

, Mi

ssissi

ppi S

tate,

MS

0930

hrs

AIAA-2

015-2

539

Optim

ized E

xplic

it Di

ssipa

tion

Oper

ator

s for

Comp

utat

ional

Aero

acou

stics

N. M

anso

uri, D

. Hixo

n, Un

iversi

ty of

Toled

o, To

ledo,

OH

1000

hrs

AIAA-2

015-2

540

DRP

schem

es pe

rform

poor

ly fo

r de

cayin

g or g

rowi

ng os

cillat

ions

E. Br

amble

y, Un

iversi

ty of

Camb

ridge

, Ca

mbrid

ge, U

nited

King

dom

1030

hrs

AIAA-2

015-2

541

Towa

rds C

asca

de Tr

ailing

-Edge

No

ise M

odeli

ng U

sing a

Mod

e-Ma

tching

Tech

nique

M. Ro

ger, É

cole

Centr

ale de

Lyon

, Ecu

lly,

Franc

e; S.

More

au, G

AUS,

She

rbroo

ke,

Cana

da

1100

hrs

AIAA-2

015-2

542

Zero

-Ave

rage

Sour

ce Te

rms f

or

Multid

imen

siona

l Non

linea

r Di

sturb

ance

Equa

tions

D. H

ixon,

Unive

rsity

of To

ledo,

Toled

o, OH

Tues

day,

23 Ju

ne 2

015

82-A

CD-2

Aircr

aft D

esign

Meth

ods a

nd To

olsWy

ethCh

aired

by: A

. CHA

PUT,

Unive

rsity

of Te

xas a

t Aus

tin09

00 hr

sAIA

A-201

5-254

3Stu

dent

Air

Vehic

le De

sign

and

Analy

sis -

A Sy

stems

Engin

eerin

g Mo

del B

ased

App

roac

hA.

Chap

ut, U

nivers

ity of

Texa

s, Au

stin,

Austi

n, TX

0930

hrs

AIAA-2

015-2

544

Upda

te on

HCD

struc

t - A

Tool

for

Hybr

id Wi

ng B

ody C

once

ptua

l De

sign

and S

tructu

ral O

ptim

izatio

nF.

Gern,

NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

1000

hrs

AIAA-2

015-2

545

Simult

aneo

us A

ircra

ft De

sign

and T

rip A

ssign

ment

und

er

Desig

n Pa

rame

ter an

d Dem

and

Unce

rtaint

yP.

Govin

daraj

u, W.

Cros

sley,

Purdu

e Un

iversi

ty, W

est L

afaye

tte, I

N

1030

hrs

AIAA-2

015-2

546

Virtu

al fli

ght t

estin

g in

an ai

rcraf

t siz

ing an

d opt

imiza

tion

proc

ess

P. Sc

hmoll

grube

r, N. B

artoli

, ONE

RA,

Toulo

use,

Franc

e; Y.

Gouri

nat,

Unive

rsity

of To

ulous

e, To

ulous

e, Fra

nce

1100

hrs

AIAA-2

015-2

547

User

Defi

ned C

ompo

nent

s in

the

Open

VSP

Para

metri

c Geo

metry

Tool

R. Mc

Dona

ld, Ca

liforni

a Poly

techn

ic St

ate U

nivers

ity, S

an Lu

is Ob

ispo,

CA; J

. Glo

udem

ans,

Self,

San M

ateo,

CA

1130

hrs

AIAA-2

015-2

548

Deve

lopme

nt of

an In

terac

tive

Wave

Dra

g Cap

abilit

y for

the

Open

VSP

Para

metri

c Geo

metry

Tool

M. W

addin

gton,

R. Mc

Dona

ld, Ca

liforni

a Po

lytec

hnic

State

Univ

ersity

, San

Luis

Obisp

o, CA

Tues

day,

23 Ju

ne 2

015

83-A

FM-5

Aircr

aft F

light

Dyn

amics

, Con

trol, H

andli

ng Q

ualiti

es an

d Per

form

ance

IIPlu

m Bl

osso

m A

Chair

ed by

: M. G

RANT

, Purd

ue U

nivers

ity09

00 hr

sAIA

A-201

5-254

9Da

mage

Mitig

ating

on a

Larg

e Ro

torcr

aft u

sing L

oad A

llevia

ting

Fligh

t Con

trol L

aws

D. Ca

udle,

J. H

orn, E

. Kell

er, Pe

nnsy

lvania

St

ate U

nivers

ity, S

tate C

olleg

e, PA

; C.

Thais

s, C.

McCo

ll, Te

chnic

al Da

ta An

alysis

, Inc

., Ma

rietta

, GA

0930

hrs

AIAA-2

015-2

550

Aero

batic

Man

euve

rs of

a Co

nven

tiona

l and

Comp

ound

Ro

torcr

aft -

Fligh

t Pat

h Ge

nera

tion

and D

ynam

ic Sim

ulatio

nA.

Thors

en, J

. Horn

, Pen

nsylv

ania

State

Un

iversi

ty, S

tate C

olleg

e, PA

1000

hrs

AIAA-2

015-2

551

Prop

eller

Torq

ue Ef

fect

on Cr

uise

Trim

of St

anda

rd an

d Mas

s-Ac

tuat

ed A

irplan

eS.

Ertur

k, A.

Doga

n, Un

iversi

ty of

Texa

s, Arl

ington

, Arlin

gton,

TX

1030

hrs

AIAA-2

015-2

552

Ener

gy G

ain Fr

om an

Atm

osph

ere

in Mo

tion

- Dyn

amic

Soar

ing an

d Re

gen-

electr

ic Fli

ght C

ompa

red

J. Ba

rnes,

Pelica

n Aero

Grou

p, Sa

n Pe

dro, C

A

1100

hrs

AIAA-2

015-2

553

Inter

actio

ns of

Airc

raft

Desig

n an

d Con

trol: A

ctuat

ors S

izing

and

Optim

izatio

n fo

r an

Unsta

ble

Blen

ded W

ing-B

ody

Y. De

nieul,

D. A

lazard

, J. B

orden

euve

, Un

iversi

ty of

Toulo

use,

Toulo

use,

Franc

e; C.

Tous

saint

, ONE

RA, T

oulou

se, F

rance

; G.

Taqu

in, Ai

rbus,

Toulo

use,

Franc

e

1130

hrs

AIAA-2

015-2

554

Finite

Serie

s Bas

ed M

odel

Refe

renc

e Ada

ptive

Cont

rol

R. Ge

zer, R

OKET

SAN

Missi

le Ind

ustrie

s, Inc

., An

kara,

Turke

y; A.

Kutay

, Midd

le Ea

st Te

chnic

al Un

iversi

ty, An

kara,

Turke

y

62

Tues

day,

23 Ju

ne 2

015

84-A

FM-6

Aero

serv

oelas

tic (A

SE) a

nd A

erod

ynam

ic Pr

edict

ion M

ethod

sPlu

m Bl

osso

m B

Chair

ed by

: A. D

A RON

CH, U

nivers

ity of

Sou

thamp

ton an

d T. R

ICHAR

DSON

, Univ

ersity

of B

ristol

0900

hrs

AIAA-2

015-2

555

Adap

tive C

heby

shev

Neu

ral C

ontro

l of

a Mu

lti-In

put A

eroe

lastic

Syste

m De

spite

Gus

t Loa

dP.

Ghora

wat,

Unive

rsity

of Ne

vada

, Las

Ve

gas,

Las V

egas

, NV;

K. Le

e, Ca

tholic

Kwan

dong

Univ

ersity

, Gan

gnun

g, So

uth

Korea

; S. S

ingh,

Unive

rsity

of Ne

vada

, Las

Ve

gas,

Las V

egas

, NV

0930

hrs

AIAA-2

015-2

556

Mode

ling a

nd Si

mulat

ion fo

r Au

tono

mous

Aer

ial R

efue

ling U

sing

a Pro

be-D

rogu

e Sys

temH.

Wan

g, X.

Don

g, J.

Liu, J

. Wan

g, Air

Fo

rce En

ginee

ring U

nivers

ity, X

i’an,

China

1000

hrs

AIAA-2

015-2

557

Pilot

In Th

e Loo

p Aer

oser

voela

stic

Simula

tion

In Su

ppor

t To T

he

Conc

eptu

al De

sign

Of A

Fly B

y Wire

Ai

rplan

eF.

Boco

la, V.

Mus

carel

lo, G

. Qua

ranta,

P.

Masa

rati, T

echn

ical U

nivers

ity of

Mila

n, Mi

lano,

Italy

1030

hrs

AIAA-2

015-2

558

Aero

stru

ctura

l mod

eling

of a

wing

us

ing CA

TIA V5

and X

FLR5

softw

are

and e

xper

imen

tal v

alida

tion

using

th

e Pric

e- P

aïdou

ssis w

ing tu

nnel

D. Co

mmun

ier, M

. Sali

nas,

O. Ca

rranz

a Mo

yao,

R. Bo

tez, U

nivers

ity of

Qué

bec,

Montr

éal, C

anad

a

1100

hrs

AIAA-2

015-2

559

On th

e Calc

ulatio

n of

Pitc

h Da

mping

Stab

ility D

eriva

tives

of

Aircr

afts

Using

Uns

teady

Sens

itivity

Eq

uatio

nsC.

Guo,

Y. Re

n, Tsi

nghu

a Univ

ersity

, Be

ijing,

China

Tues

day,

23 Ju

ne 2

015

85-A

MT-5

/GT-5

Mode

l Atti

tude

, Def

orma

tion,

and D

ata A

cquis

ition

Tech

nique

sOb

elisk

BCh

aired

by: R

. GUY

TON,

USA

F Wrig

ht La

b09

00 hr

sAIA

A-201

5-256

0Te

mper

atur

e Mea

sure

ment

at th

e Ex

it of

Ann

ular C

ombu

stor w

ith

Sling

er in

Turb

ojet E

ngine

D. Li

u, J.

Jin, F

. Wan

g, W.

Jin,

Beiha

ng

Unive

rsity,

Beij

ing, C

hina

0930

hrs

AIAA-2

015-2

561

NASA

Data

Acqu

isition

Syste

m So

ftwar

e Dev

elopm

ent f

or Ro

cket

Prop

ulsion

Test

Facili

ties

P. Heb

ert, D

. Dav

is, M.

Turow

ski, W

. Holla

day,

NASA

Sten

nis Sp

ace Ce

nter, S

tennis

, MS;

P. Ma

rshall,

M. D

uncan

, Arct

ic Slop

e Reg

ional

Corpo

ration

(ASR

C), S

tennis

, MS;

et al.

1000

hrs

Oral

Prese

ntatio

nNe

w Wi

ngs l

evel

Yaw

Capa

bility

in

the A

EDC P

WT 1

6T Tu

nnel

B. M

ills, A

rnold

Engin

eerin

g Dev

elopm

ent

Comp

lex, T

ullah

oma,

TN

1030

hrs

Oral

Prese

ntatio

nMo

del D

efor

matio

n Me

asur

emen

ts on

a Fle

xible

Wing

R. Gu

yton,

Air Fo

rce Re

searc

h Lab

orator

y, W

right-

Patte

rson A

FB, O

H

1100

hrs

AIAA-2

015-2

562

Mode

l Def

orma

tion

Meas

urem

ent

Capa

bilitie

s at E

TWH.

Quix

, J. S

emme

lman

n, M.

Wrig

ht,

Europ

ean T

ranso

nic W

indtun

nel, C

ologn

e, Ge

rman

y

Tues

day,

23 Ju

ne 2

015

86-A

MT-6

/GT-6

Spat

ially-

Reso

lved S

pectr

osco

pic Te

chniq

ues

Edelw

eiss

Chair

ed by

: R. B

URNS

and A

. CUT

LER,

The G

eorge

Was

hingto

n Univ

ersity

0900

hrs

AIAA-2

015-2

563

WIDE

CARS

Spec

tra Fi

tting

in a

Prem

ixed E

thyle

ne-A

ir Fla

meA.

Cutle

r, E. G

allo,

L. Ca

ntu, G

eorge

Wa

shing

ton U

nivers

ity, W

ashin

gton,

DC

0930

hrs

AIAA-2

015-2

564

Dens

ity Sc

aling

and C

alibr

ation

of

FLEE

T Tem

pera

ture

Mea

sure

ment

sN.

Calve

rt, A.

Dog

ariu,

M. Ed

wards

, R.

Miles

, Prin

ceton

Univ

ersity

, Prin

ceton

, NJ

1000

hrs

AIAA-2

015-2

565

Preci

sion o

f FLE

ET Ve

locim

etry u

sing

High

-Spee

d CMO

S Cam

era Sy

stems

C. Pe

ters,

Prince

ton Un

iversit

y, Pri

nceton

, NJ;

P. Dan

ehy,

B. Ba

thel, N

ASA L

angle

y Rese

arch

Cente

r, Ham

pton,

VA; N

. Jian

g, Sp

ectral

En

ergies

, LLC

, Day

ton, O

H; N.

Calve

rt, R.

Miles

, Prin

ceton

Unive

rsity,

Prince

ton, N

J

1030

hrs

AIAA-2

015-2

566

Appli

catio

n of

FLEE

T Velo

cimetr

y in

the N

ASA

Lang

ley 0

.3-M

eter

Trans

onic

Cryo

genic

Tunn

elR.

Burns

, Nati

onal

Institu

te of

Aeros

pace

, Ha

mpton

, VA;

P. Da

nehy

, S. J

ones

, NAS

A La

ngley

Rese

arch C

enter

, Ham

pton,

VA;

B. H

alls,

N. Ji

ang,

Spec

tral E

nergi

es, L

LC,

Dayto

n, OH

1100

hrs

AIAA-2

015-2

567

Desig

n an

d App

licat

ion of

Filte

red

Rayle

igh Sc

atter

ing Ex

perim

ents

for M

ixing

Stud

ies of

New

Stru

t In

jecto

rs fo

r Scra

mjets

C. Gr

ound

, D. T

humi

ah, L

. Mad

dalen

a, Un

iversi

ty of

Texa

s, Arl

ington

, Arlin

gton,

TX

Tues

day,

23 Ju

ne 2

015

87-A

PA-9

High

Ang

le of

Atta

ck an

d High

Lift

Aero

dyna

mics

Stemm

ons C

Chair

ed by

: D. L

ACY,

Boein

g Com

merci

al Air

plane

s and

P. H

ARTW

ICH, B

oeing

Rese

arch &

Tech

nolog

y09

00 hr

sAIA

A-201

5-256

8Hi

gh A

ngle

of A

ttack

Fligh

t of a

Su

bsca

le Ae

roba

tic A

ircra

ftO.

Dan

tsker,

M. S

elig,

Unive

rsity

of Illi

nois,

Ur

bana

-Cham

paign

, Urba

na, I

L

0930

hrs

AIAA-2

015-2

569

Pres

sure

Mea

sure

ment

s of B

urst

Wake

s Ove

r a Th

ree-

Eleme

nt A

irfoil

B. Po

meroy

, M. S

elig,

Unive

rsity

of Illi

nois,

Ur

bana

-Cham

paign

, Urba

na, I

L

1000

hrs

Oral

Prese

ntatio

nDe

velop

ment

Status

of th

e High

Lift

Comm

on Re

search

Mod

el (H

L-CRM

): A

Repr

esenta

tive H

igh Li

ft Co

nfigu

ratio

n for

Tran

sonic

Tran

spor

tsD.

Lacy,

The B

oeing

Comp

any,

Evere

tt, WA

; E.

Dicke

y, A.

Sclaf

ani, T

he Bo

eing C

ompa

ny,

Hunti

ngton

Beach

, CA

1030

hrs

AIAA-2

015-2

570

Stall M

aneu

ver S

imula

tion

of an

ela

stic T

rans

port

Aircr

aft b

ased

on

Fligh

t Tes

t Dat

aD.

Rohlm

ann,

S. Ke

ye, G

erman

Aeros

pace

Ce

nter (

DLR)

, Brau

nsch

weig,

Germ

any

1100

hrs

AIAA-2

015-2

571

Nume

rical

Inve

stiga

tion

of th

e Dy

nami

c Beh

avior

of a

High

-Lift

Confi

gura

tion

with

Circu

lation

Co

ntro

lD.

Kelle

r, R. R

udnik

, Germ

an Ae

rospa

ce

Cente

r (DL

R), B

rauns

chwe

ig, G

erman

y

1130

hrs

AIAA-2

015-2

572

Wall m

odele

d lar

ge ed

dy

simula

tion

of th

e VFE

-2 de

lta w

ingC.

Zwerg

er, S

. Hick

el, C.

Brei

tsamt

er, N

. Ad

ams,

Tech

nical

Unive

rsity

of Mu

nich,

Munic

h, Ge

rman

y

63

Tues

day,

23 Ju

ne 2

015

88-A

PA-1

0Wi

nd Tu

nnel

and F

light

Testi

ngCa

rpen

ter B

allro

omCh

aired

by: J

. PIN

IER, N

ASA L

angle

y Res

earch

Cente

r and

G. G

ATLIN

, NAS

A Lan

gley R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-2

573

Analy

sis of

Sing

le Ho

le Sim

ulated

Ba

ttle D

amag

e on

a Wing

Usin

g Pa

rticle

Imag

e Velo

cimetr

yM.

Almo

nd, P

. Ren

der, A

. Walk

er,

Loug

hboro

ugh U

nivers

ity, L

ough

borou

gh,

Unite

d King

dom

0930

hrs

AIAA-2

015-2

574

Wind

spee

d and

Flow

Ang

le Me

asur

emen

t by T

rack

ing of

a La

ser-I

nduc

ed B

reak

down

Spar

kM.

Renn

ie, M

. Ngu

yen,

S. G

ordey

ev, E

. Ju

mper,

Univ

ersity

of N

otre D

ame,

Notre

Da

me, I

N; A.

Cain,

Inno

vativ

e Tec

hnolo

gy

Appli

catio

ns Co

mpan

y, LLC

, Che

sterfie

ld,

MO; T

. Hay

den,

U.S.

Air F

orce A

cade

my,

Color

ado S

pring

s, CO

1000

hrs

AIAA-2

015-2

575

Low

Spee

d Wind

Tunn

el In

vesti

gatio

n of

a Cir

culat

ion

Cont

rol W

ing fo

r Enh

ance

d Lift

K. Ka

nistra

s, P.

Saka

, K. V

alava

nis, N

. Vit

zilaio

s, M.

Ruthe

rford,

Univ

ersity

of

Denv

er, D

enve

r, CO

1030

hrs

AIAA-2

015-2

576

Desig

n of

a sw

ept w

ing w

ind tu

nnel

mode

l for

stud

y of c

ross-

flow

insta

bility

J. Se

rpieri

, M. K

otson

is, D

elft U

nivers

ity of

Te

chno

logy,

Delft,

The N

etherl

ands

1100

hrs

AIAA-2

015-2

577

Nume

rical

Repli

catio

n and

Im

prov

emen

t of W

ind Tu

nnel

Tests

for D

esign

and O

ff-De

sign O

pera

ting

Point

s of W

ind Tu

rbine

Airfo

ilsT.

Kuhn

, ENE

RCON

GmbH

, Brem

en, G

erman

y; A.

Altmi

kus,

ENER

CON

GmbH

, Auri

ch,

Germ

any;

N. Ba

laresq

ue, D

eutsc

he W

indGu

ard

GmbH

, Vare

l, Germ

any;

M. Lip

pert,

Unive

rsity

of Ap

plied S

cience

s, Kie

l, Germ

any

1130

hrs

AIAA-2

015-2

578

Deve

lopme

nt, S

tartu

p Ope

ratio

ns

and T

ests

of a

Prop

eller

Wind

Tu

nnel

Test

Rig

S. S

peck

, S. H

erbst,

H. K

im, F

. Stei

n, M.

Ho

rnung

, Tec

hnica

l Univ

ersity

of M

unich

, Ga

rching

, Germ

any

1200

hrs

AIAA-2

015-2

579

Study

of th

e flow

field

nea

r the

AO

A se

nsor

of an

A32

0 air

craft

J. Ka

tz, S

an D

iego S

tate U

nivers

ity, S

an

Diego

, CA

Tues

day,

23 Ju

ne 2

015

89-A

PA-1

1Sp

ecial

Sessi

on: L

ow B

oom

Activ

ities I

ISte

mmon

s ACh

aired

by: S

. CLIF

F, NA

SA-Am

es an

d K. W

AITHE

, Gulf

strea

m Ae

rospa

ce Co

rporat

ion09

00 hr

sAIA

A-201

5-258

0De

sign

of O

ptim

um Eq

uivale

nt-

Area

Targ

et fo

r High

-Fide

lity Lo

w-Bo

om A

ircra

ft De

sign

C. Oc

heltre

e, S.

Choi,

Virgi

nia Po

lytec

hnic

Institu

te an

d Stat

e Univ

ersity

, Blac

ksbu

rg,

VA

0930

hrs

AIAA-2

015-2

581

Feas

ibility

of Su

perso

nic A

ircra

ft Co

ncep

ts fo

r Low

-Boo

m an

d Flig

ht

Trim

Cons

traint

sW.

Li, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1000

hrs

AIAA-2

015-2

582

Unce

rtaint

y Ana

lysis

and R

obus

t De

sign

of Lo

w-Bo

om Co

ncep

ts us

ing A

tmos

pher

ic Ad

joint

sS.

Ralla

bhan

di, N

ation

al Ins

titute

of Ae

rospa

ce, H

ampto

n, VA

1030

hrs

AIAA-2

015-2

583

Rise

Time

Pre

dictio

n of

Sonic

Bo

om by

Full-

Field

Simula

tion

with

Th

erma

l Non

equil

ibrium

R. Ya

mash

ita, K

. Suz

uki, U

nivers

ity of

To

kyo,

Kash

iwa,

Japa

n

1100

hrs

AIAA-2

015-2

584

Free

Fligh

t Mea

sure

ment

of A

ircra

ft Mo

del u

sing A

ero B

allist

ic Ra

nge

A. Iw

akaw

a, D.

Furuk

awa,

Y. Ao

ki, A.

Sa

soh,

Nago

ya U

nivers

ity, N

agoy

a, Ja

pan

Tues

day,

23 Ju

ne 2

015

90-A

PA-1

2We

apon

s Aer

odyn

amics

: Miss

ile/P

rojec

tile/G

uided

-Mun

itions

, Car

riage

and S

tore

Sepa

ratio

n I

Stemm

ons B

Chair

ed by

: C. P

ASILI

AO, A

FRL/

RWW

V an

d C. R

OSEM

A, US

Army

AMRD

EC09

00 hr

sAIA

A-201

5-258

5Fli

ght B

ehav

iors o

f a Co

mplex

Pr

ojecti

le us

ing a

Coup

led CF

D-ba

sed S

imula

tion

Tech

nique

: Fre

e Mo

tion

J. Sa

hu, F

. Fres

coni,

Army

Rese

arch

Labo

ratory

, Abe

rdeen

Prov

ing G

round

, MD

0930

hrs

AIAA-2

015-2

586

Effe

ct of

Cana

rd D

eflec

tion

on Fi

n Pe

rform

ance

of a

Fin-S

tabil

ized

Proje

ctile

S. S

ilton,

Army R

esea

rch La

borat

ory,

Aberd

een P

roving

Grou

nd, M

D; C.

Coyle

, U.

S. M

ilitary

Acad

emy,

West

Point

, NY

1000

hrs

AIAA-2

015-2

587

Enha

nced

Bod

y Vor

tex M

odeli

ng

With

in Mi

ssile

Datco

mJ.

Doyle

, C. R

osem

a, Arm

y Avia

tion

and M

issile

Rese

arch D

evelo

pmen

t and

En

ginee

ring C

enter

, Red

stone

Arse

nal, A

L

1030

hrs

AIAA-2

015-2

588

A Co

mpar

ison

of P

redic

tive

Meth

odolo

gies f

or M

issile

Co

nfigu

ratio

ns w

ith St

rake

sC.

Rose

ma, A

rmy A

viatio

n and

Miss

ile

Rese

arch D

evelo

pmen

t and

Engin

eerin

g Ce

nter, R

edsto

ne Ar

sena

l, AL

1100

hrs

AIAA-2

015-2

589

Delay

ed D

etach

ed Ed

dy Si

mulat

ion

of P

rojec

tile Fl

ows

J. Ga

n, G.

Zha,

Unive

rsity

of Mi

ami, C

oral

Gable

s, FL

Tues

day,

23 Ju

ne 2

015

91-A

TIO-9

Term

inal &

Surfa

ce O

pera

tions

III

Manc

heste

rCh

aired

by: A

. SAR

AF, S

aab S

ensis

Corpo

ration

0900

hrs

AIAA-2

015-2

590

Identi

fying

Key I

ssues

and P

otenti

al So

lution

s for

Integ

rated

Arriv

al,

Depa

rture,

Surfa

ce Op

eratio

ns by

Su

rvey

ing St

akeh

older

Prefe

rences

B. Ap

onso,

R. Co

ppen

barge

r, Y. J

ung,

NASA

Am

es Re

search

Cente

r, Moff

ett Fi

eld, C

A; C.

O’Co

nnor,

G. Lo

hr, N

ASA L

angle

y Rese

arch

Cente

r, Ham

pton,

VA; L

. Quo

n, NA

SA Am

es

Resea

rch Ce

nter, M

offett

Field

, CA;

et al.

0930

hrs

AIAA-2

015-2

591

Integ

ratio

n of U

ncert

ain Ra

mp Ar

ea

Aircra

ft Tra

jector

ies an

d Gen

eratio

n of

Optim

al Ta

xiway

Sche

dules

at

Char

lotte

Doug

las (C

LT) Ai

rpor

tJ.

Coup

e, D.

Milut

inovic

, Univ

ersity

of

Califo

rnia,

Santa

Cruz

, San

ta Cru

z, CA

; W.

Malik,

UARC

at N

ASA A

mes R

esearc

h Cen

ter,

Moffe

tt Field

, CA;

Y. Jun

g, NA

SA Am

es

Resea

rch Ce

nter, M

offet

Field,

CA

1000

hrs

AIAA-2

015-2

592

The e

ffects

of El

ectri

c Tax

i Sys

tems

on ai

rpor

t sur

face

cong

estio

nP.

Rolin

g, P.

Sillek

ens,

R. Cu

rran,

Delft

Unive

rsity

of Te

chno

logy,

Delft,

The

Nethe

rland

s; W.

Wild

er, KL

M Ro

yal D

utch

Airlin

es, S

chiph

ol, Th

e Neth

erlan

ds

1030

hrs

AIAA-2

015-2

593

Punc

tuali

ty as

KPI

for P

erfo

rman

ce

Base

d Airp

ort M

anag

emen

tS.

Loth,

S. H

elm, G

erman

Aeros

pace

Ce

nter (

DLR)

, Brau

nsch

weig,

Germ

any

1100

hrs

AIAA-2

015-2

594

Deter

minin

g Airp

ort A

irside

Ca

pacit

y Utili

zatio

n: A

Dem

and-

Drive

n Ap

proa

chC.

Schin

wald,

M. H

ornun

g, Te

chnic

al Un

iversi

ty of

Munic

h, Mu

nich,

Germ

any

1130

hrs

AIAA-2

015-2

595

Integ

ratio

n of

a Ro

uting

Tool

in an

Adv

ance

d Airp

ort C

ontro

ller

Work

ing P

ositio

nM.

Ellej

mi, E

UROC

ONTR

OL, B

russe

ls,

Belgi

um; B

. Weis

s, F.

Schm

itt, S

. Stra

ub,

Deuts

che F

lugsic

herun

g Gmb

H (D

FS),

Frank

furt,

Germ

any

64

Tues

day,

23 Ju

ne 2

015

92-A

TIO-1

0AT

M I -

Traje

ctory

Enha

ncem

ents

Milan

Chair

ed by

: S. R

OY, W

ashin

gton S

tate U

niv09

00 hr

sAIA

A-201

5-259

6Im

pact

of A

irspa

ce Ch

arge

s on

Trans

atlan

tic A

ircra

ft Tra

jecto

ries

B. S

ridha

r, NAS

A Ame

s Res

earch

Cente

r, Mo

ffett

Field,

CA; H

. Ng,

Unive

rsity

of Ca

liforni

a, Sa

nta Cr

uz, M

offett

Field

, CA;

F. Lin

ke, G

erman

Aeros

pace

Cente

r (DL

R),

Hamb

urg, G

erman

y; N.

Chen

, NAS

A Ame

s Re

searc

h Cen

ter, M

offett

Field

, CA

0930

hrs

AIAA-2

015-2

597

Pres

enta

tion

of th

ree m

ethod

s re

sults

comp

ariso

n fo

r Ver

tical

Navig

ation

VNAV

traje

ctory

op

timiza

tion

for t

he Fl

ight

Mana

geme

nt Sy

stem

FMS

B. B

eulze

, B. D

ancila

, R. B

otez,

Unive

rsity

of Qu

ébec

, Mon

tréal,

Cana

da

1000

hrs

AIAA-2

015-2

598

Simple

Tool

for A

ircra

ft No

ise-

Redu

ction

Rou

te De

sign

J. Li,

N. C

hen,

B. S

ridha

r, H. N

g, NA

SA

Ames

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1030

hrs

AIAA-2

015-2

599

Trajec

tory

Accu

racy

Sens

itivity

to

Mode

ling F

acto

rsS.

Torre

s, Lo

ckhe

ed M

artin

Corpo

ration

, Ro

ckvil

le, M

D

1100

hrs

AIAA-2

015-2

600

Trajec

tory

Inef

ficien

cy M

etric

for M

easu

ring O

pera

tiona

l Pe

rform

ance

of Fl

ights

in th

e Na

tiona

l Airs

pace

Syste

mS.

Tsao

, R. M

ayer,

A. M

ahas

habd

e, MI

TRE

Corpo

ration

, McLe

an, V

A

Tues

day,

23 Ju

ne 2

015

93-A

TIO-1

1Tra

nsfo

rmat

ional

Fligh

t - O

n-De

mand

Mob

ility

Metro

polita

n Ba

llroo

mCh

aired

by: B

. GER

MAN,

Geo

rgia I

nstitu

te of

Tech

nolog

y09

00 hr

sOr

al Pre

senta

tion

On-D

eman

d Mob

ility:

Aviat

ion’s

Futu

re P

ath

to H

igh Sp

eed R

egion

al Mo

bility

M. M

oore,

NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

0930

hrs

Oral

Prese

ntatio

nOn

-Dem

and M

obilit

y Tec

hnica

l Pa

thwa

y: En

ablin

g Eas

e of U

se

and S

afety

K. Go

odric

h, M.

Moo

re, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

1000

hrs

Oral

Prese

ntatio

nOn

-Dem

and M

obilit

y Tec

hnica

l Pa

thwa

y: En

ablin

g Low

Comm

unity

No

ise, L

ow O

pera

ting C

osts,

Rob

ust

Cont

rol, a

nd R

ide Q

uality

M. M

oore,

NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

Tues

day,

23 Ju

ne 2

015

94-C

ASE-4

09

00 -

1200

hrs

Appli

ed Co

mplex

ity W

orks

hop

Gran

d Ball

room

D

Partic

ipants

can l

earn

how

to em

brace

and t

hrive

with

in tec

hnica

lly, so

cially,

and o

rganiz

ation

ally c

omple

x env

ironm

ents.

Partic

ipants

will

be im

merse

d in a

three

-pron

ged a

pproa

ch to

learn

ing, w

ith in

dustr

y exa

mples

, app

lied t

heory

, and

inter

activ

e prac

tice.

Pleas

e join

us fo

r this

en

gage

ment,

and b

ring y

our o

wn ex

perie

nces

to sh

are an

d a de

sire t

o stre

ngthe

n you

r com

plex s

ystem

s eng

ineeri

ng th

inking

.

Pan

elists

:Pa

ul C.

Lamb

ertso

nSy

stems

Engin

eerin

g & In

tegrat

ion Te

am 7

77X

Boein

g Com

merci

al Air

plane

s

Steve

Holt

E ngin

eerin

g Inte

grated

Strat

egy,

Airpla

ne Le

vel E

ngine

ering

Integ

ration

The B

oeing

Comp

any

Jim B

lohow

iak77

7X Ai

rplan

e Lev

el Int

egrat

ion Te

amTh

e Boe

ing Co

mpan

y

Aliso

n La

uder

bach

777X

Airpl

ane L

evel

Integ

ration

Team

The B

oeing

Comp

any

Tues

day,

23 Ju

ne 2

015

95-C

FD-9

Adap

tive H

igh-O

rder

Meth

ods

Gran

d Ball

room

ACh

aired

by: G

. MAY

, RW

TH Aa

chen

and S

. ALLM

ARAS

, MIT

0900

hrs

AIAA-2

015-2

601

A Un

ifying

Comp

utat

ional

Fram

ewor

k fo

r Ada

ptive

High

-Or

der F

inite

Eleme

nt M

ethod

sM.

Woo

pen,

A. Ba

lan, G

. May

, RW

TH

Aach

en U

nivers

ity, A

ache

n, Ge

rman

y

0930

hrs

AIAA-2

015-2

602

An O

utpu

t-Bas

ed A

dapt

ive

Hybr

idize

d Disc

ontin

uous

Gale

rkin

Meth

od on

Def

ormi

ng D

omain

sK.

Fidko

wski,

Univ

ersity

of M

ichiga

n, An

n Arb

or, An

n Arbo

r, MI

1000

hrs

AIAA-2

015-2

603

An A

djoint

-Bas

ed h

p-Ad

aptiv

e Pe

trov-

Galer

kin M

ethod

for

Turb

ulent

Flow

sB.

Reza

Ahrab

i, W. A

nders

on, J

. New

man,

Unive

rsity

of Te

nnes

see,

Chatt

anoo

ga,

Chatt

anoo

ga, T

N

1030

hrs

AIAA-2

015-2

604

An Ad

aptiv

e Sim

plex C

ut-Ce

ll Meth

od

for H

igh-O

rder

Disco

ntinu

ous G

alerk

in Di

screti

zatio

ns of

Conju

gate

Heat

Trans

fer Pr

oblem

sS.

Ojeda

, H. S

un, S

. Allm

aras,

D. Da

rmofa

l, Ma

ssachu

setts

Institu

te of

Techn

ology,

Ca

mbrid

ge, M

A

1100

hrs

AIAA-2

015-2

605

Impr

oving

High

-Ord

er Fi

nite

Eleme

nt A

ppro

ximat

ion Th

roug

h Ge

ometr

ical W

arpin

gD.

San

jaya,

K. Fid

kows

ki, U

nivers

ity of

Mi

chiga

n, An

n Arbo

r, Ann

Arbo

r, MI

1130

hrs

AIAA-2

015-2

606

Hp-A

dapt

ivity

on A

nisot

ropic

Me

shes

for H

ybrid

ized

Disco

ntinu

ous G

alerk

in Sc

heme

A. Ba

lan, M

. Woo

pen,

G. M

ay, R

WTH

Aa

chen

Univ

ersity

, Aac

hen,

Germ

any

65

Tues

day,

23 Ju

ne 2

015

96-C

FD-1

0Tu

rbule

nt Fl

ow Si

mulat

ions I

Gran

d Ball

room

BCh

aired

by: S

. POR

OSEV

A, Th

e Univ

ersity

of N

ew M

exico

and S

. TIM

ME, T

he U

nivers

ity of

Live

rpool

0900

hrs

AIAA-2

015-2

607

Delay

ed D

etach

ed-Ed

dy Si

mulat

ion

of Sh

ock

Buffe

t on

Half

Wing

-Bod

y Co

nfigu

ratio

nF.

Sarto

r, S. T

imme

, Univ

ersity

of

Liverp

ool, L

iverpo

ol, U

nited

King

dom

0930

hrs

AIAA-2

015-2

608

Flow

Cont

rol o

f a R

otat

ing Cy

linde

r by

the U

se of

a Str

uctu

red S

urfa

ce:

A Vis

ualiz

ation

of Fl

ow St

ructu

res

T. Sc

homb

erg, R

. Ritz

, O. W

ünsch

, Un

iversi

ty of

Kasse

l, Kas

sel, G

erman

y; M.

Ru

etten

, R. K

essle

r, Germ

an Ae

rospa

ce

Cente

r (DL

R), G

ötting

en, G

erman

y

1000

hrs

AIAA-2

015-2

609

Simula

tions

of In

comp

ressi

ble

Sepa

rated

Turb

ulent

Flow

s aro

und

Two-

Dime

nsion

al Bo

dies w

ith

URAN

S Mod

els in

Ope

nFOA

MA.

Porte

ous,

R. Ha

bbit,

J. Co

lmen

ares,

S. Po

rosev

a, Un

iversi

ty of

New

Mexic

o, Alb

uque

rque,

Albuq

uerqu

e, NM

; S.

Murm

an, N

ASA A

mes R

esea

rch Ce

nter,

Moffe

tt Fie

ld, CA

1030

hrs

AIAA-2

015-2

610

Jet p

ump o

ptimi

zatio

n thr

ough

Re

ynold

s ave

rage

d Nav

ier-St

okes

Sim

ulatio

n Ana

lysis

G. Gh

erman

, I. M

alael,

COMO

TI Ro

mania

n Re

search

& De

velop

ment

Institu

te for

Gas

Turbin

es, Bu

chares

t, Rom

ania;

M. M

ihaesc

u, Ro

yal In

stitute

of Te

chnolo

gy (K

TH),

Stockh

olm, S

wede

n; I. P

orumb

el, CO

MOTI

Roma

nian R

esearc

h & De

velop

ment

Institu

te for

Gas T

urbine

s, Bu

chares

t, Rom

ania

Tues

day,

23 Ju

ne 2

015

97-C

FD-1

1Me

shing

Tech

nique

s II

Cora

lCh

aired

by: M

. PAR

K, NA

SA-La

ngley

Rese

arch C

enter

and D

. THO

MPSO

N, M

ississ

ippi S

tate U

nivers

ity09

00 hr

sAIA

A-201

5-261

1Co

mpar

ison

of r-

Adap

tatio

n Te

chniq

ues f

or 2

-D CF

D Ap

plica

tions

W. Ty

son,

J. De

rlaga

, A. C

houd

hary,

C.

Roy,

Virgin

ia Po

lytec

hnic

Institu

te an

d St

ate U

nivers

ity, B

lacks

burg,

VA

0930

hrs

AIAA-2

015-2

612

Imple

ment

ation

of B

all-C

enter

Sp

ring A

nalog

y Mes

h De

form

ation

Te

chniq

ue w

ith CF

D De

sign

Optim

izatio

nY.

Yang

, S. Ö

zgen

, Midd

le Ea

st Te

chnic

al Un

iversi

ty, An

kara,

Turke

y

1000

hrs

AIAA-2

015-2

613

Aniso

tropic

Non

-Unif

orm

Bloc

k-Ba

sed A

dapt

ive M

esh

Refin

emen

t fo

r Thr

ee-D

imen

siona

l Inv

iscid

and

Visco

us Fl

ows

L. Fre

ret, C

. Grot

h, Un

iversi

ty of

Toron

to,

Toron

to, Ca

nada

1030

hrs

AIAA-2

015-2

614

A sh

ifting

disco

ntinu

ous-g

rid-b

lock

lattic

e Bolt

zman

n me

thod

for

movin

g bou

ndar

y sim

ulatio

nsN.

Arora

, A. G

upta,

India

n Ins

titute

of Te

chno

logy D

elhi, N

ew D

elhi, I

ndia;

W.

Shyy

, Hon

g Kon

g Univ

ersity

of S

cienc

e and

Te

chno

logy,

Hong

Kong

, Hon

g Kon

g

1100

hrs

AIAA-2

015-2

615

Nume

rical

simula

tion o

f an X

-wing

fla

pping

wing

MAV

by m

eans

of a

defor

ming

overs

et gr

id me

thod

S. De

ng, D

elft U

nivers

ity of

Techn

ology,

Delft,

Th

e Neth

erlan

ds; T.

Xiao

, Nan

jing Un

iversit

y of

Aeron

autics

and A

stron

autics

, Nan

jing, C

hina;

M. Pe

rcin, B

. van

Oud

heusd

en, H

. Bijl,

B. Re

mes,

Delft

Unive

rsity o

f Tech

nolog

y, De

lft,

The N

etherl

ands

Tues

day,

23 Ju

ne 2

015

98-C

FD-1

2LE

S, DN

S, an

d Hyb

rid R

ANS-

LES I

IEm

erald

Chair

ed by

: N. B

ISEK,

Air Fo

rce Re

seac

h Lab

orator

y and

A. S

ESCU

, Miss

issipp

i Stat

e Univ

ersity

0900

hrs

AIAA-2

015-2

616

Simula

tion

of B

ound

ary L

ayer

flo

ws ov

er B

iofou

led Su

rface

sJ.

Sadiq

ue, X

. Yan

g, C.

Mene

veau

, R.

Mitta

l, Joh

ns H

opkin

s Univ

ersity

, Ba

ltimore

, MD

0930

hrs

AIAA-2

015-2

617

The E

ffect

of In

itial C

ondit

ions o

n Str

eamw

ise Vo

rtice

s in

the P

lane

Turb

ulent

Mixi

ng La

yer

W. M

cMull

an, S

. Garr

ett, U

nivers

ity of

Le

iceste

r, Leic

ester

, Unit

ed Ki

ngdo

m

1000

hrs

AIAA-2

015-2

618

Turb

ulent

inflo

w ge

nera

tion

in sq

uare

duct

at su

perso

nic M

ach

numb

erC.

Rous

sel, F

. Aliz

ard, F

. Gras

so, P

aris

Institu

te of

Tech

nolog

y, Pa

ris, F

rance

1030

hrs

AIAA-2

015-2

619

Furth

er Stu

dies o

f Adv

erse P

ressu

re

Grad

ient E

ffects

in Tu

rbule

nt Ch

anne

l Flo

wsA.

Jesus,

Techn

ologic

al Ins

titute

of Ae

ronau

tics

(ITA)

, São

José

dos C

ampo

s, Bra

zil; L.

Sc

hiavo

, Univ

ersity

of Ca

mpina

s, Ca

mpina

s, Bra

zil; J.

Azev

edo,

Aeron

autics

and S

pace

Ins

titute

(IAE),

São J

osé do

s Cam

pos,

Brazil;

J.

Lava

l, Nati

onal

Cente

r for S

cienti

fic Re

search

(C

NRS)

, Ville

neuv

e d’As

cq, Fr

ance

66

Tues

day,

23 Ju

ne 2

015

99-FD

-10

Boun

dary

-Laye

r Tra

nsitio

nSa

pphir

eCh

aired

by: E

. MAR

INEA

U, AE

DC W

hite O

ak an

d J. K

LENT

ZMAN

, Bay

lor U

nivers

ity09

00 hr

sAIA

A-201

5-262

0Tu

rbule

nt D

ensit

y Fluc

tuat

ions i

n Th

erma

l Bou

ndar

y Lay

ers S

tudie

d via

Mole

cular

Ray

leigh

scat

tering

J. Pa

nda,

NASA

Ames

Rese

arch C

enter

, Mo

ffett

Field,

CA

0930

hrs

AIAA-2

015-2

621

Auto

matic

tran

sition

pred

iction

in

an in

dustr

ial N

avier

-Sto

kes s

olver

us

ing h

igher

-ord

er fi

nite e

lemen

tsR.

Gros

s, F.

Chalo

t, J.

Court

y, M.

Mall

et, D

. Tra

n, Da

ssault

Grou

p, Sa

int Cl

oud,

Franc

e; D.

Arna

l, ONE

RA, T

oulou

se, F

rance

; et a

l.

1000

hrs

AIAA-2

015-2

622

Larg

e-Ed

dy Si

mulat

ion of

Tra

nsitio

nal F

lows o

n a C

ompr

esso

r Bl

ade

Z. Wa

ng, A

viatio

n Ind

ustry

Corpo

ration

of

China

(AVIC

), Sh

angh

ai, Ch

ina

1030

hrs

AIAA-2

015-2

623

A loc

al sca

tterin

g app

roac

h fo

r th

e effe

ct of

abru

pt ch

ange

s on

boun

dary

-laye

r ins

tabil

ity an

d tra

nsitio

n: a

nume

rical

meth

odZ.

Huan

g, Tia

njin U

nivers

ity, T

ianjin

, Chin

a; X.

Wu,

Impe

rial C

olleg

e Lon

don,

Lond

on,

Unite

d King

dom

1100

hrs

AIAA-2

015-2

624

Nume

rical

Simula

tion

of Th

ree-

Dime

nsion

al Wa

ve P

acke

t in

Supe

rsonic

Flow

over

a Co

mpre

ssion

Corn

erA.

Novik

ov, M

osco

w Ins

titute

of Ph

ysics

an

d Tec

hnolo

gy, Z

huko

vsky

, Rus

sia; I

. Eg

orov,

TsAGI

, Zhu

kovs

ky, R

ussia

; A.

Fedo

rov, M

osco

w Ins

titute

of Ph

ysics

and

Tech

nolog

y, Zh

ukov

sky,

Russi

a

1130

hrs

AIAA-2

015-2

625

Comp

utat

ions o

f Dist

urba

nce

Ampli

ficat

ion B

ehind

Isola

ted

Roug

hnes

s Elem

ents

and

Comp

ariso

n wi

th M

easu

reme

nts

M. Ch

oudh

ari, F

. Li, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

; M. B

ynum

, AM

A Res

earch

Asso

ciates

, Ham

pton,

VA; M

. Keg

erise

, R. K

ing, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

1200

hrs

AIAA-2

015-2

626

Acou

stic r

adiat

ion du

e to s

catte

ring

of T-

S wav

e by n

onlin

ear r

ough

ness

in su

bson

ic bo

unda

ry la

yer fl

ows

M. D

ong,

Tianji

n Univ

ersity

, Tian

jin, C

hina;

X. W

u, Im

peria

l Coll

ege L

ondo

n, Lo

ndon

, Un

ited K

ingdo

m

Tues

day,

23 Ju

ne 2

015

100-

FD-1

1Un

stead

y Wing

Aer

odyn

amics

IGo

veno

rs Le

cture

Hall

Chair

ed by

: K. M

OORE

D, Le

high U

nivers

ity an

d M. R

INGU

ETTE

, Univ

ersity

at B

uffalo

0900

hrs

AIAA-2

015-2

627

Deve

lopme

nt of

cohe

rent

stru

cture

s wi

thin

the l

amina

r sep

arat

ion

bubb

le of

a NA

CA00

18 ai

rfoil

J. Ku

relek

, A. L

ambe

rt, S

. Yaru

sevy

ch,

Unive

rsity

of Wa

terloo

, Wate

rloo,

Cana

da

0930

hrs

AIAA-2

015-2

628

Analy

zing V

ortex

Dyn

amics

in th

e La

mina

r Sep

arat

ion B

ubble

vis

Surfa

ce P

ressu

re M

easu

reme

nts

A. La

mbert

, S. Y

aruse

vych

, Univ

ersity

of

Water

loo, W

aterlo

o, Ca

nada

1000

hrs

AIAA-2

015-2

629

Analy

sis of

cruis

e fligh

t of t

he

callio

pe h

ummi

ngbir

dJ.

Song

, H. L

uo, V

ande

rbilt U

nivers

ity,

Nash

ville,

TN; B

. Tob

alske

, Univ

ersity

of

Monta

na, M

issou

la, M

issou

la, M

T; T.

Hedri

ck, U

nivers

ity of

Nort

h Caro

lina,

Chap

el Hil

l, Cha

pel H

ill, N

C

1030

hrs

AIAA-2

015-2

630

Topo

logy a

nd Fl

ow St

ructu

res o

f Th

ree-

Dime

nsion

al Se

para

tion

Bubb

les: T

he Ef

fect

of A

spec

t Rat

ioS.

Hos

seinv

erdi, R

. Jac

obi, H

. Fas

el,

Unive

rsity

of Ari

zona

, Tuc

son,

Tucso

n, AZ

Tues

day,

23 Ju

ne 2

015

101-

FD-1

2Ai

rfoil S

epar

ation

Cont

rol

Sena

tors

Lectu

re H

allCh

aired

by: M

. VISB

AL, U

SAF A

FRL/

RQVA

and K

. TAIR

A, Flo

rida S

tate U

nivers

ity09

00 hr

sAIA

A-201

5-263

1Mo

delin

g Lift

Hyste

resis w

ith a

Modifi

ed G

oman

-Khr

abro

v Mod

el on

Pit

ching

Airfo

ilsD.

Willia

ms, Il

linois I

nstitu

te of

Techn

ology,

Ch

icago

, IL; F.

Reiss

ner, T

echnic

al Un

iversit

y of

Berlin

, Berl

in, Ge

rman

y; D.

Green

blatt,

H. Mu

ehler

-Vahl,

Techn

ion--Is

rael In

stitute

of

Techn

ology,

Haifa

, Israe

l; C. S

trang

feld,

Techn

ical U

nivers

ity of

Berlin

, Berl

in, Ge

rman

y

0930

hrs

AIAA-2

015-2

632

Surfa

ce vo

rticit

y flux

analy

sis in

se

para

tion

cont

rol o

n NA

CA 0

012

airfo

ilP.

Mund

ay, K

. Tair

a, Flo

rida S

tate

Unive

rsity,

Talla

hasse

e, FL

1000

hrs

AIAA-2

015-2

633

Meas

urem

ents

of 3

-D St

all Ce

lls on

2-

D Ai

rfoil

E. De

mauro

, H. D

ell’O

rso, V

. Siva

neri,

B.

Tuna

, M. A

mitay

, Ren

sselae

r Poly

techn

ic Ins

titute,

Troy

, NY

1030

hrs

AIAA-2

015-2

634

Inter

actio

ns of

a Lo

w As

pect

Ratio

Dy

nami

c Pin

with

a La

mina

r Bo

unda

ry La

yer

S. G

ilders

leeve

, C. L

eong

, M. A

mitay

, Re

nsse

laer P

olytec

hnic

Institu

te, Tr

oy, N

Y

1100

hrs

AIAA-2

015-2

635

Simula

tion

of a

Lami

nar-F

low

Comp

atibl

e High

-Lift

Confi

gura

tion

with

Flow

Cont

rol

D. Ri

zzett

a, M.

Visb

al, Ai

r Forc

e Res

earch

La

borat

ory, W

right-

Patte

rson A

FB, O

H

1130

hrs

AIAA-2

015-2

636

Glob

al sta

bility

analy

sis of

a co

mpre

ssible

turb

ulent

flow

arou

nd

a high

-lift

confi

gura

tion

M. Io

rio, A

irbus

, Mad

rid, S

pain;

L.

Gonz

alez,

Tech

nical

Unive

rsity

of Ma

drid,

Madri

d, Sp

ain; A

. Mart

inez,

Airbu

s, Fil

ton,

Unite

d King

dom

67

Tues

day,

23 Ju

ne 2

015

102-

FD-1

3Sh

ock-

Domi

nated

Flow

sTo

paz

Chair

ed by

: M. G

AMBA

, Univ

ersity

of M

ichiga

n and

J. PO

GGIE,

USA

F AFR

L/RB

AC09

00 hr

sAIA

A-201

5-263

7As

sessi

ng B

last L

oadin

g With

in Ob

stacle

Arra

ysD.

Mott

, Nav

al Re

searc

h Lab

orator

y, Wa

shing

ton, D

C; T.

Youn

g, Be

rkeley

Re

searc

h Asso

ciates

, Belt

sville

, MD;

D.

Sch

wer, P

. Mati

c, Na

val R

esea

rch

Labo

ratory

, Was

hingto

n, DC

0930

hrs

AIAA-2

015-2

638

Study

of B

ow-S

hock

Insta

bilitie

s in

front

of H

emisp

heric

al Sh

ell at

Hy

perso

nic M

ach

Numb

er 7

A. Va

shish

tha, U

nivers

ity of

Toky

o, Ka

shiw

a, Ja

pan;

Y. Wa

tanab

e, Un

iversi

ty of

Toky

o, Bu

nkyo

, Jap

an; K

. Suz

uki,

Unive

rsity

of To

kyo,

Kash

iwa,

Japa

n

1000

hrs

AIAA-2

015-2

639

HIFiR

E-1 Tu

rbule

nt Sh

ock

Boun

dary

La

yer I

nter

actio

n -Fl

ight D

ata a

nd

Comp

utat

ions

R. Kim

mel, A

ir Forc

e Res

earch

Labo

ratory

, W

right-

Patte

rson A

FB, O

H; D

. Prab

hu, E

RC,

Inc.,

Moffe

tt Fie

ld, CA

1030

hrs

AIAA-2

015-2

640

Nume

rical

Simula

tion

Explo

ring

Supe

rsonic

Flow

Ove

r a W

all-

Moun

ted H

alf-C

ylind

er Tu

rret

P. Mo

rgan,

Ohio

Aeros

pace

Insti

tute,

Dayto

n, OH

; M. V

isbal,

Air F

orce R

esea

rch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH

1100

hrs

AIAA-2

015-2

641

Nume

rical

Inve

stiga

tion

of Sh

ock-

induc

ed La

mina

r Sep

arat

ion B

ubble

in

Supe

rsonic

Flow

sJ.

Sivas

ubram

anian

, H. F

asel,

Univ

ersity

of

Arizo

na, T

ucso

n, Tu

cson,

AZ

1130

hrs

AIAA-2

015-2

642

On u

nstea

dy sh

ock

wave

refle

ction

s fro

m we

dges

with

stra

ight a

nd

conc

ave t

ipsF.

Alzam

ora Pr

evita

li, E.

Timofe

ev, M

cGill

Unive

rsity,

Mon

tréal,

Cana

da; H

. Klei

ne,

Unive

rsity

of Ne

w So

uth W

ales a

t the

Au

strali

an D

efenc

e Forc

e Aca

demy

, Ca

nberr

a, Au

strali

a

Tues

day,

23 Ju

ne 2

015

103-

ITAR-

1ITA

R - H

yper

sonic

Flow

Phe

nome

na (I

nvite

d)

Moro

ccoCh

aired

by: K

. CAS

PER

0900

hrs

Oral

Prese

ntatio

nHT

V-2

Boun

dary

Laye

r Tra

nsitio

n -

Summ

ary a

nd Le

ssons

Lear

ned

R. Kim

mel, A

ir Forc

e Res

earch

Labo

ratory

, W

right-

Patte

rson A

FB, O

H

0930

hrs

Oral

Prese

ntatio

nST

ABL-3

D So

ftwar

e Ove

rview

H. Jo

hnso

n, Go

Hype

rsonic

, Inc

., Mi

nnea

polis,

MN

1000

hrs

Oral

Prese

ntatio

nMa

ch 1

0 Bo

unda

ry La

yer T

rans

ition

Expe

rimen

ts on

Shar

p and

Blun

ted

Cone

sE.

Marin

eau,

D. Le

wis,

J. La

fferty

, G.

Morar

u, Arn

old En

ginee

ring D

evelo

pmen

t Ce

nter, S

ilver

Sprin

g, MD

1030

hrs

Oral

Prese

ntatio

nSta

bility

Ana

lysis

of H

yper

sonic

Flo

ws U

sing S

TABL

-3D

B. W

heato

n, Jo

hns H

opkin

s Univ

ersity

Ap

plied

Phys

ics La

borat

ory, L

aurel

, MD;

H.

John

son,

GoHy

perso

nic, I

nc.,

Dayto

n, OH

; R.

Wagn

ild, S

andia

Nati

onal

Labo

ratori

es,

Albuq

uerqu

e, NM

Tues

day,

23 Ju

ne 2

015

104-

MAO-

3Ap

plica

tions

IMa

drid

Chair

ed by

: A. N

AJAF

I, AN

SYS,

Inc.

and P

. PIPE

RNI,

Bomb

ardier

Inc

0900

hrs

AIAA-2

015-2

646

Optim

izatio

n of

Syste

m Ev

olvab

ility

Unde

r Unc

erta

inty

J. Wa

tson,

J. All

en, C

. Matt

son,

Brigh

am

Youn

g Univ

ersity

, Prov

o, UT

; S. F

ergus

on,

North

Carol

ina S

tate U

nivers

ity, R

aleigh

, NC

0930

hrs

AIAA-2

015-2

647

An A

pplic

ation

of Co

ncep

tual

Desig

n an

d Mult

idisci

plina

ry

Analy

sis Tr

ansit

ioning

to D

etaile

d De

sign

Stage

sA.

Renn

er, F.

Thom

pson

, V. K

aliva

rapu,

E. W

iner, J

. Oliv

er, Io

wa S

tate U

nivers

ity,

Ames

, IA;

B. G

ilmore

, Dee

re &

Comp

any,

Molin

e, IL;

et al

.

1000

hrs

AIAA-2

015-2

648

Geom

etry D

riven

High

Fide

lity

Stabil

ity D

eriva

tives

Obtai

ned U

sing

Autom

ated C

FD An

alysis

Proc

essN.

Bhag

at, W

right

State

Unive

rsity,

Beav

ercree

k, OH

; E. A

lyana

k, Air

Force

Re

search

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH

; D. A

llison

, Opti

mal F

light S

cience

s, LLC

, Da

yton,

OH

1030

hrs

AIAA-2

015-2

649

Appli

catio

n of

auto

matic

algo

rithm

ge

nera

tion

to ai

r-to-

air re

fueli

ng

sched

uling

R. En

tz, G

. Sch

erer S

chwe

ning,

R. Fe

rnand

es de

Oliv

eira,

Airbu

s, Mu

nich,

Germ

any

1100

hrs

AIAA-2

015-2

650

Multid

iscipl

inary

and M

ultile

vel

Aircr

aft D

esign

Meth

odolo

gy

Using

Enha

nced

Colla

bora

tive

Optim

izatio

nP.

Albuq

uerqu

e, P.

Gamb

oa, M

. Silv

estre

, Un

iversi

ty of

Beira

Inter

ior, C

ovilh

a, Po

rtuga

l

1130

hrs

AIAA-2

015-2

651

Deve

lopme

nt of

a Ja

va-b

ased

fra

mewo

rk fo

r airc

raft

preli

mina

ry

desig

n an

d opt

imiza

tion

F. Nic

olosi,

A. D

e Marc

o, L.

Attan

asio,

D.

Gam

barde

lla, U

nivers

ity of

Nap

les

“Fed

erico

II”, N

aples

, Ital

y

Tues

day,

23 Ju

ne 2

015

105-

MST-5

Guida

nce,

Cont

rol, a

nd D

ynam

ics II

Trave

rtine

Chair

ed by

: T. A

LEXE

EV, U

nivers

ity of

Califo

rnia D

avis

and J

. KNO

WLE

S, Lo

ughb

oroug

h Univ

ersity

0900

hrs

AIAA-2

015-2

652

Semi

-Impli

cit N

umer

ical

Simula

tions

of N

onlin

ear D

ynam

ics

of B

eams

, Plat

es, a

nd Sh

ells

T. Ale

xeev

, Siem

ens E

nergy

, Inc

., Bo

ulder,

CO

; M. H

afez,

Unive

rsity

of Ca

liforni

a, Da

vis, D

avis,

CA

0930

hrs

AIAA-2

015-2

653

A Bi

furca

tion

Study

of a

Dyna

mic

Mode

l of a

Nos

e Lan

ding G

ear

Mech

anism

Subje

cted t

o Ext

erna

l Di

sturb

ance

sJ.

Know

les, L

ough

borou

gh U

nivers

ity,

Loug

hboro

ugh,

Unite

d King

dom;

E.

Coetz

ee, A

irbus

, Bris

tol, U

nited

King

dom

1000

hrs

AIAA-2

015-2

654

Multi-

Fideli

ty Sim

ulatio

n of C

argo

Air

drop

: Fro

m the

Paylo

ad Ba

y to t

he

Grou

ndT.

Jann,

S. Ge

isbau

er, N

. Bier,

Germ

an

Aeros

pace

Cente

r (DL

R), B

raunsc

hweig

, Ge

rman

y; W.

Krüg

er, H.

Schm

idt, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Gött

ingen

, Germ

any

1030

hrs

AIAA-2

015-2

655

Cont

rol E

nhan

ced a

nd

Para

meter

ized L

oad R

elief

tec

hnolo

gy fo

r a La

unch

Vehic

leW.

Yang

, S. T

ang,

Z. Xu

, Nort

hwes

tern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

1100

hrs

AIAA-2

015-2

656

The m

ode s

witch

cont

rol r

esea

rch

of sm

all-ty

pe pa

ralle

l TBC

C eng

ine

base

d on

SQP

meth

odQ.

Xiao

jie, W

. Su,

Y. Ta

ng, A

viatio

n Ind

ustry

Corpo

ration

of Ch

ina (A

VIC),

Wux

i, Chin

a

68

Tues

day,

23 Ju

ne 2

015

106-

NW-3

09

00 -

0930

hrs

Netw

orkin

g Cof

fee B

reak

Chan

tilly B

allro

om Ea

st

Tues

day,

23 Ju

ne 2

015

107-

PDL-4

Plasm

a Assi

sted C

ombu

stion

Miro

Chair

ed by

: K. X

U, U

nivers

ity of

Alab

ama i

n Hun

tsville

0900

hrs

AIAA-2

015-2

657

Electr

on Te

mper

atur

e in

a Me

than

e-Ai

r Flam

e und

er a

DC

Electr

ic Fie

ldS.

Jaco

bs, K

. Xu,

Unive

rsity

of Ala

bama

, Hu

ntsvil

le, H

untsv

ille, A

L

0930

hrs

AIAA-2

015-2

658

Lase

r-Ind

uced

Hea

ting U

sing a

No

n-Re

sona

nt D

ual-P

ulse A

ppro

ach

with

App

licat

ion to

Lase

r Ign

ition

C. Du

mitra

che,

C. Ro

se, A

. Yali

n, Co

lorad

o St

ate U

nivers

ity, F

ort Co

llins,

CO

1000

hrs

AIAA-2

015-2

659

Magn

etic p

ositio

ning o

f the

ele

ctric

disch

arge

in th

e volu

me of

su

perso

nic fl

owA.

Firso

v, Ru

ssian

Acad

emy o

f Scie

nces

, Mo

scow,

Russi

a; S.

Leon

ov, U

nivers

ity of

No

tre D

ame,

Notre

Dam

e, IN

1030

hrs

AIAA-2

015-2

660

Towa

rds L

aser

Ignit

ion by

Rap

id He

ating

of W

ater

Vapo

rC.

Dumi

trach

e, A.

Yalin

, Colo

rado S

tate

Unive

rsity,

Fort

Collin

s, CO

1100

hrs

AIAA-2

015-2

661

Multip

hysic

s sim

ulatio

ns of

plas

ma-

assis

ted co

mbus

tion

dyna

mics

in a

direc

t-cou

pled m

icrow

ave r

eacto

rA.

Palla

, J. Z

imme

rman

, D. C

arroll

, CU

Aeros

pace

, Cha

mpaig

n, IL;

C. M

itsing

as,

S. H

amma

ck, T

. Lee

, Univ

ersity

of Ill

inois,

Ur

bana

-Cham

paign

, Urba

na, I

L

1130

hrs

AIAA-2

015-2

662

Inve

stiga

tion

of Th

erma

l Cyc

ling

Prop

erty

of Th

erma

l Bar

rier

Coat

ings w

ith La

ser D

epos

ited M

esh

Struc

ture

S. S

hi, W

. Che

n, Z.

Hong

, D. G

ao, A

viatio

n Ind

ustry

Corpo

ration

of Ch

ina (A

VIC),

Shan

ghai,

China

Tues

day,

23 Ju

ne 2

015

108-

TP-5

Plasm

a and

Arc

Jet T

estin

g, Di

agno

stics

and C

ompu

tatio

nal M

ethod

sRo

setta

Chair

ed by

: M. W

INTE

R, Un

iversi

ty of

Kentu

cky a

nd P.

YEE

, The

Aeros

pace

Corpo

ration

0900

hrs

AIAA-2

015-2

663

Arc J

et Fa

cility

Test

Cond

ition

Pred

iction

s Usin

g the

ADS

I Cod

eG.

Palm

er, D

. Prab

hu, E

RC, I

nc.,

Hunts

ville,

AL

; I. T

erraz

as-Sa

linas

, NAS

A Ame

s Re

searc

h Cen

ter, M

offett

Field

, CA

0930

hrs

AIAA-2

015-2

664

Comp

ariso

ns of

PICA

In-de

pth M

ateria

l Pe

rform

ance

and A

blator

Resp

onse

Mo

delin

g fro

m ME

DLI A

rc Je

t Test

sD.

Smith

, Univ

ersity

of Ke

ntucky

, Lex

ington

, Lex

ington

, KY;

T. Wh

ite, E

RC, In

c., M

offett

Fie

ld, CA

; A. M

artin,

Unive

rsity o

f Ken

tucky,

Lex

ington

, Lex

ington

, KY

1000

hrs

AIAA-2

015-2

665

Enab

ling t

he St

atist

ical C

alibr

ation

of

Acti

ve N

itrida

tion

of G

raph

ite by

At

omic

Nitro

gen

P. Ba

uman

, Stat

e Univ

ersity

of N

ew Yo

rk,

Buffa

lo, N

Y

1030

hrs

AIAA-2

015-2

666

Side A

rm R

eacto

r Stu

dy of

Copp

er

Cata

lysis

D. D

river,

NAS

A Ame

s Res

earch

Cente

r, Mo

ffett

Field,

CA; S

. Sep

ka, E

RC, I

nc.,

Moffe

tt Fie

ld, CA

1100

hrs

AIAA-2

015-2

667

Cons

olida

ting N

ASA’s

Arc-

Jet

J. Ba

lboni,

T. G

okce

n, F.

Hui, P

. Grau

be, P

. Mo

rrisse

y, NA

SA Am

es Re

searc

h Cen

ter,

Moffe

tt Fie

ld, CA

; R. L

ewis,

NAS

A Joh

nson

Sp

ace C

enter

, Hou

ston,

TX

1130

hrs

AIAA-2

015-2

668

Phys

ico-C

hemi

stry o

f CN

in th

e Bo

unda

ry La

yer o

f Gra

phite

in

Nitro

gen

Plasm

asB.

Helb

er, T.

Ales

sand

ro, O

. Cha

zot,

M.

Thier

ry, vo

n Kárm

án In

stitut

e for

Fluid

Dyna

mics,

Rhod

e-Sain

t-Gen

èse,

Belgi

um

Tues

day,

23 Ju

ne 2

015

109-

F360

-3

0930

- 12

00 h

rsDa

y in

the L

ife of

Ope

ratio

ns -

Effe

ctive

ly Ma

nagin

g Disr

uptio

nGr

and B

allro

om E

Mode

rator:

Neil

Plan

zer, V

ice Pr

eside

nt, Ai

r Traf

fic M

anag

emen

t, Bo

eing C

omme

rcial

Airpla

nes

Pane

lits:

Tim Ca

mpbe

llSe

nior V

ice Pr

eside

nt, Ai

r Ope

ration

sAm

erica

n Airli

nes

Jim Cr

ites

Exec

utive

Vice

Pres

ident

of Op

eratio

nsDF

W In

terna

tiona

l Airp

ort

Brian

Quigl

eyMa

nagin

g Dire

ctor F

light

Opera

tions

Unite

d Airli

nes

Dan

Smile

yVic

e Pres

ident

for S

ystem

s Ope

ration

s, Fe

deral

Aviat

ion

Admi

nistra

tion A

ir Traf

fic O

ffice

Tues

day,

23 Ju

ne 2

015

111-

LNCH

-1

1230

- 14

00 h

rsAw

ards

Lunc

heon

: Cele

brat

ing A

chiev

emen

ts in

Aero

spac

e Scie

nces

Chan

tilly B

allro

om W

est

A tick

et is

requir

ed an

d inc

luded

in th

e con

feren

ce re

gistra

tion f

ee w

here

indica

ted.

69

Tues

day,

23 Ju

ne 2

015

112-

AA-1

6CA

A So

und G

ener

ation

IIFle

ur-d

e-lis

ACh

aired

by: J

. DEL

FS, D

LR - G

erman

Aeros

pace

Cente

r14

00 hr

sAIA

A-201

5-266

9Pr

edict

ion of

low-

spee

d fan

tra

iling-

edge

nois

e bas

ed on

RAN

S an

d on

scale

reso

lved s

imula

tions

G. G

rasso

, J. C

hristo

phe,

C. Sc

hram,

von

Kárm

án In

stitut

e for

Fluid

Dyna

mics,

Rh

ode-S

aint-G

enès

e, Be

lgium

1430

hrs

AIAA-2

015-2

670

Synt

hetic

Turb

ulenc

e Meth

ods f

or

Lead

ing Ed

ge N

oise P

redic

tions

F. Ge

a-Agu

ilera,

X. Z

hang

, X. C

hen,

J. Gil

l, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom;

T. N

odé-L

anglo

is, Ai

rbus,

Toulo

use,

Franc

e

1500

hrs

AIAA-2

015-2

671

Pred

iction

of Sl

at B

road

band

Nois

e wi

th R

ANS R

esult

sB.

Bai,

X. L

i, Y. G

uo, B

eihan

g Univ

ersity

, Be

ijing,

China

; F. T

hiele,

Tech

nical

Unive

rsity

of Be

rlin, B

erlin,

Germ

any

1530

hrs

AIAA-2

015-2

672

Towa

rds h

igh-li

ft no

ise fr

om Fa

st Mu

ltipole

BEM

with

aniso

tropic

sy

nthe

tic tu

rbule

nce s

ource

sN.

Reich

e, M.

Lumm

er, R.

Ewert

, Germ

an

Aeros

pace

Cente

r (DL

R), B

rauns

chwe

ig,

Germ

any

1600

hrs

AIAA-2

015-2

673

Comp

act A

ssump

tion

Appli

ed to

th

e Mon

opole

Term

of Fa

rassa

t’s

Form

ulatio

nL.

Lope

s, NA

SA La

ngley

Rese

arch C

enter

, Ha

mpton

, VA

1630

hrs

AIAA-2

015-2

674

Cent

rifug

al Co

mpre

ssor:

The S

ound

of

Surg

eE.

Sund

ström

, M. M

ihaes

cu, R

oyal

Institu

te of

Tech

nolog

y (KT

H), S

tockh

olm,

Swed

en

Tues

day,

23 Ju

ne 2

015

113-

AA-1

7CA

A Pr

opag

ation

and S

catte

ring I

Fleur

-de-

lis B

Chair

ed by

: S. C

ARO,

CD-Ad

apco

1400

hrs

AIAA-2

015-2

675

Dire

ct an

d inv

erse

unc

erta

inty

quan

tifica

tion

of ac

ousti

c ref

racti

on

phen

omen

a thr

ough

a sh

ear l

ayer

P. Cin

nella

, Univ

ersità

del S

alento

, Lec

ce,

Italy;

X. G

loerfe

lt, X.

Merl

e, Pa

ris In

stitut

e of

Tech

nolog

y, Pa

ris, F

rance

1430

hrs

AIAA-2

015-2

676

Stabil

ized T

ime-

doma

in Im

peda

nce

Mode

l and

the A

pplic

ation

in

Bypa

ss Du

ct No

ise Si

mulat

ions

X. Li

u, X.

Hua

ng, P

eking

Univ

ersity

, Be

ijing,

China

1500

hrs

AIAA-2

015-2

677

Evalu

ation

and D

evelo

pmen

t of

Non

-Refl

ectiv

e Bou

ndar

y Co

nditio

ns fo

r Aer

oaco

ustic

Sim

ulatio

nsJ.

Gill, R

. Fatt

ah, X

. Zha

ng, U

nivers

ity

of So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1530

hrs

AIAA-2

015-2

678

Imple

ment

ation

of a

surfa

ce ba

sed

coup

ling a

ppro

ach

in a h

igh-o

rder

DG

aero

acou

stics

prop

agat

ion

solve

rM.

Muri

el Gr

acia,

W. D

e Roe

ck, W

. De

smet,

Catho

lic Un

iversi

ty of

Leuv

en,

Leuv

en, B

elgium

1600

hrs

AIAA-2

015-2

679

Acou

stic S

catte

ring M

atric

es fo

r Hi

gher

-Ord

er M

odes

for S

imple

Or

ifice

Confi

gura

tions

with

Flow

C. Te

mmler

, M. S

chulz

e, T.

Satte

lmay

er,

Tech

nical

Unive

rsity

of Mu

nich,

Munic

h, Ge

rman

y

1630

hrs

AIAA-2

015-2

680

Nume

rical

asse

ssmen

t of t

he

scatte

ring o

f aco

ustic

wav

es by

tu

rbule

nt st

ructu

res

V. Cla

ir, G.

Gab

ard, U

nivers

ity of

So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1700

hrs

AIAA-2

015-2

681

Enha

ncem

ents

of a

time-

doma

in eq

uivale

nt so

urce

meth

od fo

r ac

ousti

c sca

tterin

gS.

Swi

ft, G

. Blai

sdell

, Purd

ue U

nivers

ity,

West

Lafay

ette,

IN; A

. Lyri

ntzis,

Embry

-Rid

dle Ae

ronau

tical

Unive

rsity,

Day

tona

Beac

h, FL

Tues

day,

23 Ju

ne 2

015

114-

AA-1

8Ge

nera

l Aco

ustic

s IIn

vern

ess

Chair

ed by

: C. B

AILLY,

Ecole

Centr

ale de

Lyon

1400

hrs

AIAA-2

015-2

682

Soun

d and

Dist

ortio

n Pr

oduc

ed

by a

Brak

ing R

otor

Ope

ratin

g in

a Plan

ar B

ound

ary L

ayer

with

Ap

plica

tion

to W

ind Tu

rbine

sH.

Murr

ay, D

. Wisd

a, W.

Alex

ande

r, M.

Nelso

n, W.

Dev

enpo

rt, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA

; S. G

legg,

Florid

a Atla

ntic U

nivers

ity,

Boca

Raton

, FL

1430

hrs

AIAA-2

015-2

683

Nozz

le-to

-Gro

und D

istan

ce Ef

fect

on N

ondo

mina

ted So

lution

s of

Multio

bjecti

ve A

eroa

cous

tic Fl

ame

Defle

ctor D

esign

Pro

blem

T. Ta

tsuka

wa, T

. Non

omura

, A. O

yama

, K.

Fujii,

Japa

n Aero

spac

e Exp

lorati

on Ag

ency

(JA

XA),

Kana

gawa

, Jap

an

1500

hrs

AIAA-2

015-2

684

The A

cous

tic En

viron

ment

of th

e NA

SA G

lenn

9- by

15-

Foot

Low-

Spee

d Wind

Tunn

elD.

Step

hens

, NAS

A Glen

n Res

earch

Cente

r, Cle

velan

d, OH

1530

hrs

AIAA-2

015-2

685

Sonic

Boo

m As

sessm

ent o

f a

Hype

rsonic

Tran

spor

t Veh

icle w

ith

Adva

nced

Num

erica

l Meth

ods

D. Lu

quet,

R. M

archia

no, F

. Cou

louvra

t, Pie

rre an

d Mari

e Curi

e Univ

ersity

, Pari

s, Fra

nce;

I. Sa

lah El

Din,

ONE

RA, M

eudo

n, Fra

nce;

A. Lo

seille

, Fren

ch N

ation

al Ins

titute

for Re

searc

h in C

ompu

ter S

cienc

e an

d Con

trol (

INRIA

), Le

Ches

nay,

Franc

e

Tues

day,

23 Ju

ne 2

015

115-

AA-1

9Ai

rfram

e Nois

e II

Laliq

ueCh

aired

by: C

. DOO

LAN,

The U

nivers

ity of

Adela

ide14

00 hr

sAIA

A-201

5-268

6Ae

roac

ousti

c Sim

ulatio

ns of

a S

impli

fied H

igh-Li

ft De

vice

Acco

untin

g for

Insta

llatio

ns Ef

fects

P. Sa

las, S

. More

au, U

nivers

ity of

Sh

erbroo

ke, S

herbr

ooke

, Can

ada

1430

hrs

AIAA-2

015-2

687

Aero

dyna

mic N

oise S

imula

tion

of an

Airf

oil in

a Pe

riodic

ally

Fluctu

ating

Free

strea

mY.

Yauw

enas

, N. A

hmed

, Univ

ersity

of N

ew

South

Wale

s, Ke

nsing

ton, A

ustra

lia

1500

hrs

AIAA-2

015-2

688

Wall P

ressu

re Sp

ectra

on a

DU96

-W-1

80 P

rofil

e Fro

m Lo

w to

Pr

e-Sta

ll Ang

les of

Atta

ckA.

Surya

di, M

. Herr

, Germ

an Ae

rospa

ce

Cente

r (DL

R), B

rauns

chwe

ig, G

erman

y

1530

hrs

AIAA-2

015-2

689

Supp

ressi

on of

spur

ious n

oise

sour

ces i

n air

foil s

elf-n

oise

meas

urem

ents

M. Tu

instra

, Nati

onal

Aeros

pace

Labo

ratory

(N

LR),

Emme

loord,

The N

etherl

ands

; P.

Sijtsm

a, Pie

ter S

ijtsma

Adva

nced

Ae

roAco

ustic

s, We

zep,

The N

etherl

ands

1600

hrs

AIAA-2

015-2

690

A pa

rame

tric e

xper

imen

tal s

tudy

of

jet-fl

ap in

terac

tion

noise

for a

re

alisti

c sma

ll-sca

le sw

ept w

ing

mode

lI.

Belya

ev, G

. Fara

noso

v, N.

Ostr

ikov,

TsAGI

, Mos

cow,

Russi

a; G.

Paran

in, O

JS

Irkut

Corpo

ration

, Mos

cow,

Russi

a

1630

hrs

AIAA-2

015-2

691

Airfr

ame S

hieldi

ng of

Non

comp

act

Aviat

ion N

oise S

ource

s: Th

eory

and

Expe

rimen

tN.

Ostr

ikov,

S. D

eniso

v, TsA

GI, M

osco

w,

Russi

a

1700

hrs

AIAA-2

015-2

692

Asses

smen

t of C

oncep

tual N

oise

Redu

ction

Dev

ices f

or A

Main

Land

ing

Gear

using

SNGR

Meth

odH.

Yao,

L. Da

vidson

, Cha

lmers

Unive

rsity o

f Tec

hnolo

gy, Gö

teborg

, Swe

den;

S. Pe

ng,

Swed

ish De

fense

Resea

rch Ag

ency

(FOI)

, Sto

ckholm

, Swe

den;

F. Cap

izzan

o, M.

Ba

rbarin

o, G.

Ming

ione,

Italian

Aeros

pace

Re

search

Cente

r (CIR

A), C

apua

, Italy

70

Tues

day,

23 Ju

ne 2

015

116-

AA-2

0Du

ct Ac

ousti

cs III

Obeli

sk A

Chair

ed by

: C. R

OYAL

TY, H

oney

well I

nterna

tiona

l, Inc

.14

00 hr

sAIA

A-201

5-269

3Mo

delin

g of B

road

band

Line

rs Ap

plied

to th

e Adv

ance

d Nois

e Co

ntro

l Fan

D. N

ark, M

. Jon

es, N

ASA L

angle

y Res

earch

Ce

nter, H

ampto

n, VA

; D. S

utliff,

NAS

A Gle

nn Re

searc

h Cen

ter, C

levela

nd, O

H

1430

hrs

AIAA-2

015-2

694

Desig

n Op

timiza

tion

of B

road

band

Ac

ousti

c Line

rs Th

roug

h Fin

ite

Eleme

nt Ef

ficac

y Stu

dies

K. Mi

tchell

, Virg

inia P

olytec

hnic

Institu

te an

d Stat

e Univ

ersity

, Blac

ksbu

rg, VA

1500

hrs

AIAA-2

015-2

695

Effect

of Po

rosit

y and

Joint

Bias

-gr

azing

Flow

on th

e Aco

ustic

Dam

ping

Perfo

rman

ce of

Doub

lean

d Sing

le-lay

er Pe

rfora

ted Li

ners

C. Ji,

D. Zh

ao, S

. Li, X

. Li, N

anya

ng

Techn

ologic

al Un

iversit

y, Sin

gapo

re, Si

ngap

ore

1530

hrs

AIAA-2

015-2

696

Nonli

near

impe

danc

e mod

eling

of

reso

nato

r with

high

inten

sity

incide

nt ac

ousti

c wav

eJ.

Xu, X

. Li, Y

. Guo

, Beih

ang U

nivers

ity,

Beijin

g, Ch

ina

1600

hrs

AIAA-2

015-2

697

Evalu

ation

of Va

riable

-Dep

th

Liner

Confi

gura

tions

for I

ncre

ased

Br

oadb

and N

oise R

educ

tion

M. Jo

nes,

W. W

atson

, D. N

ark, B

. Ho

werto

n, NA

SA La

ngley

Rese

arch C

enter

, Ha

mpton

, VA

Tues

day,

23 Ju

ne 2

015

117-

ACD-

3Ai

rcraf

t Per

form

ance

Stud

iesWy

ethCh

aired

by: C

. BIL,

RMIT

Unive

rsity

and W

. ANE

MAAT,

DAR

corpo

ration

1400

hrs

AIAA-2

015-2

698

The I

mpac

t of A

TTCS

on R

educ

ed-

Thru

st Ta

keof

f Fiel

d Per

form

ance

T. Ta

kaha

shi, A

rizon

a Stat

e Univ

ersity

, Te

mpe,

AZ

1430

hrs

AIAA-2

015-2

699

Unce

rtaint

y Mod

eling

and

Asse

ssmen

t in

Aircr

aft E

vacu

ation

Sim

ulatio

nR.

Silva

, D. F

errari

, Tec

hnolo

gical

Institu

te of

Aeron

autic

s (ITA

), Sã

o Jos

é dos

Ca

mpos

, Braz

il; L.

Santo

s, Em

braer,

São

Jo

sé do

s Cam

pos,

Braz

il

1500

hrs

AIAA-2

015-2

700

Simula

ted Ti

ltrot

or A

ircra

ft Op

erat

ion in

Clos

e Pro

ximity

to a

Build

ing in

Wind

and G

roun

d-Ef

fect

Cond

itions

L. Yo

ung,

NASA

Ames

Rese

arch C

enter

, Mo

ffett

Field,

CA

1530

hrs

AIAA-2

015-2

701

Optim

al Cli

mb Tr

ajecto

ries T

hrou

gh

Expli

cit Si

mulat

ionT.

Taka

hash

i, Ariz

ona S

tate U

nivers

ity,

Temp

e, AZ

1600

hrs

AIAA-2

015-2

702

Desig

n fo

r Res

ilienc

e in

Auto

nomo

us Sy

stems

: Les

sons

Le

arne

d fro

m Co

ntro

lled F

light

into

Sta

ll Acci

dent

sL.

Sherr

y, Ge

orge M

ason

Univ

ersity

, Fa

irfax,

VA

1630

hrs

AIAA-2

015-2

703

Adap

tive a

nd In

tellig

ent p

ower

co

ntro

l allo

catio

n an

d sch

eduli

ng

for a

Mor

e Elec

tric A

ircra

ftS.

Laza

rus, E

aton C

orpora

tion,

Pune

, Ind

ia; S

. Fris

chem

eier, M

. Holl

and,

J. Sk

inner,

A. S

mith,

Eaton

Corpo

ration

, Ja

ckso

n, MS

Tues

day,

23 Ju

ne 2

015

118-

AFM-

7Fli

ght T

est,

Syste

m Id

entifi

catio

n, an

d Par

amete

r Esti

matio

nPlu

m Bl

osso

m A

Chair

ed by

: J. G

RAUE

R, NA

SA La

ngley

Rese

arch C

enter

and J

. BRA

NDON

, NAS

A-Lan

gley R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-2

704

A Ne

w Fo

rmula

tion

of th

e Filte

r-Er

ror M

ethod

for A

erod

ynam

ic Pa

rame

ter Es

timat

ion in

Turb

ulenc

eJ.

Grau

er, E.

More

lli, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

1430

hrs

AIAA-2

015-2

705

Unste

ady a

nd P

ost-S

tall M

odel

Iden

tifica

tion

Using

Dyn

amic

Stall

Mane

uver

sJ.

Dias,

Braz

ilian A

ir Forc

e, Sã

o Jos

é dos

Ca

mpos

, Braz

il

1500

hrs

AIAA-2

015-2

706

Mode

ling a

nd Si

mulat

ion of

a Qu

adro

tor u

sing C

urve

Fitti

ng

Meth

odD.

Kaya

, A. K

utay,

Midd

le Ea

st Te

chnic

al Un

iversi

ty, An

kara,

Turke

y

1530

hrs

AIAA-2

015-2

707

Nonli

near

Aero

dyna

mic M

odeli

ng

from

Fligh

t Data

at H

igh An

gles o

f Att

ack U

sing N

eura

l-Gau

ss-Ne

wton

Me

thod

R. Ku

mar, P

EC Un

iversit

y of T

echno

logy,

Chan

digarh

, India

; A. G

hosh,

India

n Inst

itute

of Tec

hnolo

gy Ka

npur,

Kanp

ur, In

dia

Tues

day,

23 Ju

ne 2

015

119-

AFM-

8La

unch

Vehic

les, M

issile

s, an

d Pro

jectile

Fligh

t Mec

hanic

sPlu

m Bl

osso

m B

Chair

ed by

: T. L

AVIN

, San

dia N

ation

al La

borat

ories

and F

. FRE

SCON

I, US

Army

Rese

arch L

ab14

00 hr

sAIA

A-201

5-270

8De

liver

y of M

odula

r Leth

ality

via a

Pa

rent

-Chil

d Con

cept

F. Fre

sconi,

M. F

ermen

-Coke

r, Arm

y Re

searc

h Lab

orator

y, Ab

erdee

n Prov

ing

Grou

nd, M

D

1430

hrs

AIAA-2

015-2

709

An A

dapt

ive Pa

rame

ter Co

oper

ative

Gu

idanc

e Law

for M

ultipl

e fligh

t ve

hicles

Z. En

jiao,

T. Ch

ao, S

. Wan

g, M.

Yang

, Ha

rbin I

nstitu

te of

Tech

nolog

y, Ha

rbin,

China

1500

hrs

AIAA-2

015-2

710

Fligh

t Dyn

amics

Num

erica

l Co

mputa

tion o

f a So

undin

g Roc

ket

Includ

ing El

astic

Defo

rmati

on M

odel

E. Oli

veira

, Aero

nauti

cs an

d Spa

ce Ins

titute

(IAE),

São J

osé do

s Cam

pos,

Brazil;

P.

Gasba

rri, Un

iversit

y of R

ome “

La Sa

pienz

a”,

Rome

, Italy

; I. M

ilagre

da Fo

nseca,

Tec

hnolo

gical

Institu

te of

Aeron

autics

(ITA)

, Sã

o José

dos C

ampo

s, Bra

zil

1530

hrs

AIAA-2

015-2

711

Aero

ther

moela

stic R

educ

ed-O

rder

Mo

del o

f a H

yper

sonic

Vehic

leR.

Klock

, C. C

esnik

, Univ

ersity

of M

ichiga

n, An

n Arbo

r, Ann

Arbo

r, MI

1600

hrs

AIAA-2

015-2

712

Demo

nstra

tion

of La

unch

Vehic

le Slo

sh In

stabil

ity on

a Po

le-Ca

rt Pla

tform

J. Pe

i, P. R

othha

ar, N

ASA L

angle

y Res

earch

Ce

nter, H

ampto

n, VA

71

Tues

day,

23 Ju

ne 2

015

120-

AMT-7

/GT-7

Desig

n of

Expe

rimen

tOb

elisk

BCh

aired

by: G

. GAR

RARD

, Aero

spac

e Tes

ting A

llianc

e (AT

A) an

d D. Y

ODER

1400

hrs

AIAA-2

015-2

713

Case

Stud

ies fo

r the

Stat

istica

l De

sign

of Ex

perim

ents

Appli

ed to

Po

were

d Rot

or W

ind Tu

nnel

Tests

A. Ov

ermey

er, P.

Mart

in, P.

Tann

er, S

. Co

mmo,

NASA

Lang

ley Re

searc

h Cen

ter,

Hamp

ton, V

A

1430

hrs

Oral

Prese

ntatio

nCo

mpar

ison

betw

een

DOE a

nd

Tradit

ional

1-Fa

ctor a

t a Ti

me

Calib

ratio

n of

a Tra

nson

ic Wi

nd

Tunn

elG.

Garr

ard, M

. Mills

, Arno

ld En

ginee

ring

Deve

lopme

nt Co

mplex

, Tull

ahom

a, TN

Tues

day,

23 Ju

ne 2

015

121-

AMT-8

/FD-

14/T

P-6/

GT-8

Molec

ular-B

ased

Opt

ical D

iagno

stics

for H

yper

sonic

Non

equil

ibrium

Flow

sTo

paz

Chair

ed by

: P. D

ANEH

Y, NA

SA La

ngley

Rese

arch C

enter

and M

. WIN

TER,

Unive

rsity

of Ke

ntuck

y14

00 hr

sOr

al Pre

senta

tion

Intro

ducti

on an

d App

licat

ion

Cons

idera

tions

for O

ptica

l Di

agno

stics

in Hy

perso

nic

None

quilib

rium

Flows

P. Da

nehy

, NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

1430

hrs

Oral

Prese

ntatio

nIn

trodu

ction

to Em

ission

Sp

ectro

scopy

for H

yper

sonic

No

nequ

ilibriu

m Flo

wsM.

Wint

er, U

nivers

ity of

Kentu

cky,

Lexin

gton,

Lexin

gton,

KY

1500

hrs

Oral

Prese

ntatio

nIn

trodu

ction

to A

bsor

ption

Sp

ectro

scopy

for H

yper

sonic

No

nequ

ilibriu

m Flo

wsS.

O’B

yrne,

Unive

rsity

of Ne

w So

uth

Wales

, Can

berra

, Aus

tralia

1530

hrs

Oral

Prese

ntatio

nIn

trodu

ction

to M

olecu

lar Ta

gging

Ve

locim

etry f

or H

yper

sonic

No

nequ

ilibriu

m Flo

wsB.

Bath

el, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1600

hrs

Oral

Prese

ntatio

nIn

trodu

ction

to La

ser I

nduc

ed

Fluor

esce

nce S

pectr

osco

py fo

r Hy

perso

nic N

oneq

uilibr

ium Fl

ows

C. Jo

hans

en, U

nivers

ity of

Calga

ry,

Calga

ry, Ca

nada

1630

hrs

Oral

Prese

ntatio

nIn

trodu

ction

to R

aman

Ray

leigh

Sp

ectro

scopy

for H

yper

sonic

No

nequ

ilibriu

m Flo

wsP.

Dane

hy, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1700

hrs

Oral

Prese

ntatio

nIn

trodu

ction

to CA

RS Sp

ectro

scopy

fo

r Hyp

erso

nic N

oneq

uilibr

ium

Flows

A. Cu

tler, G

eorge

Was

hingto

n Univ

ersity

, Wa

shing

ton, D

C

Tues

day,

23 Ju

ne 2

015

122-

APA-

13Ap

plied

CFD

& Nu

meric

al Co

rrelat

ions w

ith Ex

perim

enta

l Dat

a II

Stemm

ons B

Chair

ed by

: N. H

ARIH

ARAN

, CRE

ATE-A

V an

d C. S

HENG

, Univ

ersity

of To

ledo

1400

hrs

AIAA-2

015-2

714

CFD

Analy

sis of

Coun

ter-R

otat

ing

Open

Rot

ors U

sing a

Rot

ating

Ac

tuat

or D

isk M

odel

M. M

alick

, R. A

garw

al, W

ashin

gton

Unive

rsity

in St

. Lou

is, S

t. Lo

uis, M

O

1430

hrs

AIAA-2

015-2

715

Nume

rical

Simula

tion

of

Comp

ressi

ble Fl

ow in

a Di

ffusin

g S-

duct

with

and w

ithou

t Vor

tex

Gene

rato

rsS.

Kama

li, B.

Reza

Ahrab

i, R. W

ebste

r, K.

Sree

nivas

, Univ

ersity

of Te

nnes

see,

Chatt

anoo

ga, C

hatta

noog

a, TN

1500

hrs

AIAA-2

015-2

716

Massi

vely

separ

ated t

urbu

lent fl

ow

simula

tion a

roun

d non

-rotat

ing

MEXI

CO bl

ade b

y mea

ns of

RANS

and

DDES

appr

oach

es in

Open

FOAM

Y. Zh

ang,

A. va

n Zuijl

en, G

. van

Busse

l, De

lft Un

iversit

y of T

echno

logy,

Delft,

The

Nethe

rland

s

1530

hrs

AIAA-2

015-2

717

Wind

Tunn

el Wa

ll Int

erfe

renc

e Ef

fects

on an

Osci

llatin

g Aer

ofoil

in

the S

tall R

egim

eJ.

Chen

g, M.

Lowe

nberg

, Univ

ersity

of

Brist

ol, B

ristol

, Unit

ed Ki

ngdo

m; X

. Wan

g, J.

Yu, N

anjin

g Univ

ersity

of S

cienc

e and

Te

chno

logy,

Nanji

ng, C

hina

Tues

day,

23 Ju

ne 2

015

123-

APA-

14Sp

ecial

Sessi

on: H

istor

ically

Sign

ifica

nt/I

nflue

ntial

Pap

ers i

n Ap

plied

Aer

odyn

amics

Carp

enter

Ball

room

Chair

ed by

: B. M

CGRA

TH, J

HU/A

pplie

d Phy

sics L

abora

tory a

nd J.

PINI

ER, N

ASA L

angle

y Res

earch

Cente

r14

00 hr

sOr

al Pre

senta

tion

Thou

ghts

on w

orkin

g with

AMO

Smith

(Inv

ited)

R. Lie

beck

, The

Boe

ing Co

mpan

y, Hu

nting

ton B

each

, CA

1500

hrs

Oral

Prese

ntatio

nTh

e Spa

lart-A

llmar

as Tu

rbule

nce M

odel

Pape

r of 1

992

(Invit

ed)

P. Sp

alart,

The B

oeing

Comp

any,

Seatt

le, W

A; S.

Allm

aras,

Massa

chus

etts I

nstitu

te of

Tech

nolog

y, Ca

mbrid

ge, M

A

1600

hrs

AIAA-2

015-2

718

Origi

ns an

d Fur

ther

Dev

elopm

ent o

f the

Jame

son-

Schm

idt-Tu

rkel

Sche

me (I

nvite

d)A.

Jame

son,

Stan

ford U

nivers

ity, S

tanfor

d, CA

72

Tues

day,

23 Ju

ne 2

015

124-

APA-

15Sp

ecial

Sessi

on: A

erod

ynam

ic-Str

uctu

ral M

odeli

ng, O

ptim

izatio

n, an

d Tes

t Tec

hniqu

es fo

r Flex

ible W

ing Te

chno

logy I

ISte

mmon

s ACh

aired

by: W

. SILV

A, NA

SA-La

ngley

Rese

arch C

enter

and B

. STA

NFOR

D, N

ASA L

angle

y Res

earch

Cente

r14

00 hr

sAIA

A-201

5-271

9On

going

Fixe

d Wing

Res

earch

wi

thin

the N

ASA

Lang

ley

Aero

elasti

city B

ranc

hR.

Barte

ls, P.

Chwa

lowsk

i, C. F

unk,

J. He

eg, J

. Hur,

M. S

anetr

ik, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

; et a

l.

1430

hrs

AIAA-2

015-2

720

Analy

sis of

Limi

t Cyc

le Os

cillat

ion

Data

from

the A

eroe

lastic

Test

of th

e SUG

AR Tr

uss-B

race

d Wing

Mo

del

R. Ba

rtels,

R. S

cott,

NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA

1500

hrs

AIAA-2

015-2

721

Comp

utat

ional

Aero

elasti

c Ana

lyses

of

a Lo

w-Bo

om Su

perso

nic

Confi

gura

tion

W. Si

lva, M

. San

etrik,

P. Ch

walow

ski, N

ASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA

1530

hrs

AIAA-2

015-2

722

Unste

ady A

eros

ervo

elasti

c Mo

delin

g of F

lexibl

e Wing

Gen

eric

Trans

port

Aircr

aft w

ith Va

riable

Ca

mber

Cont

inuou

s Tra

iling E

dge

Flap

E. Ta

l, Delf

t Univ

ersity

of Te

chno

logy,

Delft,

Th

e Neth

erlan

ds; N

. Ngu

yen,

NASA

Ames

Re

searc

h Cen

ter, M

offett

Field

, CA

1600

hrs

AIAA-2

015-2

723

Optim

izatio

n fo

r Loa

d Alle

viatio

n of

Trus

s-Bra

ced W

ing A

ircra

ft Wi

th Va

riable

Camb

er Co

ntinu

ous

Trailin

g Edg

e Flap

S. Le

bofsk

y, E.

Ting,

K. Tri

nh, S

tinge

r Gh

affari

an Te

chno

logies

, Inc

., Mo

untai

n Vie

w, CA

; N. N

guye

n, NA

SA Am

es

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1630

hrs

AIAA-2

015-2

724

Meas

urem

ent a

nd M

odeli

ng of

Ae

roela

stic R

espo

nse u

nder

Gus

tY.

Babb

ar, V.

Sury

akum

ar, T.

Strg

anac

, Te

xas A

&M U

nivers

ity, C

olleg

e Stat

ion, T

X;

A. Ma

ngala

m, Ta

o of S

ystem

s Inte

gratio

n, Inc

., Ha

mpton

, VA

Tues

day,

23 Ju

ne 2

015

125-

APA-

16Flo

w Co

ntro

l App

licat

ions &

Dem

onstr

ation

s (Ac

tive &

Pas

sive)

IISte

mmon

s CCh

aired

by: M

. OL,

US Ai

r Forc

e Res

each

Labo

ratory

and G

. ZHA

, Univ

ersity

of M

iami

1400

hrs

AIAA-2

015-2

725

Simula

tion

and S

urro

gate-

Base

d De

sign

of R

ecta

ngula

r Vor

tex

Gene

rato

rs fo

r Tiltr

otor

Airc

raft

Wing

sR.

Beva

n, D.

Poole

, C. A

llen,

T. Re

ndall

, Un

iversi

ty of

Brist

ol, B

ristol

, Unit

ed

Kingd

om

1430

hrs

AIAA-2

015-2

726

Multip

oint D

esign

of Vo

rtex

Gene

rato

rs on

a Sw

ept I

nfinit

e-Wi

ng u

nder

Cruis

e and

Critic

al Co

nditio

nN.

Nam

ura, K

. Shim

oyam

a, S.

Oba

yash

i, To

hoku

Univ

ersity

, Sen

dai, J

apan

1500

hrs

AIAA-2

015-2

727

Flow

Cont

rol in

a Ma

ch 4

.0 In

let

by Sl

otted

Wed

ge-sh

aped

Vorte

x Ge

nera

tors

D. Va

rma,

S. S

aurav

, S. G

hosh

, Ind

ian

Institu

te of

Tech

nolog

y Mad

ras, C

henn

ai,

India

1530

hrs

AIAA-2

015-2

728

Wind

Tunn

el Ex

perim

ents

with

Activ

e Flo

w Co

ntrol

for an

Oute

r Wing

Mod

elV.

Cioba

ca, J.

Wild,

Germ

an Ae

rospa

ce Ce

nter

(DLR

), Bra

unsch

weig,

Germ

any;

M. Ba

uer, T

. Gru

nd, T

echnic

al Un

iversit

y of B

erlin,

Berlin

, Ge

rman

y; C.

Hueh

ne, P.

Scho

lz, Te

chnica

l Un

iversit

y of B

raunsc

hweig

, Brau

nschw

eig,

Germ

any;

et al.

1600

hrs

AIAA-2

015-2

729

Passi

ve Fl

ow Co

ntro

l App

lied t

o a

NACA

2301

2 Ai

rfoil I

n A

Subs

onic

Flow

N. Fi

ndan

is, U

nivers

ity of

New

Sou

th Wa

les, S

ydne

y, Au

strali

a

1630

hrs

AIAA-2

015-2

730

Comp

utat

ions o

f Acti

ve O

pen-

Loop

Flo

w Co

ntro

l on

a Flut

tering

Wing

J. Se

idel, C

. Fag

ley, T

. McLa

ughli

n, U.

S.

Air Fo

rce Ac

adem

y, Co

lorad

o Spri

ngs,

CO

Tues

day,

23 Ju

ne 2

015

126-

ATIO

-12

ATM

II - A

ir Tra

ffic A

nalys

isMi

lanCh

aired

by: A

. RAO

, Purd

ue U

nivers

ity14

00 hr

sAIA

A-201

5-273

1A

Wave

let A

nalys

is Ap

proa

ch fo

r Ca

tegor

izing

Air

Traffi

c Beh

avior

M. D

rew, U

nivers

ity of

Califo

rnia,

Santa

Cru

z, Mo

ffett

Field,

CA; K

. She

th, N

ASA

Ames

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1430

hrs

AIAA-2

015-2

732

Appli

catio

n of

Dat

a Mini

ng in

Air

Traffi

c For

ecas

ting

J. Bu

sque

ts, Ci

ty Un

iversi

ty Lo

ndon

, Lo

ndon

, Unit

ed Ki

ngdo

m; A.

Evan

s, Un

iversi

ty Co

llege

Lond

on, L

ondo

n, Un

ited K

ingdo

m; E.

Alon

so, C

ity U

nivers

ity

Lond

on, L

ondo

n, Un

ited K

ingdo

m

1500

hrs

AIAA-2

015-2

733

Iden

tifica

tion

of A

ircra

ft Co

nflict

Re

solut

ionTy

pes f

rom

Reco

rded

Fli

ght D

ata

S. S

hin, K

. Kim

, I. H

wang

, Purd

ue

Unive

rsity,

Wes

t Lafa

yette

, IN

Tues

day,

23 Ju

ne 2

015

127-

ATIO

-13

Trans

form

ation

al Fli

ght -

Adv

ance

d Con

cept

sMe

tropo

litan

Ballr

oom

Chair

ed by

: N. B

ORER

, NAS

A Lan

gley R

esea

rch Ce

nter

1400

hrs

Oral

Prese

ntatio

nNA

SA G

L-10

Tilt-W

ing Ti

lt-Ta

il Co

ncep

tW.

Fred

erick

s, NA

SA La

ngley

Rese

arch

Cente

r, Ham

pton,

VA

1430

hrs

Oral

Prese

ntatio

nLE

APTe

ch D

istrib

uted

Elec

tric

Prop

ulsion

Integ

ratio

n Co

ncep

tM.

Moo

re, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1500

hrs

Oral

Prese

ntatio

nCo

mpar

ison o

f Com

putat

ional

Aero

dyna

mics

Tools

for P

redict

ing

Low-

Spee

d Perf

orma

nce o

f a

Distr

ibuted

Prop

eller

Conc

ept

M. Pa

tterso

n, N.

Borer

, NAS

A Lan

gley

Resea

rch Ce

nter, H

ampto

n, VA

; B. G

erman

, Ge

orgia

Institu

te of

Techn

ology,

Atlan

ta, GA

1530

hrs

Oral

Prese

ntatio

nTh

e Sam

son

Switc

hblad

e Mult

i-Mo

de A

ircra

ft Co

ncep

tS.

Bou

sfield

, Sam

son A

ircraf

t, Au

burn,

CA

1600

hrs

Oral

Prese

ntatio

nHo

verle

ss VT

OL H

yper

Comm

uter

Mi

ssion

Conc

ept

M. M

oore,

NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

1630

hrs

AIAA-2

015-2

734

Pred

icting

the A

ero L

oads

Beh

ind a

Prop

eller

in th

e Pre

senc

e of a

Wing

Us

ing Fl

ightst

ream

V. Ah

uja, R

. Hart

field,

Fligh

tstrea

m,

Aubu

rn, AL

1700

hrs

AIAA-2

015-2

735

Cent

rifug

ally S

tiffe

ned R

otor

: A

Comp

lete D

eriva

tion

of th

e Plan

t Mo

del w

ith N

onlin

ear D

ynam

icsJ.

Selfri

dge,

G. Ta

o, Un

iversi

ty of

Virgin

ia,

Charl

ottes

ville,

Charl

ottes

ville,

VA

73

Tues

day,

23 Ju

ne 2

015

128-

ATIO

-14

Prod

uct D

esign

and S

uppo

rtMa

nche

ster

Chair

ed by

: A. C

HAPU

T, Un

iversi

ty of

Texa

s at A

ustin

1400

hrs

AIAA-2

015-2

736

Value

Driv

en Co

ncep

tual

Desig

n of

Un

mann

ed A

ir Sy

stem

for D

efen

se

Appli

catio

nsE.

Papa

georg

io, M

. Eres

, J. S

canla

n, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom

1430

hrs

AIAA-2

015-2

737

Mont

e Car

lo ba

sed R

obus

t MDO

ap

plied

to A

ircra

ft Co

ncep

tual

Desig

n: a

techn

ical-fi

nanc

ial

coup

ling o

ptim

izatio

n str

ateg

yD.

Bian

chi, T

. Orra

, Emb

raer, S

ão Jo

sé do

s Ca

mpos

, Braz

il; P.

Pagli

one,

Tech

nolog

ical

Institu

te of

Aeron

autic

s (ITA

), Sã

o Jos

é do

s Cam

pos,

Braz

il

1500

hrs

AIAA-2

015-2

738

Deve

lopme

nt an

d App

licat

ion of

a Pa

rame

tric D

esign

Tool

for D

esign

Ite

ratio

ns of

Larg

e Tur

bopr

op

Aircr

aft

M. Kü

gler, N

. Ran

dt, Te

chnic

al Un

iversi

ty of

Munic

h, Mu

nich,

Germ

any

1530

hrs

AIAA-2

015-2

739

3D P

rinted

Par

ts fo

r Quic

k Tu

rnar

ound

Airc

raft

Proje

cts an

d Le

gacy

Issu

esU.

Rehm

anjan

, Qan

tas Ai

rway

s, Ltd

., Sy

dney

, Aus

tralia

1600

hrs

AIAA-2

015-2

740

UGV a

nd U

AV Co

oper

ation

for

Cons

tructi

ng P

roba

bilist

ic Th

reat

Ex

posu

re M

ap (P

TEM)

O. D

askir

an, H

. Sev

il, A.

Doga

n, B.

Huff

, Un

iversi

ty of

Texa

s, Arl

ington

, Arlin

gton,

TX 16

30 hr

sAIA

A-201

5-274

1To

ward

Effic

ient M

odel-

Base

d De

velop

ment

of A

eros

pace

Ap

plica

tions

I. Am

unds

on, L

. Ship

ton, A

. Liu,

M.

Nowa

k, Ea

ton Co

rporat

ion, C

levela

nd, O

H

1700

hrs

AIAA-2

015-2

742

Relia

bility

Ana

lysis

of th

e In

tegra

ted M

odula

r Avio

nics

Syste

m Us

ing A

ADL a

nd G

SPN

P. Wa

ng, F.

Yan,

R. Liu

, C. Z

hao,

Z. Ma

, Civil

Av

iation

Unive

rsity o

f Chin

a, Tia

njin, C

hina

Tues

day,

23 Ju

ne 2

015

129-

CASE

-5

1400

- 17

30 h

rsCA

SE Se

ssion

I &

IISte

uben

1400

-1530

hrs

Conc

ept D

evelo

pmen

t of C

omple

x Sys

tems

This

pane

l add

resse

s the

phas

e of d

evelo

pmen

t tha

t inclu

des a

ctivit

ies fr

om th

e beg

inning

of de

cision

activ

ities f

or bu

ilding

new

syste

ms to

the t

ransit

ion to

the p

roduc

t des

ign at

mile

stone

“B” (

DoD)

or th

e end

of Ph

ase B

for N

ASA.

Sessi

on Ch

airs:

Stev

en D

’Urso

, Prog

ram Co

ordina

tor an

d Lec

turer,

Aeros

pace

Sys

tems E

ngine

ering

, Univ

ersity

of Ill

inois

at Ur

bana

-Cham

paign

and M

at Fre

nch,

Electr

ical S

ystem

s Eng

ineer,

Rolls-

Royc

e Corp

oratio

n

Pan

elists

:Ri

ck M

ange

F-35

PNR P

rogram

Man

ager

Lock

heed

Mart

in Ae

ronau

tics

Robe

rt (R

ob) S

imon

sT e

chnic

al Fe

llow

The B

oeing

Comp

any

Jaso

n Me

rret

Tech

nical

Spec

ialist

, Gulf

strea

m Ae

rospa

ce Pe

rform

ance

Engin

eerin

gGu

lfstre

am Ae

rospa

ce Co

rporat

ion

1545

-1730

hrs

Produ

ct De

sign f

or Co

mplex

Sys

tems A

cross

the S

upply

Chain

This

sessi

on w

ill foc

us on

the c

halle

nges

and e

nabli

ng te

chno

logies

for p

roduc

t des

ign ac

ross a

supp

ly ch

ain. I

n part

icular

, the

sessi

on w

ill ad

dress

the la

yered

chain

cons

isting

of O

EM/a

irfram

er, Ti

er 1,

Tier

2, an

d the

appro

ache

s for

desig

ning c

omple

x sys

tems t

hat h

andle

the

integ

ration

aspe

cts. M

ethod

s and

mod

el-ba

sed t

ool a

pproa

ches

will

be di

scusse

d in t

erms o

f exis

ting c

apab

ilities

, gap

s, an

d futu

re tre

nds.

Sessi

on Ch

airs:

Eelco

Sch

olte,

Mana

ger, A

dvan

ced M

ethod

s - El

ectric

Sys

tems,

UTC A

erosp

ace S

ystem

s and

Carm

en S

choo

ley, M

anag

er, S

ystem

s Eng

ineeri

ng an

d Inte

gratio

n, Gu

lfstre

am Ae

rospa

ce Co

rporat

ion

Pan

elists

:Fe

rnan

do D

ones

Tech

nical

Fello

wTh

e Boe

ing Co

mpan

y

Bern

ard D

ionCT

OAN

SYS

Bren

da N

uhfe

rPro

gram

Mana

ger

UTC/

Pratt

& W

hitne

y

Tues

day,

23 Ju

ne 2

015

130-

CFD-

13Flu

x Re

cons

tructi

on M

ethod

sGr

and B

allro

om A

Chair

ed by

: Z. W

ANG,

Univ

ersity

of Ka

nsas

and B

. VER

MEIRE

, McG

ill Un

iversi

ty14

00 hr

sAIA

A-201

5-274

3On

the U

tility

of H

igh-O

rder

Me

thod

s for

Uns

tructu

red G

rids:

A Co

mpar

ison

Betw

een

PyFR

and

Indu

stry S

tand

ard T

ools

B. Ve

rmeir

e, F.

With

erden

, P. V

incen

t, Im

peria

l Coll

ege L

ondo

n, Lo

ndon

, Unit

ed

Kingd

om

1430

hrs

AIAA-2

015-2

744

De-A

liasin

g thr

ough

Ove

r-In

tegra

tion

Appli

ed to

the F

lux

Reco

nstru

ction

and D

iscon

tinuo

us

Galer

kin M

ethod

sS.

Spie

gel, H

. Huy

nh, J

. DeB

onis,

NAS

A Gle

nn Re

searc

h Cen

ter, C

levela

nd, O

H

1500

hrs

AIAA-2

015-2

745

Fully

-cons

erva

tive H

igh-o

rder

FR

Sche

me on

Mov

ing an

d Def

ormi

ng

Grids

Y. Ab

e, Un

iversi

ty of

Toky

o, Sa

gami

hara,

Ja

pan;

T. Ha

ga, T

. Non

omura

, K. F

ujii,

Japa

n Aero

spac

e Exp

lorati

on Ag

ency

(JA

XA),

Saga

miha

ra, Ja

pan

1530

hrs

AIAA-2

015-2

746

A WE

NO-ty

pe Li

miter

for 4

th

Orde

r Con

strain

ed D

eriva

tive F

lux

Reco

nstru

ction

Meth

odZ.

Sun,

F. Xia

o, To

kyo I

nstitu

te of

Tech

nolog

y, Yo

koha

ma, J

apan

74

Tues

day,

23 Ju

ne 2

015

131-

CFD-

14Ad

joint

s and

Erro

r Esti

matio

nGr

and B

allro

om B

Chair

ed by

: C. R

OY, V

irgini

a Tec

h and

C. O

LLIVIE

R GOO

CH, U

nivers

ity of

Briti

sh Co

lumbia

1400

hrs

AIAA-2

015-2

747

Accu

racy

of D

iscre

tizat

ion Er

ror

Estim

ation

by th

e Erro

r Tra

nspo

rt Eq

uatio

n on

Uns

tructu

red M

eshe

s -

Nonli

near

Syste

ms of

Equa

tions

G. Ya

n, C.

Olliv

ier G

ooch

, Univ

ersity

of

Britis

h Colu

mbia,

Vanc

ouve

r, Can

ada

1430

hrs

AIAA-2

015-2

748

Comp

ariso

n of T

runc

ation

Erro

r Est

imato

rs for

Defe

ct Co

rrecti

on

and O

utput

Error

Estim

ation

in th

e Un

struc

tured

Mesh

Finit

e Volu

me

Metho

dM.

Sharb

atdar,

C. O

llivier

Gooch

, Univ

ersity

of

British

Colum

bia, V

ancou

ver, C

anad

a

1500

hrs

AIAA-2

015-2

749

Stabil

isatio

n of

Disc

rete

Adjoi

nt

Solve

rs fo

r Inc

ompr

essib

le Flo

wY.

Wang

, S. A

kbarz

adeh

, J. M

uelle

r, Qu

een M

ary U

nivers

ity of

Lond

on, L

ondo

n, Un

ited K

ingdo

m

1530

hrs

AIAA-2

015-2

750

Fixed

point

discr

ete ad

joint

of

SIMPL

E-like

solve

rsS.

Akba

rzade

h, Y.

Wang

, J. M

uelle

r, Qu

een M

ary U

nivers

ity of

Lond

on, L

ondo

n, Un

ited K

ingdo

m

1600

hrs

AIAA-2

015-2

751

Conv

erge

nce A

cceler

ation

Usin

g Co

nver

genc

e Erro

r Esti

matio

nS.

Eyi, M

iddle

East

Tech

nical

Unive

rsity,

An

kara,

Turke

y

Tues

day,

23 Ju

ne 2

015

132-

CFD-

15Tim

e Int

egra

tion

Meth

ods

Cora

lCh

aired

by: X

. WAN

G, Ai

r Forc

e Res

earch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

and J

. NOR

DSTR

OM, L

inköp

ing U

nivers

ity14

00 hr

sAIA

A-201

5-275

2Op

timal

Rung

e-Ku

tta Sc

heme

s for

Hi

gh-o

rder

Spat

ial an

d Tem

pora

l Di

screti

zatio

nsN.

Mun

dis, E

RC, I

nc.,

Edwa

rds AF

B, CA

; A.

Edoh

, Univ

ersity

of Ca

liforni

a, Lo

s Ang

eles,

Los A

ngele

s, CA

; V. S

anka

ran, A

ir Forc

e Re

searc

h Lab

orator

y, Ed

wards

AFB,

CA

1430

hrs

AIAA-2

015-2

753

Appli

catio

n of

Dua

l Tim

e Step

ping

to Fu

lly Im

plicit

Run

ge K

utta

Sc

heme

s for

Uns

teady

Flow

Ca

lculat

ions

A. Ja

meso

n, St

anfor

d Univ

ersity

, Stan

ford,

CA

1500

hrs

AIAA-2

015-2

754

Asse

ssmen

t of t

ime i

mplic

it dis

cretiz

ation

s for

the c

ompu

tatio

n of

turb

ulent

comp

ressi

ble fl

ows

P. Cin

nella

, Univ

ersità

del S

alento

, Le

cce, I

taly;

C. Ce

dric,

Paris

Insti

tute o

f Te

chno

logy,

Paris

, Fran

ce

1530

hrs

AIAA-2

015-2

755

A Ma

pped

Cheb

yshe

v Ps

eudo

spec

tral M

ethod

for

Unste

ady F

low A

nalys

isD.

Im, S

. Cho

i, J. M

cClur

e, J.

Choi,

F.

Skies

, Virg

inia P

olytec

hnic

Institu

te an

d St

ate U

nivers

ity, B

lacks

burg,

VA

1600

hrs

AIAA-2

015-2

756

Unste

ady S

olutio

ns of

Non

-Line

ar

Diffe

rent

ial Eq

uatio

ns U

sing W

alsh

Func

tion

Serie

sP.

Gnoff

o, NA

SA La

ngley

Rese

arch C

enter

, Ha

mpton

, VA

1630

hrs

AIAA-2

015-2

757

Inve

stiga

tion

of Ef

ficien

t High

-Or

der I

mplic

it Ru

nge-

Kutta

Me

thod

s Bas

ed on

Gen

erali

zed

Summ

ation

-by-

Parts

Ope

rato

rsP.

Boom

, D. Z

ingg,

Unive

rsity

of To

ronto,

To

ronto,

Cana

da

Tues

day,

23 Ju

ne 2

015

133-

CFD-

16RA

NS M

odeli

ngEm

erald

Chair

ed by

: P. H

ARTW

ICH, B

oeing

Rese

arch &

Tech

nolog

y and

J. CA

RLSO

N, Co

mputa

tiona

l Aero

scien

ces B

ranch

1400

hrs

AIAA-2

015-2

758

Node

-Cen

tered

Wall

Func

tion

Mode

ls fo

r the

Uns

tructu

red F

Low

Code

Fun3

DJ.

Carls

on, V

. Vats

a, J.

Whit

e, NA

SA

Lang

ley Re

searc

h Cen

ter, H

ampto

n, VA

1430

hrs

AIAA-2

015-2

759

Analy

sis of

a low

Rey

nolds

dif

fere

ntial

Rey

nolds

stre

ss mo

del

in ho

moge

neou

s she

ar fl

ow w

ith

resp

ect t

o num

erica

l sta

bility

C. Mo

rsbac

h, Ge

rman

Aeros

pace

Cente

r (D

LR),

Colog

ne, G

erman

y

1500

hrs

AIAA-2

015-2

760

Exten

sion o

f the

SU2 o

pen s

ource

CFD

code

to th

e sim

ulatio

n of t

urbu

lent

flows

of fu

ids m

odell

ed w

ith co

mplex

the

rmop

hysic

al law

sS.

Vitale

, Delf

t Univ

ersity

of Te

chnolo

gy, De

lft,

The N

etherl

ands;

G. Go

ri, Tec

hnica

l Univ

ersity

of

Milan

, Milan

, Italy

; M. P

ini, De

lft Un

iversit

y of

Techn

ology,

Delft,

The N

etherl

ands;

A.

Guard

one,

Techn

ical U

nivers

ity of

Milan

, Milan

, Ita

ly; T.

Econ

omon

, F. Pa

lacios

, Stan

ford

Unive

rsity,

Palo

Alto,

CA; e

t al.

1530

hrs

AIAA-2

015-2

761

Turb

ulent

Flow

Simu

lation

s on

Uns

tructu

red G

rids u

sing a

Re

ynold

s Stre

ss Mo

dels

Y. Mo

r-Yos

sef,

Israe

li CFD

Cente

r, Cae

sarea

Ind

ustria

l Park

, Isra

el

1600

hrs

AIAA-2

015-2

762

Rece

nt Im

prov

emen

t of a

Co

rrelat

ion-B

ased

Tran

sition

Tu

rbule

nce M

odel

for S

imula

ting

Thre

e-Di

mens

ional

Boun

dary

La

yers

J. Ch

oi, O

. Kwo

n, Ko

rea Ad

vanc

ed In

stitut

e of

Scien

ce an

d Tec

hnolo

gy, D

aejeo

n, So

uth Ko

rea

1630

hrs

AIAA-2

015-2

763

Prop

er or

thog

onal

deco

mpos

ition

closu

re m

odels

for B

urge

rs an

d Na

vier-S

toke

s Equ

ation

sH.

Imtia

z, I.

Akhta

r, M. S

aif U

llah K

halid

, Na

tiona

l Univ

ersity

of S

cienc

es an

d Te

chno

logy,

Rawa

lpind

i, Pak

istan

Tues

day,

23 Ju

ne 2

015

134-

CFD-

37

1400

- 16

00 h

rsCF

D Flo

w Vis

ualiz

ation

Show

case

Chan

tilly B

allro

om Fo

yer

The C

FD Fl

ow V

isuali

zatio

n Sho

wcas

e will

be he

ld in

the fo

yer a

rea ou

tside

the E

xpos

ition H

all. A

uthors

of pa

pers

conta

ining

CFD

visua

lizati

ons w

ill de

scribe

their

work

and t

he si

gnific

ance

of th

eir an

imati

on as

it pla

ys on

a lar

ge-sc

reen m

onito

r. Mult

iple v

isuali

zatio

ns w

ill be

sh

own d

uring

each

of th

e fou

r 30-m

inute

time s

lots d

uring

the e

vent.

At th

e con

clusio

n of t

he ev

ent,

award

s will

be pr

esen

ted fo

r, Mos

t Artis

tic Fl

ow V

isuali

zatio

n Anim

ation

, Mos

t Qua

ntitat

ively

Descr

iptive

Flow

Visu

aliza

tion A

nimati

on, M

ost C

ompre

hens

ive Fl

ow V

isuali

zatio

n An

imati

on. T

he vi

suali

zatio

ns of

the t

hree w

inners

will

be di

splay

ed on

a mo

nitor

in the

Expo

sition

Hall

durin

g the

rema

inder

of the

expo

sition

.

75

Tues

day,

23 Ju

ne 2

015

135-

F360

-4

1400

- 16

30 h

rsIn

terna

tiona

l UAS

Integ

ratio

n Fo

rum

Gran

d Ball

room

E

Mode

rator:

Rob H

ughe

s, No

rthrop

Grum

man,

Inc.

P

aneli

sts:

Cees

Bil

Asso

ciate

Profes

sor, S

choo

l of A

erosp

ace,

Mech

anica

l and

Man

ufactu

ring E

ngine

ering

RMIT

Unive

rsity

Chuc

k Jo

hnso

nVic

e Pres

ident

of Op

eratio

nsTh

e Pad

ina G

roup

Marty

Rog

ers

Unive

rsity

of Ala

ska-F

airba

nks

Marsh

all Ja

ckso

nPro

ject M

anag

er - A

viatio

n Safe

ty Au

dits

Offic

e of I

nspe

ctor G

enera

lU.

S. D

epart

ment

of Tra

nspo

rtatio

n

Rand

y Willi

sFA

A, Co

-Chair

of IC

AO RP

AS(R

emote

ly Pil

oted A

ircraf

t Sys

tems)

Dale

Rich

ards

Senio

r Res

earch

Fello

w, H

uman

Facto

rsFa

culty

of En

ginee

ring &

Comp

uting

Cove

ntry U

nivers

ity, U

nited

King

dom

Tues

day,

23 Ju

ne 2

015

136-

FD-1

5Un

stead

y Wing

Aer

odyn

amics

IIGo

veno

rs Le

cture

Hall

Chair

ed by

: K. T

AIRA,

Florid

a Stat

e Univ

ersity

and B

. JOL

LY, U

S Air

Force

1400

hrs

AIAA-2

015-2

764

Aero

mech

anics

of M

embr

ane W

ings

in Gr

ound

-Effe

ctR.

Bleisc

hwitz

, R. D

e Kat,

B.

Gana

pathi

subra

mani,

Univ

ersity

of

South

ampto

n, So

utham

pton,

Unite

d Kin

gdom

1430

hrs

AIAA-2

015-2

765

The I

nflue

nce o

f Stre

amlin

e Cu

rvat

ure o

n Lo

w As

pect

Ratio

Ro

tatin

g Wing

sC.

Kronin

ger, A

. Harr

ington

, M. M

unso

n, Arm

y Res

earch

Labo

ratory

, Abe

rdeen

Pro

ving G

round

, MD

1500

hrs

AIAA-2

015-2

766

Effe

ct of

Turb

ulenc

e Mod

eling

on

Hove

ring R

otor

Flow

sS.

Yoon

, N. C

hade

rjian,

T. Pu

lliam,

T.

Holst

, NAS

A Ame

s Res

earch

Cente

r, Mo

ffett

Field,

CA

1530

hrs

AIAA-2

015-2

767

A Data

-Driv

en M

odeli

ng Fr

amew

ork

for Pr

edict

ing Fo

rces a

nd Pr

essur

es on

a R

apidl

y Pitc

hing A

irfoil

S. Da

wson

, N. S

chiav

one,

C. Ro

wley,

Pri

nceton

Unive

rsity,

Prince

ton, N

J; D.

Wi

lliams

, Illino

is Inst

itute

of Tec

hnolo

gy,

Chica

go, IL

1600

hrs

AIAA-2

015-2

768

Nonli

near

Char

acter

izatio

n of F

low

over

Oscill

ating

Ellip

tic Ai

rfoils

M. Kh

alid, I.

Akhta

r, Nati

onal

Unive

rsity o

f Sc

iences

and T

echno

logy,

Islama

bad,

Pakis

tan;

H. Do

ng, U

nivers

ity of

Virgi

nia, C

harlo

ttesvi

lle,

Charl

ottesv

ille, V

A; N.

Ahsan

, Instit

ute of

Space

Tec

hnolo

gy, Is

lamab

ad, P

akista

n

1630

hrs

AIAA-2

015-2

769

Inter

mitte

ncy B

ehav

iour i

n th

e Flo

w Pa

st an

Osci

llatin

g Airf

oilS.

Bad

rinath

, S. S

arkar,

India

n Ins

titute

of Te

chno

logy M

adras

, Che

nnai,

India

1700

hrs

AIAA-2

015-2

770

Analy

sis of

Defl

ected

Vorte

x Str

eet

Prod

uced

by an

Osci

llatin

g Airf

oilS.

Bad

rinath

, S. S

arkar,

India

n Ins

titute

of Te

chno

logy M

adras

, Che

nnai,

India

Tues

day,

23 Ju

ne 2

015

137-

FD-1

6Bo

unda

ry La

yer T

rans

ition:

Cros

sflow

Sapp

hire

Chair

ed by

: M. B

ORG,

Air F

orce R

esea

rch La

borat

ory an

d T. J

ULIAN

O, U

nivers

ity of

Notr

e Dam

e14

00 hr

sAIA

A-201

5-277

1Di

rect

Nume

rical

Simula

tion

of Tr

ansit

ion du

e to T

rave

ling

Cros

sflow

Vorti

ces

F. Li,

M. C

houd

hari,

NASA

Lang

ley

Rese

arch C

enter

, Ham

pton,

VA; L

. Dua

n, Mi

ssouri

Univ

ersity

of S

cienc

e and

Te

chno

logy,

Rolla

, MO

1430

hrs

AIAA-2

015-2

772

EPIC:

NPS

E Ana

lysis

of H

yper

sonic

Cr

ossfl

ow In

stabil

ity on

Yawe

d Str

aight

Circu

lar Co

neN.

Oliv

iero,

T. Ko

cian,

A. Mo

yes,

H. Re

ed,

Texa

s A&M

Univ

ersity

, Coll

ege S

tation

, TX

1500

hrs

AIAA-2

015-2

773

Seco

ndar

y Ins

tabil

ity of

Stat

ionar

y Cr

ossfl

ow Vo

rtice

s on

an In

cline

d Co

ne at

Mac

h 6

C. Wa

rd, R.

Hen

derso

n, S.

Sch

neide

r, Pu

rdue U

nivers

ity, W

est L

afaye

tte, I

N

1530

hrs

AIAA-2

015-2

774

Expe

rimen

tal s

tudy

of cr

ossfl

ow

insta

bility

on a

Mach

6 ya

wed c

one

S. Cr

aig, W

. Sari

c, Te

xas A

&M U

nivers

ity,

Colle

ge S

tation

, TX

1600

hrs

AIAA-2

015-2

775

Comp

utat

ional

Inve

stiga

tion o

f Step

Ex

cresce

nce S

ensit

ivity

in a

Swep

t-Wi

ng B

ound

ary L

ayer

M. Tu

fts, H

. Ree

d, B.

Craw

ford,

G. D

unca

n, W.

Sari

c, Te

xas A

&M U

nivers

ity, C

olleg

e St

ation

, TX

1630

hrs

AIAA-2

015-2

776

The E

ffect

of Ba

ckwa

rd-fa

cing S

tep

Heigh

t on I

nstab

ility G

rowt

h and

Br

eakd

own i

n Swe

pt-Wi

ng Bo

unda

ry-

Laye

r Tra

nsitio

nJ.

Eppin

k, NA

SA La

ngley

Resea

rch Ce

nter,

Hamp

ton, V

A; R.

Wlez

ien, Io

wa St

ate

Unive

rsity,

Ames,

IA; R

. King

, M. C

houd

hari,

NASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA

Tues

day,

23 Ju

ne 2

015

138-

FD-1

7Bo

unda

ry La

yer a

nd B

luff B

ody C

ontro

lSe

nato

rs Le

cture

Hall

Chair

ed by

: Z. Z

HANG

, Univ

ersity

of Te

nnes

see a

nd J.

LIN,

NAS

A-Lan

gley R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-2

777

Cont

rol o

f Afte

rbod

y Vor

tices

by

Blow

ingR.

Jack

son,

Z. Wa

ng, I

. Gurs

ul, U

nivers

ity

of Ba

th, B

ath, U

nited

King

dom

1430

hrs

AIAA-2

015-2

778

Simpli

fied m

odel

for fl

ow-h

eatin

g ef

fect

on w

ave d

rag o

f blun

t bod

ies

and i

ts va

lidat

ionE.

Schü

lein,

Germ

an Ae

rospa

ce Ce

nter

(DLR

), Gö

ttinge

n, Ge

rman

y

1500

hrs

AIAA-2

015-2

779

The e

ffects

of M

ach a

nd Re

ynold

s nu

mber

on th

e flow

mixi

ng pr

opert

ies

of mi

cro-ra

mp vo

rtex g

enera

tors in

a su

perso

nic bo

unda

ry la

yer

R. Gie

pman

, A. S

rivast

ava,

F. Schr

ijer, B

. van

Ou

dheu

sden,

Delft

Unive

rsity o

f Tech

nolog

y, De

lft, Th

e Neth

erlan

ds

1530

hrs

AIAA-2

015-2

780

Expe

rimen

tal in

vesti

gatio

n of

bo

unda

ry la

yer t

rippin

g dev

ices

for s

hock

wav

e - bo

unda

ry la

yer

cont

rol

R. Gie

pman

, R. L

ouma

n, F.

Schri

jer, B

. va

n Oud

heus

den,

Delft

Unive

rsity

of Te

chno

logy,

Delft,

The N

etherl

ands

1600

hrs

AIAA-2

015-2

781

Cont

rol o

f Sho

ck W

ave B

ound

ary

Laye

r Int

erac

tion

using

Lase

r Puls

e En

ergy

Dep

ositio

nsA.

Iwak

awa,

T. Ta

mba,

P. So

n, T.

Shod

a, A.

Saso

h, Na

goya

Univ

ersity

, Nag

oya,

Japa

n

76

Tues

day,

23 Ju

ne 2

015

139-

FD-1

8Tu

rbule

nce M

odeli

ngEd

elweis

sCh

aired

by: C

. RUM

SEY,

NASA

-Lang

ley Re

searc

h Cen

ter an

d G. B

LAISD

ELL,

Purdu

e Univ

ersity

1400

hrs

AIAA-2

015-2

782

Stretc

hed-

Vorte

x ba

sed S

ubgr

id-sca

le Mo

delin

g of V

ariab

le-De

nsity

Flo

wsG.

Sidh

arth,

G. Ca

ndler

, Univ

ersity

of

Minn

esota

, Minn

eapo

lis, M

innea

polis,

MN

; P. D

imota

kis, C

alifor

nia In

stitut

e of

Tech

nolog

y, Pa

sade

na, C

A

1430

hrs

AIAA-2

015-2

783

DNS/

LES S

imula

tions

of Se

para

ted

Flows

at H

igh R

eyno

lds N

umbe

rsP.

Balak

umar,

NAS

A Lan

gley R

esea

rch

Cente

r, Ham

pton,

VA; G

. Park

, Stan

ford

Unive

rsity,

Palo

Alto,

CA

1500

hrs

AIAA-2

015-2

784

Baye

sian

Calib

ratio

n of

a RA

NS

Mode

l with

a Co

mplex

Res

pons

e Su

rface

- A

Case

Stud

y with

Jet-i

n-Cr

ossfl

ow Co

nfigu

ratio

nJ.

Ray,

S. Le

fantzi

, San

dia N

ation

al La

borat

ories

, Live

rmore

, CA;

S.

Aruna

jates

an, L

. DeC

hant,

San

dia N

ation

al La

borat

ories

, Albu

querq

ue, N

M

1530

hrs

AIAA-2

015-2

785

Exten

sion

of W

ray-

Agar

wal

Turb

ulenc

e Mod

el fo

r Flow

Ove

r Ro

ugh

Surfa

ces

T. W

ray, R

. Aga

rwal,

Was

hingto

n Un

iversi

ty in

St. L

ouis,

St.

Louis

, MO

1600

hrs

AIAA-2

015-2

786

An Im

prov

ed Ve

rsion

of O

ne-

Equa

tion

RAS T

urbu

lence

Mod

elM.

Rahm

an, A

alto U

nivers

ity, H

elsink

i, Fin

land;

R. Ag

arwal,

Was

hingto

n Un

iversi

ty in

St. L

ouis,

St.

Louis

, MO;

M.

Lamp

inen,

T. Sii

kone

n, Aa

lto U

nivers

ity,

Helsin

ki, Fi

nland

Tues

day,

23 Ju

ne 2

015

140-

ITAR-

2ITA

R - A

ircra

ft De

sign

and M

odeli

ng

Moro

ccoCh

aired

by: K

. CAS

PER

1400

hrs

AIAA-2

015-2

787

Deve

lopme

nt an

d Tes

ting o

f a So

lar

Powe

red A

ircra

ftJ.

Jaco

b, Ok

lahom

a Stat

e Univ

ersity

, St

illwate

r, OK;

J. Gr

imsle

y, S.

Atkin

s, De

sign I

ntellig

ence

, Inc

., No

rman

, OK

1430

hrs

AIAA-2

015-2

788

Airfi

eld Li

fting

Load

s a CF

D/Fu

ll Sc

ale R

otar

y Wing

Test

Study

F. Za

jaczk

owsk

i, J. T

arter,

T. B

agwe

ll, Ap

plied

Rese

arch L

abora

tory,

State

Co

llege

, PA

Tues

day,

23 Ju

ne 2

015

141-

MAO-

4Ap

plica

tions

IIMa

drid

Chair

ed by

: R. K

HIRE

, Unit

ed Te

chno

logies

Rese

arch C

enter

and E

. WIN

ER, I

owa S

tate U

nivers

ity14

00 hr

sAIA

A-201

5-278

9De

sign S

pace

Explo

ratio

n of W

ingbo

x Su

bstru

ctures

Confi

gura

tion U

sing

SPAN

DSET

C. Po

tter, G

eorgi

a Inst

itute

of Tec

hnolo

gy,

Atlan

ta, GA

; S. R

ussell,

Trium

ph Ae

rostru

ctures

, Da

llas, T

X; V.

Kim, Z

. Liu,

D. M

avris,

Georg

ia Ins

titute

of Tec

hnolo

gy, At

lanta,

GA

1430

hrs

AIAA-2

015-2

790

High

-Fide

lity A

eros

tructu

ral

Otim

izatio

n Co

nside

ring B

uffe

t On

set

G. Ke

nway

, J. M

artins

, Univ

ersity

of

Mich

igan,

Ann A

rbor, A

nn Ar

bor, M

I

1500

hrs

AIAA-2

015-2

791

Aero

elasti

c Tail

oring

Stud

y of

an N

+2 Lo

w-bo

om Su

perso

nic

Comm

ercia

l Tra

nspo

rt Ai

rcraf

tC.

Pak,

NASA

Arms

trong

Fligh

t Res

earch

Ce

nter, E

dward

s, CA

1530

hrs

AIAA-2

015-2

792

Optim

al Mi

ssion

Pat

h fo

r the

Un

inhab

ited L

oyal

Wing

man

C. Hu

mphre

ys, R

. Cob

b, D.

Jacq

ues,

J. Re

eger,

Air F

orce I

nstitu

te of

Tech

nolog

y, W

right-

Patte

rson A

FB, O

H

1600

hrs

AIAA-2

015-2

793

Multid

iscipl

inary

Ana

lysis

of a

Box-

Wing

Airc

raft

Desig

ned f

or a

Regio

nal-J

et Mi

ssion

S. An

drews

, R. P

erez,

Roya

l Milit

ary

Colle

ge of

Cana

da, K

ingsto

n, Ca

nada

Tues

day,

23 Ju

ne 2

015

142-

MST-6

Shad

ow M

ode A

ssessm

ent u

sing R

ealis

tic Te

chno

logies

for N

ation

al Ai

rspac

e Sys

tem (S

MART

NAS

) Tes

t Bed

Dev

elopm

ent (

Invit

ed)

Trave

rtine

Chair

ed by

: K. P

ALOP

O, N

ASA A

mes R

esea

rch Ce

nter a

nd G

. CHA

TTER

JI, N

ASA A

mes R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-2

794

Shad

ow M

ode A

ssessm

ent u

sing

Reali

stic T

echno

logies

for t

he N

ation

al Air

spac

e Sys

tem (S

MART

NAS

) Tes

t Bed

Dev

elopm

ent (

Invite

d)K.

Palop

o, NA

SA Am

es Re

search

Cente

r, Mo

ffett F

ield, C

A; G.

Chatt

erji, U

nivers

ity of

Ca

liforni

a, Sa

nta Cr

uz, M

offett

Field

, CA;

M.

Gumi

nsky,

P. Glaa

b, NA

SA La

ngley

Resea

rch

Cente

r, Ham

pton,

VA

1430

hrs

AIAA-2

015-2

795

Desig

n Ch

allen

ges f

or a

Shad

ow

Mode

Asse

ssmen

t Too

l for

Air

Traffi

c Man

agem

ent (

Invit

ed)

R. Ho

ffman

, Metr

on Av

iation

, Inc

., Du

lles,

VA; J

. Kroz

el, In

nova

tion L

abora

tory,

Inc.,

Portla

nd, O

R; D.

Mille

r, J. S

mith,

Metr

on

Aviat

ion, I

nc.,

Dulle

s, VA

1500

hrs

AIAA-2

015-2

796

Platfo

rm A

s A Se

rvice

(PAA

S)

Arch

itectu

re fo

r NAS

A’s SM

ART N

AS

(Invit

ed)

P. Co

bb, M

. Blak

e, Cro

wn Co

nsult

ing, I

nc.,

Arling

ton, V

A

1530

hrs

AIAA-2

015-2

797

Arch

itectu

re D

evelo

pmen

t for

Sh

adow

Mod

e Asse

ssmen

ts of

Air

Traffi

c Man

agem

ent T

echn

ologie

s (In

vited

)P.

Kosti

uk, R

obus

t Ana

lytics

, Gam

brills,

MD

1600

hrs

AIAA-2

015-2

798

A Da

ta Ex

chan

ge an

d Tra

nsfo

rmat

ion Sy

stem

for S

MART

NA

S (In

vited

)P.

Cobb

, Crow

n Con

sultin

g, Inc

., Arl

ington

, VA

; M. G

arlan

d, Mo

saic

ATM,

Lees

burg,

VA

1630

hrs

AIAA-2

015-2

799

Para

llel S

imula

tion

of A

gent

-Bas

ed

Mode

l for

Air

Traffi

c Netw

ork

Y. Kim

, O. P

inon-F

ische

r, D. M

avris

, Ge

orgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1700

hrs

AIAA-2

015-2

800

An In

tegra

ted Fr

amew

ork

for

Mode

ling A

ir Ca

rrier

Beh

avior

, Po

licy,

and I

mpac

ts in

the U

.S. A

ir Tra

nspo

rtatio

n Sy

stem

B. H

orio,

V. Ku

mar, V

. Stou

ffer, S

. Has

an,

A. De

Cicco

, LMI

, Tys

ons C

orner,

VA; J

. Sm

ith, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA;

et al.

77

Tues

day,

23 Ju

ne 2

015

143-

PDL-6

Plasm

a Diag

nosti

cs I

Miro

Chair

ed by

: C. D

UMITR

ACHE

, Colo

rado S

tate U

nivers

ity14

00 hr

sAIA

A-201

5-280

1Co

mpos

ition-

Inde

pend

ent

Temp

erat

ure a

nd P

ressu

re

Meas

urem

ents

using

Line

shap

e Sc

aling

Info

rmat

ion fr

om K

r PLIF

D. Ze

lenak

, F. K

idd, V

. Nara

yana

swam

y, No

rth Ca

rolina

Stat

e Univ

ersity

, Rale

igh,

NC

1430

hrs

AIAA-2

015-2

802

Comp

utat

ional

and E

xper

imen

tal

Lase

r Diff

eren

tial I

nter

fero

metry

fo

r Sup

erso

nic Tu

rbule

nt B

ound

ary-

Laye

r Flow

N. B

isek,

M. B

rown,

Air Fo

rce Re

searc

h La

borat

ory, W

right-

Patte

rson A

FB, O

H

1500

hrs

AIAA-2

015-2

803

Unde

rstan

ding t

he Im

pact

of

Buffe

r Gas

es on

the R

adar

REM

PI

Diag

nosti

cT.

Chng

, R. M

iles,

Princ

eton U

nivers

ity,

Princ

eton,

NJ

1530

hrs

AIAA-2

015-2

804

Wave

front

Mea

sure

ment

s of a

Su

perso

nic B

ound

ary L

ayer

Usin

g a

Lase

r-Ind

uced

Bre

akdo

wn Sp

ark

M. N

guye

n, M.

Renn

ie, S.

Gorde

yev,

E. Jum

per, U

nivers

ity of

Notr

e Dam

e, No

tre

Dame

, IN; A

. Cain

, Inno

vativ

e Tech

nolog

y Ap

plicati

ons C

ompa

ny, LL

C, Ch

esterfi

eld, M

O;

T. Ha

yden

, U.S.

Air F

orce A

cadem

y, Co

lorad

o Sp

rings,

CO

1600

hrs

AIAA-2

015-2

805

Lang

muir

Prob

e Diag

nosti

cs of

an

Atmo

sphe

ric-P

ressu

re M

icrop

lasma

L. Bla

ir, K.

Xu, U

nivers

ity of

Alab

ama,

Hunts

ville,

Hun

tsville

, AL

Tues

day,

23 Ju

ne 2

015

144-

PDL-7

Plasm

a Aer

odyn

amics

& Fl

ow Co

ntro

l III

Mone

t Ball

room

Chair

ed by

: T. M

OELLE

R, Un

iversi

ty of

Tenn

esse

e Spa

ce In

stitut

e14

00 hr

sAIA

A-201

5-280

6In

vesti

gatio

n of

Cath

odic-

Arc-J

et In

fluen

ce on

Cros

s Flow

usin

g Pa

rticle

Imag

e Velo

cimetr

yI.

Kronh

aus,

Tech

nion--

Israe

l Insti

tute o

f Te

chno

logy,

Haifa

, Isra

el

1430

hrs

AIAA-2

015-2

807

Dyna

mics

of Ch

arge

Tran

sfer i

n At

mosp

heric

Pre

ssure

Bar

rier

Disch

arge

at Si

ngle

and A

ltern

ative

Po

laritie

s of S

upply

ing Vo

ltage

S. Le

onov

, Univ

ersity

of N

otre D

ame,

Notre

Dam

e, IN

1500

hrs

AIAA-2

015-2

808

Effect

of N

ew El

ectro

n Imp

act

Ioniza

tion o

n the

Aero

dyna

mic

Heati

ng En

viron

ment

for Su

per-O

rbita

l Re

entry

Vehic

lesH.

Otsu,

Ryuk

oku U

nivers

ity, O

tsu, J

apan

; K.

Yama

da, T

. Abe

, Jap

an Ae

rospa

ce Ex

plorat

ion

Agen

cy (JA

XA),

Saga

miha

ra, Ja

pan

1530

hrs

AIAA-2

015-2

809

Nume

rical

Study

on P

erfo

rman

ce

Impr

ovem

ent M

echa

nism

of Tr

i-Ele

ctrod

e Plas

ma A

ctuat

orH.

Nish

ida, M

. Tam

ura, T

okyo

Univ

ersity

of

Agric

ulture

and T

echn

ology

, Kog

anei,

Ja

pan;

T. Ma

tsuno

, Tott

ori U

nivers

ity,

Totto

ri, Ja

pan

1600

hrs

AIAA-2

015-2

810

Effe

ct of

Volta

ge an

d Fre

quen

cy

on St

artin

g Rep

etitiv

e Nan

osec

ond

Pulse

d DBD

X. H

an, H

. Li, X

. Men

g, No

rthwe

stern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

; F.

Liu, S

. Luo

, Univ

ersity

of Ca

liforni

a, Irv

ine,

Los A

ngele

s, CA

Tues

day,

23 Ju

ne 2

015

145-

TP-7

Heat

Tran

sfer I

IRo

setta

Chair

ed by

: E. S

HORT

, Ray

theon

Comp

any a

nd E.

KHAL

IL, Ca

iro U

nivers

ity14

00 hr

sAIA

A-201

5-281

1Re

spon

se of

poro

us fo

ams fi

lled

with

phas

e cha

nge m

ater

ial u

nder

tra

nsien

t hea

ting

G. Jac

kson,

K. Sm

ith, P.

Mcca

rthy,

T. Fis

her,

Purdu

e Univ

ersity,

West

Lafay

ette,

IN

1430

hrs

AIAA-2

015-2

812

Evalu

ation

of di

ffere

nt Tu

rbule

nce

Mode

ls fo

r ana

lysis

of Je

t Im

pinge

ment

in G

as Tu

rbine

Blad

esB.

Upa

lkar, M

. Rick

lick, E

mbry-

Riddle

Ae

ronau

tical

Unive

rsity,

Day

tona B

each

, FL

1500

hrs

AIAA-2

015-2

813

Benc

hmar

king o

f Com

puta

tiona

l Mo

dels

For A

diaba

tic Fi

lm-C

oolin

g Ef

fecti

vene

ss Fo

r Lar

ge Sp

acing

Co

mpou

nd A

ngle

Full C

over

age

Film

Cooli

ng A

rrays

S. M

artine

z, M.

Rick

lick, E

mbry-

Riddle

Ae

ronau

tical

Unive

rsity,

Day

tona B

each

, FL

1530

hrs

AIAA-2

015-2

814

Nume

rical

Analy

sis of

Film

Cooli

ng

Char

acter

istic

on a

Turb

ine N

on-

axisy

mmetr

ic Co

ntou

red E

ndwa

llQ.

Pan,

H. Ta

ng, J

. Bai,

Aviat

ion In

dustr

y Co

rporat

ion of

China

(AVIC

), Sh

angh

ai,

China

1600

hrs

AIAA-2

015-2

815

POD

Analy

sis of

the T

rans

ient

Flow

Field

at P

ulse E

ngine

Exha

ust

Regio

nW.

Cai, C

. Yan

g, B.

Qi, H

. Ma,

L. Yu

, X.

Chen

, Nan

jing U

nivers

ity of

Scie

nce a

nd

Tech

nolog

y, Na

njing

, Chin

a

1630

hrs

AIAA-2

015-2

816

Fluid

flow

and h

eat t

rans

fer i

n a

rota

ting t

wo-p

ass s

quar

e cha

nnel

with

smoo

th w

alls a

nd ax

ial

inwar

d/ou

twar

d flow

J. Ba

i, Q. P

an, A

viatio

n Ind

ustry

Corpo

ration

of

China

(AVIC

), Sh

angh

ai, Ch

ina

1700

hrs

AIAA-2

015-2

817

Nume

rical

and e

xper

imen

tal

analy

sis of

hea

t tra

nsfe

r of p

iccolo

tu

be je

t imp

ingem

ent o

n a c

onca

ve

surfa

ceY.

Bo, S

. Cha

ng, Y

. Zha

o, M.

Leng

, Be

ihang

Univ

ersity

, Beij

ing, C

hina

Tues

day,

23 Ju

ne 2

015

146-

NW-4

15

30 -

1600

hrs

Netw

orkin

g Cof

fee B

reak

Chan

tilly B

allro

om Ea

st

Tues

day,

23 Ju

ne 2

015

147-

LEC-

2 16

30 -

1730

hrs

Plasm

adyn

amics

and L

aser

s Awa

rd Le

cture

Gran

d Ball

room

D

From

Plasm

adyn

amics

and S

hock

Tube

s to A

ero-Op

tics a

nd La

ser Ra

dar: A

n Aero

spac

e Care

erPh

ilip E.

Cassa

dySe

nior T

echn

ical F

ellow

(Reti

red)

The B

oeing

Comp

any

78

Tues

day,

23 Ju

ne 2

015

148-

NW-5

17

30 -

1900

hrs

Rece

ption

in th

e Exp

ositio

n Ha

llCh

antill

y Ball

room

East

A tick

et is

requir

ed an

d inc

luded

in th

e con

feren

ce re

gistra

tion f

ee w

here

indica

ted.

Wedn

esda

y

Wedn

esda

y, 24

June

201

514

9-SB

-3

0730

- 08

00 h

rsSp

eake

rs’ B

riefin

gSe

ssion

Roo

ms

Wedn

esda

y, 24

June

201

515

0-PL

NRY-3

08

00 -

0900

hrs

Plena

ry K

eyno

teCh

antill

y Ball

room

Wes

t

NASA

and t

he Fu

ture o

f Aero

spac

eCh

arles

F. B

olden

Jr.

Admi

nistra

torNa

tiona

l Aero

nauti

cs an

d Spa

ce Ad

minis

tratio

n

Wedn

esda

y, 24

June

201

515

1-AA

-21

Turb

omac

hiner

y and

Core

Nois

eFle

ur-d

e-lis

BCh

aired

by: H

. ATA

SSI,

Unive

rsity

of No

tre D

ame

0900

hrs

AIAA-2

015-2

818

Entro

py N

oise G

ener

ation

and

Redu

ction

in a

Heat

ed N

ozzle

Flow

K. Kn

obloc

h, T.

Werne

r, F. B

ake,

Germ

an

Aeros

pace

Cente

r (DL

R), B

erlin,

Germ

any

0930

hrs

AIAA-2

015-2

819

Dyna

mic T

empe

ratu

re an

d Pre

ssure

Me

asur

emen

ts in

the C

ore o

f a

Prop

ulsion

Engin

eW.

Sch

uster

, Hon

eywe

ll Inte

rnatio

nal,

Inc.,

Phoe

nix, A

Z; L.

Hultg

ren, N

ASA G

lenn

Rese

arch C

enter

, Clev

eland

, OH

1000

hrs

AIAA-2

015-2

820

Broa

dban

d ind

irect

noise

ge

nera

tion

by ac

celer

ated

vorti

city

N. Ki

ngs,

L. En

ghard

t, F.

Bake

, Germ

an

Aeros

pace

Cente

r (DL

R), B

erlin,

Germ

any

1030

hrs

AIAA-2

015-2

821

Linea

r Ana

lysis

of En

gine C

ore

Noise

Usin

g a H

ybrid

Mod

eling

Ap

proa

chJ.

O’Br

ien, J

. Kim

, M. I

hme,

Stan

ford

Unive

rsity,

Stan

ford,

CA

1100

hrs

AIAA-2

015-2

822

Acou

stic C

ompa

rison

of D

iffer

ent

Turb

ine Ex

it Gu

ide Va

ne D

esign

s - P

art 1

: Des

ign P

hilos

ophy

and

Nume

rical

Pred

iction

sD.

Bros

zat,

M. H

öger,

MTU

Aero

Engin

es,

Munic

h, Ge

rman

y; A.

Marn,

T. S

elic,

F. Sc

hönle

itner,

F. H

eitme

ir, Gr

az U

nivers

ity

of Te

chno

logy,

Graz

, Aus

tria

1130

hrs

AIAA-2

015-2

823

Acou

stic C

ompa

rison

of D

iffer

ent

Turb

ine Ex

it Gu

ide Va

ne D

esign

s Pa

rt 2:

Expe

rimen

tal A

nalys

isA.

Marn,

T. S

elic,

F. Sc

hönle

itner,

S.

Zerob

in, G

raz U

nivers

ity of

Tech

nolog

y, Gr

az, A

ustria

; D. B

rosza

t, M.

Hög

er, M

TU

Aero

Engin

es, M

unich

, Germ

any;

et al.

1200

hrs

AIAA-2

015-2

824

Expe

rimen

tal S

tudy

on th

e Tu

rbom

achin

ery T

railin

g Edg

e Nois

e Re

ducti

on B

ased

on Li

near

Casca

de

Test

with

Pha

sed A

rray

W. Q

iao, L

. Wan

g, W.

Chen

, F. T

ong,

L. Ji,

Nort

hwes

tern P

olytec

hnica

l Univ

ersity

, Xi’

an, C

hina

Wedn

esda

y, 24

June

201

515

2-AA

-22

Gene

ral A

cous

tics I

IIn

vern

ess

Chair

ed by

: S. R

IZZI,

NASA

Lang

ley Re

searc

h Cen

ter09

00 hr

sAIA

A-201

5-282

5On

a mo

de-m

atchin

g tech

nique

for

soun

d gen

eratio

n and

tran

smiss

ion in

a l

inear

casca

de of

outle

t guid

e van

esS.

Boule

y, B.

Franço

is, M.

Roge

r, Écol

e Ce

ntrale

de Ly

on, E

cully,

France

; S. M

oreau

, Un

iversit

y of S

herbr

ooke

, She

rbroo

ke, C

anad

a

0930

hrs

AIAA-2

015-2

826

Noise

cont

rol b

y a ro

tatin

g rod

in a

rod-

airfo

il con

figur

ation

L. Sio

zos-R

ouso

ulis,

G. G

horba

niasl,

C.

Laco

r, Vrije

Univ

ersite

it Brus

sel, B

russe

ls,

Belgi

um

1000

hrs

AIAA-2

015-2

827

Acou

stic e

ffects

of a

rota

tiona

lly

oscil

lating

rod i

n a r

od-a

irfoil

co

nfigu

ratio

nL.

Siozo

s-Rou

souli

s, G.

Gho

rbania

sl, C.

La

cor, V

rije U

nivers

iteit B

russe

l, Brus

sels,

Be

lgium

1030

hrs

AIAA-2

015-2

828

Activ

e Con

trol o

f Fan

Tone

s by

mean

s of T

railin

g Edg

e Blow

ingL.

Engh

ardt,

P. Ka

usch

e, A.

Morea

u, Ge

rman

Aeros

pace

Cente

r (DL

R), B

erlin,

Ge

rman

y; T.

Carol

us, U

nivers

ity of

Sieg

en,

Siege

n, Ge

rman

y

1100

hrs

AIAA-2

015-2

829

Acou

stic R

eson

ance

Phe

nome

na

in a T

hree

-Dim

ensio

nal C

asca

de

Inter

actin

g with

Onc

oming

Un

stead

y Wak

esH.

Koda

ma, I

HI Co

rporat

ion, N

ishita

ma,

Japa

n; M.

Nam

ba, K

yusy

u Univ

ersity

, Fu

kuok

a, Ja

pan

1130

hrs

AIAA-2

015-2

830

Aero

foil g

eome

try ef

fects

on

turb

ulenc

e int

erac

tion

noise

C. Pa

ruchu

ri, J.

Gill, N

. Sub

raman

ian,

P. Jo

seph

, C. V

ande

rwel,

X. Z

hang

, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom;

et al

.

1200

hrs

AIAA-2

015-2

831

Wall-

Moun

ted Fi

nite A

irfoil

Nois

e Pr

oduc

tion

and P

redic

tion

D. M

oreau

, C. D

oolan

, Univ

ersity

of

New

South

Wale

s, Sy

dney

, Aus

tralia

; W.

Alex

ande

r, T. M

eyers

, W. D

even

port,

Vir

ginia

Polyt

echn

ic Ins

titute

and S

tate

Unive

rsity,

Blac

ksbu

rg, VA

79

Wedn

esda

y, 24

June

201

515

3-AA

-23

Jet N

oise N

ear F

ield a

nd Je

t Nois

e Red

uctio

nLa

lique

Chair

ed by

: A. P

ILON,

Lock

heed

Mart

in Ae

ronau

tics

0900

hrs

AIAA-2

015-2

832

On Th

eore

tical

Broa

dban

d Sho

ck-

Asso

ciated

Nois

e Nea

r-Fiel

d Cro

ss-Sp

ectra

S. M

iller, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

0930

hrs

AIAA-2

015-2

833

Near

-field

Pre

ssure

Wav

efor

m An

alysis

of an

Excit

ed M

ach

0.9

Jet

C. Ku

o, M.

Craw

ley, M

. Sam

imy,

Ohio

State

Univ

ersity

, Colu

mbus

, OH

1000

hrs

AIAA-2

015-2

834

Meas

uring

shea

r lay

er gr

owth

ra

tes in

aero

acou

stica

lly fo

rced

axisy

mmetr

ic su

perso

nic je

tsD.

Edgin

gton-M

itche

ll, O.

Amili,

D.

Honn

ery, J

. Sori

a, Mo

nash

Univ

ersity

, Me

lbourn

e, Au

strali

a

1030

hrs

AIAA-2

015-2

835

Impa

ct of

Chev

rons

on N

oise

Sour

ce Ch

arac

terist

ics In

Im

perfe

ctly E

xpan

ded J

et Flo

wsJ.

Liu, A

. Corr

igan,

K. Ka

ilasa

nath,

Nav

al Re

searc

h Lab

orator

y, Wa

shing

ton, D

C; E.

Gutm

ark, U

nivers

ity of

Cinc

innati

, Cin

cinna

ti, OH

1100

hrs

AIAA-2

015-2

836

Effe

ct of

Inve

rted T

riang

ular T

abs

on M

itigat

ion of

Jet N

oise f

rom

Axisy

mmetr

ic Co

nver

gent

Noz

zles

A. Su

brama

nyam

, K. N

ataraj

an, N

ation

al Ae

rospa

ce La

borat

ories

, Ban

galor

e, Ind

ia

1130

hrs

AIAA-2

015-2

837

An In

vesti

gatio

n of

Twin

Supe

rsonic

Je

ts’ N

ear-fi

eldJ.

Cluts,

C. Ku

o, M.

Sam

imy,

Ohio

State

Un

iversi

ty, Co

lumbu

s, OH

1200

hrs

AIAA-2

015-2

838

Acou

stic s

ource

analy

sis of

a su

perso

nic re

ctang

ular c

hevr

on je

tJ.

Kreitz

man,

J. Nic

hols,

Univ

ersity

of

Minn

esota

, Minn

eapo

lis, M

innea

polis,

MN

Wedn

esda

y, 24

June

201

515

4-AA

-24

CAA

Prop

agat

ion an

d Sca

tterin

g II

Obeli

sk A

Chair

ed by

: M. R

OGER

, Eco

le Ce

ntrale

de Ly

on09

00 hr

sAIA

A-201

5-283

9CA

A ana

lysis o

f a W

ing Se

ction

with

Fla

p Side

-Edge

s Bas

ed on

Hyb

rid

RANS

-LES C

ompu

tation

S. Pe

ng, L

. Tyse

ll, Sw

edish

Defen

se Re

search

Ag

ency

(FOI)

, Stoc

kholm

, Swe

den;

H. Ya

o, L.

David

son, L

. Erik

sson,

Chalm

ers Un

iversit

y of

Techn

ology,

Göteb

org, S

wede

n

0930

hrs

AIAA-2

015-2

840

Pred

iction

of Fa

r-Fiel

d Wind

Turb

ine

Noise

Pro

paga

tion

with

Par

aboli

c Eq

uatio

nS.

Lee,

Gene

ral El

ectric

Comp

any,

Niska

yuna

, NY

1000

hrs

AIAA-2

015-2

841

Nume

rical

simula

tion

of sp

ectra

l br

oade

ning o

f an

acou

stic w

ave

by a

spat

ially

grow

ing tu

rbule

nt

mixin

g lay

erI.

Benn

aceu

r, D. M

incu,

I. Ma

ry, M

. Te

rraco

l, ONE

RA, C

hâtill

on, F

rance

; L.

Larch

eveq

ue, D

. Pier

re, Ai

x-Mars

eille

Unive

rsity,

Mars

eille,

Fran

ce

1030

hrs

AIAA-2

015-2

842

Comp

ariso

n of

Comp

utat

ional

Aero

acou

stics

Pred

iction

of Vo

rtica

l Gu

st Sc

atter

ing by

a 2D

Stat

or w

ith

Flat P

late T

heor

yC.

Duran

d, D.

Hixo

n, Un

iversi

ty of

Toled

o, To

ledo,

OH

1100

hrs

AIAA-2

015-2

843

Nume

rical

and A

nalyt

ical

Inve

stiga

tion

of O

rthog

onal

Blad

e/Vo

rtex

Inter

actio

n No

iseF.

Faliss

ard, P

. Zeh

ner, O

NERA

, Châ

tillon

, Fra

nce;

M. Ro

ger, É

cole

Centr

ale de

Lyon

, Ec

ully,

Franc

e; X.

Gloe

rfelt,

Arts M

etiers

Pa

risTe

ch, P

aris,

Franc

e

Wedn

esda

y, 24

June

201

515

5-AA

-25

Benc

hmar

k Pr

oblem

s for

Airf

rame

Nois

e Com

puta

tions

III (

BANC

-III)

Summ

ary (

Invit

ed)

Fleur

-de-

lis A

Chair

ed by

: M. C

HOUD

HARI,

NAS

A-Lan

gley R

esea

rch Ce

nter

0900

hrs

Oral

Prese

ntatio

nAn

Ove

rview

of Co

ntrib

ution

s on

Nose

Land

ing G

ear C

onfig

urat

ion

for B

ANC-

III W

orks

hop

M. Kh

orram

i, NAS

A Lan

gley R

esea

rch

Cente

r, Ham

pton,

VA

0930

hrs

AIAA-2

015-2

844

Asse

ssmen

t of S

lat N

oise

Pred

iction

s for

30P

30N

High

-Lift

Confi

gura

tion

from

BANC

-III

Work

shop

M. Ch

oudh

ari, D

. Loc

kard,

NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA

1000

hrs

AIAA-2

015-2

845

Varia

bility

in th

e Pro

paga

tion P

hase

of

CFD-

Based

Nois

e Pred

iction

: Sum

mary

of

Resu

lts fr

om Ca

tegor

y 8 of

the

BANC

-III W

orks

hop

L. Lo

pes,

NASA

Lang

ley Re

search

Cente

r, Ha

mpton

, VA;

S. Re

donn

et, O

NERA

, Tou

louse,

Fra

nce; T

. Imam

ura, U

nivers

ity of

Toky

o, Tok

yo, J

apan

; T. Ik

eda,

Japan

Aeros

pace

Ex

plorat

ion Ag

ency

(JAXA

), Ch

ofu, J

apan

; N.

Zawo

dny,

NASA

Lang

ley Re

search

Cente

r, Ha

mpton

, VA;

G. Cu

nha,

ONER

A, Tou

louse,

Fra

nce

1030

hrs

AIAA-2

015-2

846

Summ

ary o

f the

LAGO

ON So

lution

s fro

m th

e Ben

chma

rk pr

oblem

s for

Ai

rfram

e Nois

e Com

puta

tions

-III

Work

shop

E. Ma

noha

, ONE

RA, C

hâtill

on, F

rance

; B.

Carue

lle, A

irbus

, Tou

louse

, Fran

ce

1100

hrs

AIAA-2

015-2

847

Broa

dban

d Tra

iling-

Edge

Nois

e Pr

edict

ions—

Over

view

of B

ANC-

III

Resu

ltsM.

Herr

, R. E

wert,

C. Ra

utman

n, Ge

rman

Ae

rospa

ce Ce

nter (

DLR)

, Brau

nsch

weig,

Ge

rman

y; M.

Kamr

uzza

man,

ENER

CON

GmbH

, Auri

ch, G

erman

y; D.

Bek

iropo

ulos,

Unive

rsity

of St

uttga

rt, S

tuttga

rt,

Germ

any;

R. Ari

na, T

echn

ical U

nivers

ity of

Tu

rin, T

orino

, Ital

y; et

al.

80

Wedn

esda

y, 24

June

201

515

6-AC

D-4

Gene

ral A

viatio

nMo

rocco

Chair

ed by

: M. O

RR, B

oeing

Comm

ercial

Airpl

anes

0900

hrs

AIAA-2

015-2

848

Iden

tifyin

g High

-Risk

Occu

rrenc

e Ch

ains i

n He

licop

ter O

pera

tions

fro

m Ac

ciden

t Dat

aA.

Rao,

K. Ma

rais,

Purdu

e Univ

ersity

, Wes

t La

fayett

e, IN

0930

hrs

AIAA-2

015-2

849

Pilot

Per

cept

ion an

d Use

of A

DS-B

In

Traf

fic an

d Wea

ther

Serv

ices

(TIS-

B an

d FIS-

B)S.

Silv

a, L.

Jens

en, R

. Han

sman

, Ma

ssach

usett

s Ins

titute

of Te

chno

logy,

Camb

ridge

, MA

1000

hrs

AIAA-2

015-2

850

Imple

menta

taion

and V

alida

tion o

f an

Inter

nal C

ombu

stion

Engin

e and

Pr

opell

er Mo

del fo

r Gen

eral A

viatio

n Air

craft

Perfo

rman

ce Stu

dies

E. Ha

rrison

, S. M

in, H.

Jimen

ez, D

. Mav

ris,

Georg

ia Ins

titute

of Tec

hnolo

gy, At

lanta,

GA

1030

hrs

AIAA-2

015-2

851

Iden

tifyin

g Pha

ses o

f Flig

ht in

Ge

nera

l Avia

tion

Oper

ation

sN.

Fala,

V. G

oblet

, K. M

arais,

Purdu

e Un

iversi

ty, W

est L

afaye

tte, I

N

1100

hrs

AIAA-2

015-2

852

Pilot

-Frien

dline

ss Co

nside

ratio

ns fo

r Pe

rsona

l Air

Vehic

le Fli

ght C

ontro

l Sy

stems

I. Ch

akrab

orty,

B. Lo

zano

, D. M

avris

, Ge

orgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1130

hrs

AIAA-2

015-2

853

Deve

lopme

nt of

Aero

dyna

mic

Mode

ling a

nd Ca

libra

tion M

ethod

s for

Ge

nera

l Avia

tion A

ircra

ft Pe

rform

ance

An

alysis

- a Su

rvey

and C

ompa

rison

of

Mode

lsS.

Min,

E. Ha

rrison

, H. J

imen

ez, D

. Mav

ris,

Georg

ia Ins

titute

of Tec

hnolo

gy, At

lanta,

GA

Wedn

esda

y, 24

June

201

515

7-AF

M-9

Unma

nned

Airc

raft

Syste

ms II

Plum

Blos

som

ACh

aired

by: T

. FIEL

DS, U

nivers

ity of

Miss

ouri a

nd G

. SHA

H, N

ASA-L

angle

y Res

earch

Cente

r09

00 hr

sAIA

A-201

5-285

4Un

stead

y Aer

odyn

amics

Mod

eling

fo

r a Fl

exibl

e Unm

anne

d Air

Vehic

leA.

Kotik

alpud

i, H. P

fifer, G

. Bala

s, Un

iversi

ty of

Minn

esota

, Minn

eapo

lis,

Minn

eapo

lis, M

N

0930

hrs

AIAA-2

015-2

855

A Com

paris

on of

Filte

rs for

UAS

-Bas

ed

Loca

lizati

on of

Stati

onar

y RF S

ource

sM.

Stach

ura, B

lack S

wift T

echno

logies

, LLC

, Bo

ulder,

CO; N

. Wag

le, E.

Frew

, Univ

ersity

of

Color

ado,

Bould

er, Bo

ulder,

CO

1000

hrs

AIAA-2

015-2

856

Robu

st Th

ree-

Dime

nsion

al Ch

arac

teriza

tion

of a

Comp

lex

Atmo

sphe

re at

High

Res

olutio

n us

ing M

ulti-A

gent

Wind

mapp

ers

C. Mo

ntalvo

, J. R

ichard

son,

J. Ma

rshall

, Un

iversi

ty of

South

Alab

ama,

Mobil

e, AL

1030

hrs

AIAA-2

015-2

857

Nonli

near

Mod

el Pr

edict

ive Co

ntro

l Ap

plied

to Tr

ajecto

ry Tr

ackin

g for

Un

mann

ed A

erial

Vehic

lesK.

Subb

arao,

C. Tu

le, P.

Ru, U

nivers

ity of

Te

xas,

Arling

ton, A

rlingto

n, TX

1100

hrs

AIAA-2

015-2

858

A La

unch

Syste

m De

sign

Meth

odolo

gy fo

r Sma

ll Unm

anne

d Ai

rcraf

t App

licat

ions

A. Pa

tterso

n, A.

Arena

, Okla

homa

Stat

e Un

iversi

ty, S

tillwa

ter, O

K

1130

hrs

AIAA-2

015-2

859

Feas

ibility

Stud

y of C

losed

Cycle

Pr

opuls

ion fo

r Unm

anne

d Aer

ial

Syste

msT.

Hays

, A. A

rena,

Oklah

oma S

tate

Unive

rsity,

Still

water

, OK

Wedn

esda

y, 24

June

201

515

8-AM

T-9/G

T-9Gr

ound

Test

Facil

ity Im

prov

emen

ts I

Obeli

sk B

Chair

ed by

: R. R

HEW,

NAS

A-Lan

gley R

esea

rch Ce

nter a

nd S

. SIM

ERLY,

NAS

A Glen

n Res

earch

Cente

r09

00 hr

sAIA

A-201

5-286

0De

velop

ment

of a

Rese

arch

Facil

ity

to St

udy t

he Fl

ow Fi

eld in

an A

PU-

Style

Inlet

F. Lo

u, W.

Murr

ay, N

. Key

, Purd

ue

Unive

rsity,

Wes

t Lafa

yette

, IN

0930

hrs

AIAA-2

015-2

861

Deve

lopme

nt an

d Tes

ting o

f an

Unste

ady L

ow-S

peed

Wind

Tunn

elD.

Gree

nblat

t, Te

chnio

n--Isr

ael In

stitut

e of

Tech

nolog

y, Ha

ifa, I

srael

1000

hrs

AIAA-2

015-2

862

Expa

nsion

of th

e AED

C H2

Arc

Heat

er Fa

cility

Test

Enve

lope U

sing

Cold-

Air M

ixing

G. H

ammo

ck, A

rnold

Engin

eerin

g De

velop

ment

Comp

lex, A

rnold

AFB,

TN

1030

hrs

AIAA-2

015-2

863

Expe

rimen

ts wi

th th

e Mod

el Te

st Ap

para

tus I

nsta

lled i

n th

e AFIT

Low

Spee

d Tun

nel

J. La

ncas

ter, M

. Ree

der, A

ir Forc

e Ins

titute

of Te

chno

logy,

Wrig

ht-Pa

tterso

n AFB

, OH;

M.

Syts

ma, A

ir Forc

e Res

earch

Labo

ratory

, Eg

lin AF

B, FL

; P. R

owe,

RE2,

Inc.,

Pit

tsburg

h, PA

; R. C

obb,

Air Fo

rce In

stitut

e of

Tech

nolog

y, W

right-

Patte

rson A

FB, O

H

1100

hrs

AIAA-2

015-2

864

Upgr

ades

to th

e Tex

as A

&M O

ran

W. N

icks L

ow-S

peed

Wind

Tunn

el fo

r M=0

.4 O

pera

tion

A. He

rring,

D. Ku

tz, L.

Brow

n, E.

Whit

e, Te

xas A

&M U

nivers

ity, C

olleg

e Stat

ion, T

X

1130

hrs

Oral

Prese

ntatio

nNA

SA La

ngley

Aer

oaco

ustic

Wind

Tu

nnel

Capa

bility

Mov

ing Fo

rwar

dM.

Doty

, F. H

utche

son,

H. H

askin

, P.

Quint

o, D.

Smi

th, N

ASA L

angle

y Res

earch

Ce

nter, H

ampto

n, VA

Wedn

esda

y, 24

June

201

515

9-AM

T-10/

GT-1

0Pa

rticle

-Bas

ed Ve

locim

etry A

pplic

ation

s and

Dev

elopm

ents

Topa

zCh

aired

by: K

. LOW

E, Vir

ginia

Tech

and C

. GOY

NE, U

nivers

ity of

Virg

inia

0900

hrs

AIAA-2

015-2

865

Veloc

ity M

easu

reme

nts i

n an

Un

seed

ed Tu

rboje

t Eng

ine Ex

haus

t Us

ing P

lanar

Dop

pler V

elocim

etry

T. Je

nkins

, Metr

oLas

er, In

c., La

guna

Hills

, CA

; J. S

eitzm

an, S

. Adu

sumi

lli, G

eorgi

a Ins

titute

of Te

chno

logy,

Atlan

ta, G

A

0930

hrs

AIAA-2

015-2

866

Stere

osco

pic P

IV m

easu

reme

nts

in a t

urbo

fan

engin

e inle

t with

ta

ilore

d swi

rl dis

torti

onM.

Nels

on, K

. Low

e, W.

O’B

rien,

C. Kir

k, Vir

ginia

Polyt

echn

ic Ins

titute

and S

tate

Unive

rsity,

Blac

ksbu

rg, VA

1000

hrs

AIAA-2

015-2

867

Multi-

stere

o PIV

mea

sure

ment

of

prop

eller

wak

e flow

in in

dustr

ial

facil

ityM.

Nov

ara, R

. Geis

ler, A

. Sch

roede

r, Ge

rman

Aeros

pace

Cente

r (DL

R),

Göttin

gen,

Germ

any

1030

hrs

AIAA-2

015-2

868

Appli

catio

n of

Par

ticle

Imag

e Ve

locim

etry a

nd La

ser I

nduc

ed

Fluor

esce

nce i

n a c

oolin

g duc

t flow

H. Ro

chlitz

, P. S

cholz

, Tec

hnica

l Univ

ersity

of

Brau

nsch

weig,

Brau

nsch

weig,

Germ

any

1100

hrs

AIAA-2

015-2

869

Biolo

gical

Flow

Meas

urem

ent u

sing

Optic

al Flo

w Me

thod

Z. Ya

ng, H

. Yu,

G. H

uang

, B. L

udwi

g, W

right

State

Univ

ersity

, Bea

vercr

eek,

OH

1130

hrs

AIAA-2

015-2

870

Deve

lopme

nt an

d cha

racte

rizat

ion

of an

inex

pens

ive LE

D-ba

sed

light

sour

ce fo

r high

-fram

e-ra

te sch

liere

n im

aging

D. Li

ncoln

, K. M

urari,

C. Jo

hans

en,

Unive

rsity

of Ca

lgary,

Calga

ry, Ca

nada

81

Wedn

esda

y, 24

June

201

516

0-AP

A-17

Spec

ial Se

ssion

: Hyb

rid CF

D Me

thod

Asse

ssmen

ts fo

r F-1

6XL A

ircra

ft Ae

rody

nami

csSte

mmon

s ACh

aired

by: J

. LUC

KRIN

G, N

ASA-L

angle

y Res

earch

Cente

r and

A. RI

ZZI,

KTH

Roya

l Insti

tute T

echn

ology

0900

hrs

AIAA-2

015-2

871

Free

-Fligh

t High

AoA

Flow

s Sim

ulatio

n at

Sub-

and T

rans

onic

Spee

ds -

F-16X

L (CA

WAPI

-3)

S. H

itzel,

Airbu

s, Ma

nchin

g, Ge

rman

y

0930

hrs

AIAA-2

015-2

872

F-16X

L Hyb

rid R

eyno

lds-A

vera

ged

Navie

r-Sto

kes/

Larg

e Edd

y Sim

ulatio

n on

Uns

tructu

red G

rids

M. Pa

rk, A.

Elmi

ligui,

K. Ab

dol-H

amid,

NA

SA La

ngley

Rese

arch C

enter

, Ham

pton,

VA

1000

hrs

AIAA-2

015-2

873

Nume

rical

Simula

tion o

f the

F-16

XL

at Fu

ll-Sc

ale Fl

ight T

est C

ondit

ions

Using

a Ne

ar-B

ody O

ff-Bo

dy CF

D Ap

proa

chS.

Mort

on, D

. McD

aniel

, CRE

ATE K

estre

l Te

am, E

glin A

FB, F

L

1030

hrs

AIAA-2

015-2

874

Hybr

id RA

NS-LE

S Sim

ulatio

ns of

F-1

6XL A

ircra

ft in

Low-

spee

d High

-alp

ha Fl

ight

M. To

mac,

A. Riz

zi, Ro

yal In

stitute

of

Techn

ology

(KTH

), Sto

ckholm

, Swe

den;

A. Jira

sek, P.

Elias

son, S

wedis

h Defe

nse Re

search

Ag

ency

(FOI)

, Stoc

kholm

, Swe

den

1100

hrs

AIAA-2

015-2

875

Nume

rical

Simula

tion o

f the

F-16

XL

at Fu

ll-Sc

ale Fl

ight T

est C

ondit

ions

Using

Dela

yed D

etach

ed-Ed

dy

Simula

tion

A. Lo

fthou

se, R

. Cum

ming

s, U.

S. Ai

r Forc

e Ac

adem

y, Co

lorad

o Spri

ngs,

CO

1130

hrs

AIAA-2

015-2

876

A Sy

nthe

sis of

Hyb

rid CF

D Re

sults

fo

r F-1

6XL A

ircra

ft Ae

rody

nami

csJ.

Luck

ring,

NASA

Lang

ley Re

searc

h Ce

nter, H

ampto

n, VA

Wedn

esda

y, 24

June

201

516

1-AP

A-18

Aero

dyna

mic D

esign

Meth

odolo

gies I

ICa

rpen

ter B

allro

omCh

aired

by: J

. LAT

Z, No

rthrop

Grum

man A

erosp

ace S

ystem

s and

D. F

INLE

Y, Lo

ckhe

ed M

artin

Aeron

autic

s09

00 hr

sAIA

A-201

5-287

7Im

prov

emen

ts in

the N

ew U

nstea

dy

Far-F

ield D

rag B

reak

down

Meth

od

and A

pplic

ation

to Co

mplex

Case

sH.

Toub

in, D

. Bail

ly, M

. Cos

tes, O

NERA

, Me

udon

, Fran

ce

0930

hrs

AIAA-2

015-2

878

Aero

dyna

mic s

hape

optim

izatio

n of

BW

B air

craft

base

d on

multiz

one

colla

bora

tive o

ptim

izatio

n de

sign

meth

odZ.

Gao,

K. Zh

ao, C

. Wan

g, No

rthwe

stern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

1000

hrs

AIAA-2

015-2

879

Desig

n of

A H

igh-P

erfo

rman

ce

Taille

ss MA

V Thr

ough

Plan

form

Op

timiza

tion

M. B

ronz,

G. H

atten

berge

r, Fren

ch Ci

vil

Aviat

ion U

nivers

ity, T

oulou

se, F

rance

1030

hrs

AIAA-2

015-2

880

Aero

dyna

mic O

ptimi

zatio

n of

Integ

rated

Wing

-Engin

e Geo

metry

us

ing an

Uns

tructu

red Vo

rticit

y Solv

erL.

King,

R. Ha

rtfield

, Aub

urn Un

iversit

y, Au

burn,

AL; V

. Ahu

ja, Re

search

in Fl

ight,

Aubu

rn, AL

Wedn

esda

y, 24

June

201

516

2-AP

A-19

Prop

eller

/Rot

orcra

ft/Wi

nd Tu

rbine

Aer

odyn

amics

IISte

mmon

s BCh

aired

by: J

. FAR

NSW

ORTH

, Univ

ersity

of Co

lorad

o Bou

lder a

nd M

. POS

T, US

AF Ac

adem

y09

00 hr

sAIA

A-201

5-288

1De

velop

ment

of U

GS M

onoc

opter

: Pla

tform

Des

ign an

d Tra

jecto

ry

Track

ingS.

Srig

rarom

, K. L

ee, S

. Chn

g, M.

Bin

Abdu

l Mali

k, Un

iversi

ty of

Glasg

ow,

Glasg

ow, U

nited

King

dom

0930

hrs

AIAA-2

015-2

882

A stu

dy of

sepa

ratio

n on

airfo

ils

unde

rgoin

g pitc

h, su

rge a

nd

comb

ined m

otion

sR.

Dunn

e, B.

McK

eon,

Califo

rnia I

nstitu

te of

Tech

nolog

y, Pa

sade

na, C

A

1000

hrs

AIAA-2

015-2

883

Comp

utat

ional

Inve

stiga

tion

of Co

axial

Rot

or In

terac

tiona

l Ae

rody

nami

cs in

Stead

y For

ward

Fli

ght

B. Pa

sse, A

. Srid

haran

, J. B

aede

r, Un

iversi

ty of

Maryl

and,

Colle

ge Pa

rk,

Colle

ge Pa

rk, M

D

1030

hrs

AIAA-2

015-2

884

Comp

utatio

nal In

vesti

gatio

ns

of Tra

nsien

t Loa

ds an

d Blad

e De

forma

tions

on Co

axial

Rotor

Sy

stems

R. Sin

gh, H

. Kan

g, Arm

y Rese

arch L

abora

tory,

Aberd

een P

roving

Grou

nd, M

D; J.

Siroh

i, Un

iversit

y of T

exas,

Austin

, Aust

in, TX

1100

hrs

AIAA-2

015-2

885

Roto

r Dyn

amic

Wake

Inflo

w Mo

dellin

g in

State-

Spac

e For

mat

M. G

enna

retti,

R. Go

ri, J.

Serafi

ni, G

. Be

rnardi

ni, F.

Cardi

to, Ro

ma Tr

e Univ

ersity

, Ro

me, I

taly

1130

hrs

AIAA-2

015-2

886

Valid

ation

of In

stalla

tion

Effe

ct Pr

edict

ions t

hrou

gh Si

mulat

ions

of Co

ntra

-Rot

ating

Ope

n Ro

tors

at

Low-

Spee

d Flig

ht Co

nditio

nsA.

Stue

rmer,

Germ

an Ae

rospa

ce Ce

nter

(DLR

), Br

auns

chwe

ig, G

erman

y

1200

hrs

AIAA-2

015-2

887

A Ne

w Wh

irl Fl

utter

Ana

lysis

Meth

odY.

Yang

, G. H

uang

, D. Z

hao,

C. Ta

ng,

Aviat

ion In

dustr

y Corp

oratio

n of C

hina

(AVIC

), Xi’

an, C

hina

Wedn

esda

y, 24

June

201

516

3-AS

E-1Nu

meric

al We

athe

r Pre

dictio

n (In

vited

)Plu

m Bl

osso

m B

Chair

ed by

: N. A

HMAD

, NAS

A Lan

gley R

esea

rch Ce

nter a

nd D

. GHO

SH09

00 hr

sAIA

A-201

5-288

8Ch

allen

ges a

nd O

ppor

tunit

ies in

Mod

eling

of th

e Glob

al At

mosp

here

Z. Ja

njic,

Natio

nal O

cean

ic an

d Atm

osph

eric A

dmini

strati

on, C

olleg

e Park

, MD

1000

hrs

AIAA-2

015-2

889

Well-

Balan

ced F

ormu

lation

of

Grav

itatio

nal S

ource

Term

s for

Co

nser

vativ

e Fini

te-Di

ffere

nce

Atmo

sphe

ric Fl

ow So

lvers

D. G

hosh

, E. C

onsta

ntine

scu, A

rgonn

e Na

tiona

l Lab

orator

y, Le

mont,

IL

1030

hrs

AIAA-2

015-2

890

Use o

f Num

erica

l Wea

ther

Pr

edict

ion M

odels

for N

extG

en AT

C Wi

nd Im

pact

Studie

s (In

vited

)S.

Trox

el, T.

Reyn

olds,

Linco

ln La

borat

ory,

Massa

chus

etts I

nstitu

te of

Tech

nolog

y, Le

xingto

n, MA

1100

hrs

AIAA-2

015-2

891

Simula

tions

of or

ogra

phic fl

ows u

sing

unstr

uctur

ed an

d stru

ctured

mesh

es

(Invit

ed)

J. Sz

melte

r, Lou

ghbo

rough

Unive

rsity,

Loug

hboro

ugh,

Unite

d King

dom;

P.

Smola

rkiew

icz, E

urope

an Ce

ntre f

or Me

dium-

Rang

e Fore

castin

g, Re

ading

, Unit

ed Ki

ngdo

m;

A. Wy

szogro

dzki,

Nati

onal

Resea

rch In

stitute

, Wa

rsaw,

Polan

d

82

Wedn

esda

y, 24

June

201

516

4-AT

IO-1

5AT

M III

- Mo

delin

g in

ATM

Metro

polita

n Ba

llroo

mCh

aired

by: S

. LAN

DRY,

Purdu

e Univ

ersity

0900

hrs

AIAA-2

015-2

892

A Sy

stem

Dyna

mics

Appr

oach

to

ward

s ANS

P Mo

delin

gM.

Kreu

z, M.

Sch

ultz,

Germ

an Ae

rospa

ce

Cente

r (DL

R), B

rauns

chwe

ig, G

erman

y

0930

hrs

AIAA-2

015-2

893

Mode

ling A

ppro

ach f

or Re

silien

ce

Engin

eerin

g of t

he Fu

ture A

TM Sy

stem

R. Pa

lumbo

, A. E

rrico,

D. Pa

scarel

la, F.

Ga

rgiulo

, E. F

ilippo

ne, I

talian

Aeros

pace

Re

searc

h Cen

ter (C

IRA),

Capu

a, Ita

ly

1000

hrs

AIAA-2

015-2

894

Risk

-bas

ed Ca

usal

Mode

ling o

f Ai

rbor

ne Lo

ss of

Sepa

ratio

nS.

Geu

ther, A

. Shih

, NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA

1030

hrs

AIAA-2

015-2

895

A Da

ta-D

riven

Qua

ntita

tive

Fram

ewor

k fo

r Saf

ety A

ssessm

ent

of A

ir Tra

ffic C

ontro

l Sys

temA.

Oztek

in, H

i-Tec S

ystem

s, Inc

., Eg

g Ha

rbor T

wp, N

J

1100

hrs

AIAA-2

015-2

896

Asse

ssing

Air

Traffi

c Con

trol S

ystem

Sa

fety

with

Syste

m Co

ntro

llabil

ityJ.

Guo,

K. Ma

rais,

S. La

ndry,

Purdu

e Un

iversi

ty, W

est L

afaye

tte, I

N

Wedn

esda

y, 24

June

201

516

5-AT

IO-1

6Tra

nsfo

rmat

ional

Fligh

t - A

uton

omy I

Mone

t Ball

room

Chair

ed by

: B. A

LLEN,

NAS

A Lan

gley R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-2

897

Who’s

got t

he br

idge?

Towa

rds

Safe

, Rob

ust A

uton

omou

s Op

erat

ions -

“Dat

a, yo

u’ve

got

the b

ridge

.” - F

irst O

ffice

r Tho

mas

“Will”

Rike

r Sta

r Tre

k: Th

e Nex

t Ge

nera

tion:

: Com

ing of

Age

(198

8)B.

Allen

, C. C

ross,

H. Fa

n, W.

Fehlm

an,

L. He

mpley

, M. M

otter,

NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA; e

t al.

0930

hrs

AIAA-2

015-2

898

Towa

rds a

n Op

en, D

istrib

uted

So

ftwar

e Arch

itectu

re fo

r UxS

Op

erat

ions -

“It’s

diffi

cult

to

work

in gr

oups

whe

n yo

u’re

om

nipot

ent,”

- Q

Star T

rek:

The

Next

Gen

erat

ion::

Deja

Q (1

990)

C. Cro

ss, H

. Fan

, W. F

ehlm

an, L

. Hem

pley,

M. M

otter,

J. N

eilan

, NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA; e

t al.

1000

hrs

AIAA-2

015-2

899

Reinf

orce

ment

Lear

ning w

ith

Auto

nomo

us Sm

all U

nman

ned

Aeria

l Veh

icles

in Cl

utter

ed

Envir

onme

nts -

“Afte

r all t

hese

ye

ars a

mong

hum

ans,

you

still

have

n’t l

earn

ed to

smile

.”L.

Tran,

C. Cro

ss, M

. Mott

er, J.

Neil

an,

G. Q

ualls,

P. Ro

thhaa

r, NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA; e

t al.

1030

hrs

Oral

Prese

ntatio

n“H

is ac

tions

indic

ate t

wo-

dimen

siona

l thin

king”

- De

ciding

to

Go A

roun

d via

Mach

ine Le

arnin

gM.

Mott

er, J.

High

, C. C

ross,

H. Fa

n, W.

Fehlm

an, L

. Hem

pley,

NASA

Lang

ley

Rese

arch C

enter

, Ham

pton,

VA; e

t al.

Wedn

esda

y, 24

June

201

516

6-AT

IO-1

7Hu

man

Facto

rs in

Aviat

ion O

pera

tions

Milan

Chair

ed by

: L. B

OWER

S, Pu

rdue U

nivers

ity09

00 hr

sAIA

A-201

5-290

0A

Mode

l for

Situ

ation

al Aw

aren

ess

in Ai

rcraf

t Ups

et Pr

even

tion

and

Reco

very

K. Sc

hlimm

, Avia

tion P

erform

ance

So

lution

s, LLC

, Mes

a, AZ

0930

hrs

AIAA-2

015-2

901

Analy

sis of

Eye-

Track

ing D

ata w

ith

Rega

rds t

o the

Comp

lexity

of Fl

ight

Deck

Info

rmat

ion A

utom

ation

an

d Man

agem

ent -

Inat

tentio

nal

Blind

ness,

Syste

m Sta

te Aw

aren

ess,

and E

FB U

sage

E. Dil

l, S. Y

oung

, NAS

A Lan

gley R

esea

rch

Cente

r, Ham

pton,

VA

1000

hrs

AIAA-2

015-2

902

Thre

at an

d Erro

r Man

agem

ent

Appli

ed to

Loss

of Co

ntro

l - In

fligh

tD.

Carro

ll, Av

iation

Perfo

rman

ce S

olutio

ns,

LLC, M

esa,

AZ

1030

hrs

AIAA-2

015-2

903

Evalu

ating

Inten

sity a

s a N

extG

en

Cont

rolle

r Fun

ction

for I

ncre

ased

Tra

ffic S

cena

rios

C. Su

rakitb

anha

rn, S

. Lan

dry, P

urdue

Un

iversi

ty, W

est L

afaye

tte, I

N

1100

hrs

AIAA-2

015-2

904

A Co

mpar

ison

of an

Inten

sity

Cont

rol M

easu

re Ve

rsus D

ynam

ic De

nsity

to Ca

ptur

e Com

plexit

y Wi

thin

a Sec

tor

C. Su

rakitb

anha

rn, C.

Sura

kitba

nharn

, S.

Land

ry, Pu

rdue U

nivers

ity, W

est

Lafay

ette,

IN

1130

hrs

AIAA-2

015-2

905

Tacti

le Fe

edba

ck an

d Situ

ation

Aw

aren

ess -

Impr

oving

Adh

eren

ce

to an

Enve

lope i

n Sid

estic

k-Co

ntro

lled F

ly-by

-Wire

Airc

rafts

F. Sc

hmidt

-Skipi

ol, Te

chnic

al Un

iversi

ty of

Brau

nsch

weig,

Brau

nsch

weig,

Germ

any

1200

hrs

AIAA-2

015-2

906

Mode

ling t

he A

ir Tra

ffic C

ontro

ller’s

Di

rect-

to O

pera

tion

Using

Logis

tic

Regr

essio

nS.

Hon

g, S.

Jung

, K. L

ee, K

orea A

erosp

ace

Unive

rsity,

Goy

ang,

South

Korea

Wedn

esda

y, 24

June

201

516

7-BA

L-1Ba

lloon

Syste

ms I

Steub

enCh

aired

by: J

. NOT

T, No

tt Te

chno

logy L

LC09

00 hr

sAIA

A-201

5-290

7Th

e NAS

A Ba

lloon

Pro

gram

- Po

sition

ing Fo

r the

Futu

reD.

Fairb

rothe

r, NAS

A God

dard

Spac

e Flig

ht Ce

nter, G

reenb

elt, M

D

0930

hrs

AIAA-2

015-2

908

The F

renc

h ba

lloon

prog

ram

2013

- 2

015

A. Va

rgas,

V. Du

bourg

, D. V

assa

ux, F

rench

Sp

ace A

genc

y (CN

ES),

Toulo

use,

Franc

e

1000

hrs

Oral

Prese

ntatio

nBa

lloon

Syste

ms A

pplic

ation

T. Ge

rber, A

pplie

d Tec

hnolo

gy As

socia

tes,

Albuq

uerqu

e, NM

1030

hrs

AIAA-2

015-2

909

Quali

ficat

ion of

the N

ASA

Supe

r Pr

essu

re B

alloo

nH.

Cathe

y, Ne

w Me

xico S

tate U

nivers

ity,

Wallo

ps Is

land,

VA; J

. Tutt

le, D

. Fa

irbrot

her, M

. Said

, NAS

A God

dard

Spac

e Fli

ght C

enter

, Wall

ops I

sland

, VA

1100

hrs

AIAA-2

015-2

910

Non-

Linea

r Ana

lysis

of th

e NA

SA Su

per P

ressu

re B

alloo

ns:

Imple

ment

ation

of a

Larg

e Stra

in Ma

terial

Mod

elA.

Bown

, D. W

akefi

eld, T

ensy

s Dyn

amics

, Ltd

., Ba

th, U

nited

King

dom

1130

hrs

AIAA-2

015-2

911

Retu

rning

to H

ydro

gen

Gas :

a Str

ateg

ic De

cision

to Co

ntinu

e Ac

hieve

ment

of St

rato

sphe

ric

Ballo

ons F

light

sJ.

Gary,

Fren

ch S

pace

Agen

cy (C

NES)

, Air

e sur

l’Ado

ur, Fr

ance

; B. D

ellery

, G.

Letre

nne,

S. Ve

nel, A

. Varg

as, F

rench

Sp

ace A

genc

y (CN

ES),

Toulo

use,

Franc

e

1200

hrs

AIAA-2

015-2

912

Suita

bility

of A

DS-B

as a

Beac

on

for S

trato

sphe

ric B

alloo

n Pla

tform

s an

d Pay

loads

T. La

chen

meier

, R. D

ewey

, Nea

r Spa

ce

Corpo

ration

, Tilla

mook

, OR

83

Wedn

esda

y, 24

June

201

516

8-CA

SE-6

09

00 -

1230

hrs

CASE

Sessi

on II

& II

IGr

and B

allro

om D

0900

-1045

hrs

Integ

ration

and T

est

This

pane

l focu

ses o

n the

Integ

ration

& Te

st ph

ase o

f dev

elopm

ent.

Plann

ing fo

r integ

ration

activ

ities o

f com

plex s

ystem

s is i

nhere

ntly d

ifferen

t from

trad

itiona

l sys

tems e

ngine

ering

integ

ration

plan

ning a

ctivit

ies. D

ecisio

ns ab

out t

he sy

stems

unde

r dev

elopm

ent h

ave t

o con

sider

not o

nly th

e tec

hnica

l and

prog

ramma

tic vi

ewpo

ints b

ut als

o the

politi

cal, s

ociet

al, op

eratio

nal, a

nd ec

onom

ic vie

wpoin

ts. D

efinit

ion of

perfo

rman

ce m

easu

res, f

ound

intrin

sic in

the p

lan, w

ith tr

ans-d

iscipl

inary

impli

catio

ns w

ill be

discu

ssed.

A sce

nario

for in

tegrat

ion of

UAS

in th

e NA

S wi

ll be u

sed a

s a be

nchm

ark fo

r curr

ent v

iews a

nd lif

e cyc

le ch

allen

ges.

Sessi

on Ch

airs:

Mat F

rench

, Elec

trical

Syste

ms En

ginee

r, Roll

s-Roy

ce Co

rporat

ion, H

ernan

do Ji

mine

z, Re

searc

h Eng

ineer

II at A

erosp

ace S

ystem

s Des

ign La

borat

ory, G

eorgi

a Ins

titute

of Te

chno

logy a

nd D

avid

Loda

, Exe

cutiv

e Dire

ctor, N

CPS

Rese

arch,

LLC

Pan

elists

:Jim

Mur

phy

Projec

t Eng

ineer

for In

tegrat

ed Te

st an

d Eva

luatio

n for

the U

nman

ned A

ircraf

t Sys

tem In

tegrat

ionNA

SA Am

es Re

searc

h Cen

ter

David

Mar

oney

Princ

ipal S

ystem

s Eng

ineer

The M

itre Co

rporat

ion

1045

-1230

hrs

Entr y

into

Servi

ce/E

nd of

Life

This

pane

l focu

ses o

n the

comp

lexitie

s tha

t aris

e onc

e a sy

stem

enter

s serv

ice th

rough

out t

he lif

e of t

he sy

stem.

If th

ese c

omple

xities

are c

onsid

ered a

nd in

corpo

rated

into

the sy

stem

deve

lopme

nt ph

ase,

more

robus

t prod

ucts

can b

e dev

elope

d and

high

er cu

stome

r sati

sfacti

on

can b

e ach

ieved

.Se

ssion

Chair

: Jeff

Jeps

on, S

enior

Sys

tems E

ngine

er GN

C / G

uidan

ce D

esign

& Pe

rform

ance

, Ray

theon

Miss

ile S

ystem

s

Pan

elists

:Tim

Ada

maCh

ief En

ginee

r of F

actor

iesRa

ytheo

n Miss

ile S

ystem

s

Ed D

olans

kiPre

siden

t and

CEO

Avial

l

Jim G

allag

her

EIS Pr

ogram

Man

ager

Gulfs

tream

Aeros

pace

Corpo

ration

Wedn

esda

y, 24

June

201

516

9-CF

D-17

Adva

nces

in H

igh-O

rder

Meth

ods

Gran

d Ball

room

ACh

aired

by: D

. ZIN

GG, U

nivers

ity of

Toron

to an

d P. R

OE, U

nivers

ity of

Mich

igan

0900

hrs

AIAA-2

015-2

913

New

Appr

oach

es to

Limi

ting

P. Ro

e, T.

Lung

, J. M

aeng

, Univ

ersity

of

Mich

igan,

Ann A

rbor, A

nn Ar

bor, M

I

0930

hrs

AIAA-2

015-2

914

New

Diag

onal-

Norm

Summ

ation

-by

-Par

ts Op

erat

ors f

or th

e Firs

t De

rivat

ive w

ith In

creas

ed O

rder

of

Accu

racy

D. D

el Re

y Fern

ánde

z, D.

Zing

g, Un

iversi

ty of

Toron

to, To

ronto,

Cana

da

1000

hrs

AIAA-2

015-2

915

Deve

lopme

nt of

Gen

erali

zed

Summ

ation

-by-

Parts

Ope

rato

rs fo

r th

e Sec

ond D

eriva

tive w

ith Va

riable

Co

effic

ients

D. D

el Re

y Fern

ánde

z, D.

Zing

g, Un

iversi

ty of

Toron

to, To

ronto,

Cana

da

1030

hrs

AIAA-2

015-2

916

A Fini

te Di

fferen

ce WE

NO Sc

heme

Ma

intain

ing Ve

locity

, Pres

sure

an

d Tem

pera

ture E

quilib

rium

in Mu

lticom

pone

nt Co

mpres

sible

Fluid

Analy

sisT.

Nono

mura,

Japa

n Aero

space

Explo

ration

Ag

ency

(JAXA

), Sa

gami

hara,

Japa

n; D.

Ter

akad

o, Un

iversit

y of T

okyo

, Sag

amiha

ra,

Japan

; K. F

ujii, J

apan

Aeros

pace

Explo

ration

Ag

ency

(JAXA

), Sa

gami

hara,

Japa

n

Wedn

esda

y, 24

June

201

517

0-CF

D-18

Curre

nt Tr

ends

in CF

D Re

sear

ch I

(Invit

ed)

Gran

d Ball

room

BCh

aired

by: H

. HUY

NH, N

ASA G

lenn R

esea

rch Ce

nter a

nd Z.

WAN

G, U

nivers

ity of

Kans

as09

00 hr

sOr

al Pre

senta

tion

Comp

ariso

n of O

utput

Error

Estim

ation

for

Finit

e Elem

ent D

iscret

izatio

ns of

Co

nvect

ion-do

mina

ted Fl

ows (

Invite

d)H.

Carso

n, S.

Allma

ras, M

. Galb

raith,

D.

Darm

ofal, M

assach

usetts

Instit

ute of

Tec

hnolo

gy, Ca

mbrid

ge, M

A

0930

hrs

Oral

Prese

ntatio

nNo

vel A

dapt

ive M

echa

nics f

or H

igh-

Orde

r Uns

tructu

red C

FD (I

nvite

d)K.

Fidko

wski,

Univ

ersity

of M

ichiga

n, An

n Arb

or, An

n Arbo

r, MI

1000

hrs

AIAA-2

015-2

917

Inve

stiga

tion

of U

nstru

cture

d Hi

gher

-Ord

er M

ethod

s for

Uns

teady

flo

w an

d Mov

ing D

omain

sJ.

Newm

an, W

. And

erson

, Univ

ersity

of

Tenn

esse

e, Ch

attan

ooga

, Cha

ttano

oga,

TN

1030

hrs

Oral

Prese

ntatio

nHi

gh-o

rder

Disc

ontin

uous

Gale

rkin

Simula

tions

on D

omain

s with

Larg

e De

form

ation

s (In

vited

)P.

Perss

on, U

nivers

ity of

Califo

rnia,

Berke

ley, B

erkele

y, CA

1100

hrs

Oral

Prese

ntatio

nPr

obing

Comp

lex U

nstea

dy Fl

ow

Phys

ics U

sing a

High

-Fide

lity

Comp

utat

ional

Fram

ewor

k (In

vited

)M.

Visb

al, Ai

r Forc

e Res

earch

Labo

ratory

, W

right-

Patte

rson A

FB, O

H

84

Wedn

esda

y, 24

June

201

517

1-CF

D-19

LES,

DNS,

and H

ybrid

RAN

S-LE

S III

Cora

lCh

aired

by: J

. BAE

DER,

Unive

rsity

of Ma

rylan

d and

C. G

ROTH

, Univ

ersity

of To

ronto

0900

hrs

AIAA-2

015-2

918

Aero

dyna

mic C

hara

cteris

tics o

f SC

1095

Airfo

il usin

g Hyb

rid RA

NS-LE

S Me

thods

Imple

mente

d into

a GP

U Ac

celera

ted N

avier

-Stok

es So

lver

N. Ja

in, J.

Baed

er, Un

iversit

y of M

arylan

d, Co

llege P

ark, C

ollege

Park,

MD

0930

hrs

AIAA-2

015-2

919

Appli

catio

ns of

the i

ntegr

al Wa

ll Mod

el in

LES o

f flow

over

surfa

ces in

cludin

g res

olved

and s

ubgr

id ro

ughn

essX.

Yang

, J. S

adiqu

e, C.

Mene

veau

, R. M

ittal,

Johns

Hopk

ins Un

iversit

y, Ba

ltimore

, MD

1000

hrs

AIAA-2

015-2

920

An Em

bedd

ed LE

S-RA

NS So

lver f

or

Aero

dyna

mic S

imula

tions

K. An

upind

i, R. S

andb

erg, U

nivers

ity of

So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1030

hrs

AIAA-2

015-2

921

Asse

ssmen

t of H

ybrid

RAN

S/LE

S Me

thods

For G

as-Tu

rbine

Comb

ustor

-Re

levan

t Tur

bulen

t Flow

sJ.

West,

C. Gr

oth, U

nivers

ity of

Toron

to,

Toron

to, Ca

nada

; J. H

u, Pra

tt & W

hitne

y, Mi

ssissa

uga,

Cana

da

Wedn

esda

y, 24

June

201

517

2-CF

D-20

Turb

ulenc

e Mod

el Va

lidat

ion (I

nvite

d)Em

erald

Chair

ed by

: C. R

UMSE

Y, NA

SA-La

ngley

Rese

arch C

enter

and B

. SMI

TH, L

ockh

eed M

artin

Aeron

autic

s09

00 hr

sAIA

A-201

5-292

2Mo

difica

tion

of th

e k-k

l Two

Eq

uatio

n Tu

rbule

nce M

odel

for

Impr

oved

Jet F

low P

redic

tions

(In

vited

)B.

Smi

th, Lo

ckhe

ed M

artin

Corpo

ration

, Fo

rt Wo

rth, T

X

0930

hrs

AIAA-2

015-2

923

LagR

ST M

odel

Pred

iction

s of a

Wi

ngtip

Vorte

x Flo

wfield

(Inv

ited)

M. O

lsen,

NASA

Ames

Rese

arch C

enter

, Mo

ffett

Field,

CA; R

. Lilla

rd, N

ASA J

ohns

on

Spac

e Cen

ter, H

ousto

n, TX

; T. C

oakle

y, NA

SA Am

es Re

searc

h Cen

ter, M

offett

Fie

ld, CA

1000

hrs

AIAA-2

015-2

924

Seco

nd-M

omen

t RAN

S Mod

el Ve

rifica

tion a

nd Va

lidati

on us

ing th

e Tu

rbule

nce M

odeli

ng Re

sour

ce We

bsite

(In

vited

)B.

Eisfel

d, Ge

rman

Aeros

pace

Cente

r (DL

R),

Braun

schwe

ig, Ge

rman

y; C.

Rums

ey, N

ASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA

1030

hrs

AIAA-2

015-2

925

Asse

ssmen

t of g

-Equa

tion

Form

ulatio

n fo

r a Se

cond

-Mom

ent

Reyn

olds S

tress

Turb

ulenc

e Mod

el (In

vited

)V.

Togit

i, B. E

isfeld

, Germ

an Ae

rospa

ce

Cente

r (DL

R), B

rauns

chwe

ig, G

erman

y

1100

hrs

AIAA-2

015-2

926

Appli

catio

n of

an El

liptic

Blen

ding

Reyn

olds S

tress

Mode

l in A

ttach

ed

and S

epar

ated

flow

s (In

vited

)M.

Stoe

llinge

r, R. R

oy, U

nivers

ity of

W

yomi

ng, L

arami

e, La

ramie,

WY;

N. As

hton,

Unive

rsity

of Ma

nche

ster,

Manc

heste

r, Unit

ed Ki

ngdo

m

1130

hrs

AIAA-2

015-2

927

Rece

nt D

evelo

pmen

ts on

the

Turb

ulenc

e Mod

eling

Res

ource

We

bsite

(Inv

ited)

C. Ru

msey

, NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

Wedn

esda

y, 24

June

201

517

3-FD

-19

Turb

omac

hiner

y - Tu

rbine

sSe

nato

rs Le

cture

Hall

Chair

ed by

: Z. R

USAK

, Ren

sselae

r Poly

techn

ic Ins

titute

and Q

. WAN

G, M

IT09

00 hr

sAIA

A-201

5-292

8Da

ta P

roce

ssing

Tech

nique

s for

Me

asur

emen

ts Co

llecte

d fro

m a S

ingle

Slant

ed H

ot-W

ire fo

r Tu

rbom

achin

ery A

pplic

ation

sR.

Berda

nier, N

. Key

, Purd

ue U

nivers

ity,

West

Lafay

ette,

IN

0930

hrs

AIAA-2

015-2

929

Flowfi

eld an

d Film

Per

form

ance

Me

asur

emen

ts of

Axia

l Sha

ped

Cooli

ng H

oles o

n a F

lat P

late

D. G

etsing

er, J.

Dee

s, G.

Rode

baug

h, Ge

neral

Elec

tric Co

mpan

y, Nis

kayu

na, N

Y

1000

hrs

AIAA-2

015-2

930

Visua

lizat

ion of

Seco

ndar

y Flow

Str

uctu

res C

ause

d by R

otat

ing

Insta

bility

: Syn

chro

nized

Ster

eo

High

-Spe

ed P

IV an

d Uns

teady

Pr

essu

re M

easu

reme

nts

B. Pa

rdowi

tz, G

erman

Aeros

pace

Cente

r (D

LR),

Berlin

, Germ

any;

J. Pe

ter, T

echn

ical

Unive

rsity

of Be

rlin, B

erlin,

Germ

any;

U.

Tapk

en, G

erman

Aeros

pace

Cente

r (DL

R),

Berlin

, Germ

any;

P. Th

amse

n, Te

chnic

al Un

iversi

ty of

Berlin

, Berl

in, G

erman

y; L.

Engh

ardt,

Germ

an Ae

rospa

ce Ce

nter

(DLR

), Be

rlin, G

erman

y

1030

hrs

AIAA-2

015-2

931

Desig

n Op

timiza

tion

of P

rofil

ed

Endw

all w

ith Co

nside

ratio

n of

Co

oling

and R

im Se

al Flo

w Ef

fects

H. Ta

ng, S

. Liu,

H. L

uo, A

viatio

n Ind

ustry

Co

rporat

ion of

China

(AVIC

), Sh

angh

ai,

China

85

Wedn

esda

y, 24

June

201

517

4-FD

-20

Shoc

k Wa

ve /

Bou

ndar

y Lay

er In

terac

tions

Edelw

eiss

Chair

ed by

: N. C

LEME

NS, T

he U

nivers

ity of

Texa

s at A

ustin

and D

. GAIT

ONDE

, The

Ohio

Stat

e Univ

ersity

0900

hrs

AIAA-2

015-2

932

Expe

rimen

tal I

nves

tigat

ion of

Un

stead

iness

of Sw

ept-R

amp

Shoc

k/Bo

unda

ry La

yer I

nter

actio

ns

at M

ach

2L.

Vans

tone,

M. S

aleem

, S. S

eckin

, N.

Cleme

ns, U

nivers

ity of

Texa

s, Au

stin,

Austi

n, TX

0930

hrs

AIAA-2

015-2

933

Effe

cts of

Swee

p on

Impin

ging

Obliq

ue Sh

ock-

Turb

ulent

Bou

ndar

y La

yer I

nter

actio

nR.

Daws

on, C

. Ped

erson

, J. L

ittle,

Unive

rsity

of Ari

zona

, Tuc

son,

Tucso

n, AZ

1000

hrs

AIAA-2

015-2

934

Expe

rimen

tal I

nves

tigat

ion of

sh

ock-

induc

ed co

rner

boun

dary

lay

er se

para

tion

A. He

gde,

V. Na

rayan

aswa

my, N

orth

Carol

ina S

tate U

nivers

ity, R

aleigh

, NC

1030

hrs

AIAA-2

015-2

935

Expe

rimen

tal an

d Num

erica

l Stud

y of

Shoc

k-Wav

e Bou

ndar

y Lay

er

Intera

ction

s on a

n Axis

ymme

tric B

ody

G. Ro

berts

on, R

. Kum

ar, Fl

orida

State

Un

iversit

y, Tal

lahass

ee, F

L; T.

Eyma

nn, S

. Mo

rton,

CREA

TE Ke

strel

Team,

Eglin

AFB,

FL

1100

hrs

AIAA-2

015-2

936

An Ex

perim

enta

l Inv

estig

ation

of

the E

ffect

of B

ound

ary L

ayer

on an

In

terna

l Com

pres

sion

Inlet

H. Ta

banli

, K. Y

uceil

, Ista

nbul

Tech

nical

Unive

rsity,

Istan

bul, T

urkey

Wedn

esda

y, 24

June

201

517

5-FD

-22

Unste

ady F

lows -

Cavit

y and

Shea

r Flow

sGo

veno

rs Le

cture

Hall

Chair

ed by

: K. C

ASPE

R and

K. G

RANL

UND,

Air F

orce R

esea

rch La

borat

ory09

00 hr

sAIA

A-201

5-293

7Re

lation

ship

betw

een

Acou

stic

Tone

s and

Flow

Stru

cture

in

Trans

onic

Recta

ngula

r Cav

ity Fl

owJ.

Wagn

er, K.

Casp

er, S

. Bere

sh, B

. Prue

tt,

R. Sp

illers,

J. H

enflin

g, Sa

ndia

Natio

nal

Labo

ratori

es, A

lbuqu

erque

, NM

0930

hrs

AIAA-2

015-2

938

Moda

l Dec

ompo

sition

of P

ressu

re

Data

in Ca

vity F

lows

K. Ca

sper,

S. A

runaja

tesan

, San

dia

Natio

nal L

abora

tories

, Albu

querq

ue, N

M

1000

hrs

AIAA-2

015-2

939

Comp

ariso

n of H

igh-O

rder

and

Low-

Orde

r Meth

ods f

or La

rge-E

ddy

Simula

tion o

f a Co

mpres

sible

Shea

r La

yer

M. M

ankb

adi, J

. DeB

onis,

N. Ge

orgiad

is, NA

SA Gl

enn R

esearc

h Cen

ter, C

levela

nd, O

H

1030

hrs

AIAA-2

015-2

940

Redu

ced O

rder

Mod

eling

of

a Diel

ectri

c Bar

rier D

ischa

rge

Cont

rolle

d She

ar La

yer u

sing

Minim

um B

asis

Rota

tions

J. Ch

abot,

E. Ca

raball

o, Mi

ami U

nivers

ity,

Oxfor

d, OH

; J. L

ittle,

Unive

rsity

of Ari

zona

, Tu

cson,

Tucso

n, AZ

1100

hrs

AIAA-2

015-2

941

Shea

r-Thin

ning P

rope

rties

of B

lood

in La

rge A

rterie

sF.

Kok,

R. My

ose,

K. Ho

ffman

n, W

ichita

St

ate U

nivers

ity, W

ichita

, KS

Wedn

esda

y, 24

June

201

517

6-MA

O-5

Emer

ging M

ethod

s IMa

drid

Chair

ed by

: E. W

INER

, Iow

a Stat

e Univ

ersity

and V

. LI,

Boein

g Eng

ineeri

ng O

perat

ions &

Tech

nolog

y09

00 hr

sAIA

A-201

5-294

2Mu

ltidisc

iplina

ry D

esign

Spac

e Ex

plora

tion

Using

Add

itive

Manu

factu

ring a

nd R

apid

Prot

otyp

e Te

sting

A. Fri

edma

n, P.

Raj, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA

; E. A

lyana

k, Air

Force

Rese

arch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH

0930

hrs

AIAA-2

015-2

943

Arno

ldi-b

ased

Samp

ling f

or H

igh-

dimen

siona

l Opt

imiza

tion

using

Im

perfe

ct Da

taJ.

Hicke

n, A.

Ashle

y, Re

nsse

laer

Polyt

echn

ic Ins

titute,

Troy

, NY

1000

hrs

AIAA-2

015-2

944

Multi-

Doma

in Di

versi

ty

Pres

erva

tion

to M

itigat

e Par

ticle

Stagn

ation

and E

nable

Bett

er

Pare

to Co

vera

ge in

Mixe

d-Di

screte

Pa

rticle

Swar

m Op

timiza

tion

W. To

ng, S

yracu

se U

nivers

ity, S

yracu

se,

NY; S

. Cho

wdhu

ry, A.

Mes

sac,

Missi

ssipp

i St

ate U

nivers

ity, M

ississ

ippi S

tate,

MS

1030

hrs

AIAA-2

015-2

945

An M

DO ad

visor

y sys

tem su

ppor

ted

by k

nowl

edge

-bas

ed te

chno

logies

M. H

oogre

ef, G

. La R

occa

, Delf

t Univ

ersity

of

Tech

nolog

y, De

lft, Th

e Neth

erlan

ds

Wedn

esda

y, 24

June

201

517

7-MS

T-7Fli

ght S

imula

tion

Trave

rtine

Chair

ed by

: K. B

ILIMO

RIA09

00 hr

sAIA

A-201

5-294

6Mo

tion

Para

meter

Selec

tion

for

Fligh

t Sim

ulato

rsK.

Bilim

oria,

S. Re

ardon

, NAS

A Ame

s Re

searc

h Cen

ter, M

offett

Field

, CA

0930

hrs

AIAA-2

015-2

947

AVES

SDK:

Brid

ging t

he G

ap

betw

een

Simula

tor a

nd Fl

ight

Syste

ms D

esign

erT.

Gerla

ch, U

. Dura

k, Ge

rman

Aeros

pace

Ce

nter (

DLR)

, Brau

nsch

weig,

Germ

any

1000

hrs

AIAA-2

015-2

948

Mode

l-Bas

ed Te

sting

for O

bjecti

ve

Fideli

ty Ev

aluat

ion of

Engin

eerin

g an

d Res

earch

Fligh

t Sim

ulato

rsU.

Dura

k, Ge

rman

Aeros

pace

Cente

r (D

LR),

Brau

nsch

weig,

Germ

any;

A. Sc

hmidt

, T. P

awlet

ta, U

nivers

ity of

W

ismar,

Wism

ar, G

erman

y

86

Wedn

esda

y, 24

June

201

517

8-MS

T-8Co

mput

ation

al Me

thod

s for

Fluid

Dyn

amics

and H

eat T

rans

fer S

imula

tions

Wyeth

Chair

ed by

: M. K

OKAL

Y an

d B. J

AFFR

EZIC

0900

hrs

AIAA-2

015-2

949

Aero

dyna

mics

Fligh

t Mec

hanic

s Ap

proa

ch on

Comp

act D

omain

s for

Ai

r Veh

icle S

epar

ation

B. Ja

ffrez

ic, M

. Rue

tten,

H. Ro

sema

nn,

Germ

an Ae

rospa

ce Ce

nter (

DLR)

, Gö

ttinge

n, Ge

rman

y

0930

hrs

AIAA-2

015-2

950

Inve

stiga

tion

of th

e effe

ct of

grid

size o

n ex

terna

l sto

re se

para

tion

trajec

tory

usin

g CFD

A. Os

man,

A. Aly

, Cair

o Univ

ersity

, Cair

o, Eg

ypt;

I. El

baial

y, Qa

tar U

nivers

ity, D

oha,

Qatar

; O. A

bdell

atif,

Banh

a Univ

ersity

, Ca

iro, E

gypt;

E. Kh

alil, C

airo U

nivers

ity,

Cairo

, Egy

pt

1000

hrs

AIAA-2

015-2

951

Stren

gth An

alysis

and O

ptimi

zatio

n Tec

hniqu

e for

Therm

al Pr

otecti

on

Syste

m us

ing 3

Dime

nsion

al Ele

ment

Mode

lW.

Yan,

Aviat

ion In

dustr

y Corp

oratio

n of

China

(AVIC

), Be

ijing,

China

; X. L

uo, A

viatio

n Ind

ustry

Corpo

ration

of Ch

ina (A

VIC),

Chen

gdu,

China

; D. C

ui, Av

iation

Indu

stry

Corpo

ration

of Ch

ina (A

VIC),

Beijin

g, Ch

ina

1030

hrs

AIAA-2

015-2

952

Ther

mal s

imula

tion

and

expe

rimen

ts fo

r a st

rato

sphe

ric

ballo

on go

ndola

Q. Li

u, Ch

inese

Acad

emy o

f Scie

nces

, Be

ijing,

China

; Z. L

i, Y. Y

ang,

J. Ca

i, Ac

adem

y of O

pto-El

ectro

nics,

Chine

se

Acad

emy o

f Scie

nces

, Beij

ing, C

hina

1100

hrs

AIAA-2

015-2

953

Real

Time M

ultipl

e Fide

lity P

hysic

s Ba

sed S

imula

tion

of A

ircra

ft En

viron

ment

al Co

ntro

l Sys

temB.

Sas

anap

uri, A

NSYS

, Inc

., Pu

ne, I

ndia

Wedn

esda

y, 24

June

201

517

9-NW

-6

0900

- 09

30 h

rsNe

twor

king C

offe

e Bre

akCh

antill

y Ball

room

East

Wedn

esda

y, 24

June

201

518

0-PD

L-8/A

PA-2

0Pla

sma A

erod

ynam

ics &

Flow

Cont

rol I

VSte

mmon

s CCh

aired

by: T

. DOU

VILLE

, TLG

Aeros

pace

, LLC

.09

00 hr

sAIA

A-201

5-295

4Pla

sma L

amina

r-Sep

arat

ion-

Bubb

le Co

ntro

l ove

r Airf

oil at

Low

Reyn

olds N

umbe

rsX.

Men

g, X.

Yan,

H. H

u, No

rthwe

stern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

; F.

Liu, S

. Luo

, Univ

ersity

of Ca

liforni

a, Irv

ine,

Irvine

, CA

0930

hrs

AIAA-2

015-2

955

Pres

sure

s ove

r a Co

nical

Fore

body

un

der R

epeti

tive N

anos

econ

d Puls

e SD

BD A

ctuat

ions

D. Zh

ang,

X. M

eng,

J. Wa

ng,

North

weste

rn Po

lytec

hnica

l Univ

ersity

, Xi’

an, C

hina;

F. Liu

, S. L

uo, U

nivers

ity of

Ca

liforni

a, Irv

ine, L

os An

geles

, CA

1000

hrs

AIAA-2

015-2

956

Starti

ng Fl

ow by

Rep

etitiv

e Na

nose

cond

Puls

ed D

BD A

ctuat

ion

at M

icros

econ

ds an

d Milli

seco

nds i

n Qu

iesce

nt A

irH.

Hu,

H. Li

, X. M

eng,

J. Wa

ng,

North

weste

rn Po

lytec

hnica

l Univ

ersity

, Xi’

an, C

hina;

F. Liu

, S. L

uo, U

nivers

ity of

Ca

liforni

a, Irv

ine, L

os An

geles

, CA

1030

hrs

AIAA-2

015-2

957

Multi-

Inpu

t Gen

etic A

lgorit

hm fo

r Ex

perim

enta

l Opt

imiza

tion

of th

e Re

atta

chme

nt D

owns

tream

of a

Back

ward

-Facin

g-Ste

p with

Surfa

ce

Plasm

a Actu

ator

N. B

enard

, Nati

onal

Cente

r for

Scien

tific

Rese

arch (

CNRS

), Fu

turos

cope

, Fran

ce; J

. Po

ns-Pr

at, J.

Peria

ux, G

. Bug

eda,

CIMNE

, Ba

rcelon

a, Sp

ain; J

. Bon

net,

E. Mo

reau,

Natio

nal C

enter

for S

cienti

fic Re

searc

h (C

NRS)

, Futu

rosco

pe, F

rance

1100

hrs

AIAA-2

015-2

958

The E

ffect

of P

lasma

Clou

ds on

Ae

rody

nami

c Per

form

ance

of

Subs

onic/

Supe

rsonic

Inlet

sD.

Mei,

Aviat

ion In

dustr

y Corp

oratio

n of

China

(AVIC

), Sh

enya

ng, C

hina;

Y. Fa

n, C.

Jiang

, Beih

ang U

nivers

ity, B

eijing

, Chin

a

Wedn

esda

y, 24

June

201

518

1-PD

L-9/T

P-8

Plasm

a Diag

nosti

cs II

Miro

Chair

ed by

: N. H

ARAD

A, Na

gaok

a Univ

ersity

of Te

chno

logy a

nd J.

BUR

T, Un

iversa

l Tec

hnolo

gy Co

rporat

ion09

00 hr

sAIA

A-201

5-295

9Pla

nar T

wo-P

hoto

n LIF

Me

asur

emen

ts of

Ato

mic S

pecie

s in

a High

-Temp

erat

ure I

nduc

tively

Co

uple

Plasm

a Env

ironm

ent

J. Me

yers,

D. F

letch

er, U

nivers

ity of

Ve

rmon

t, Bu

rlingto

n, Bu

rlingto

n, VT

0930

hrs

AIAA-2

015-2

960

Parti

cle Va

poriz

ation

Veloc

imetr

y fo

r LPG

Diff

usion

Flam

esL.

Tolom

elli, T

echn

ologic

al Ins

titute

of Ae

ronau

tics (

ITA),

São J

osé d

os Ca

mpos

, Br

azil

1000

hrs

AIAA-2

015-2

961

Inve

stiga

tion

of N

on-Eq

uilibr

ium

Nitro

gen

Plasm

asA.

Lutz,

D. F

letch

er, U

nivers

ity of

Verm

ont,

Burlin

gton,

Burlin

gton,

VT

1030

hrs

AIAA-2

015-2

962

Hybr

id fs/

ps co

here

nt an

ti-Sto

kes

Rama

n sca

tterin

g in

a non

-eq

uilibr

ium en

viron

ment

initia

ted

by a

ns la

ser s

park

C. De

dic, J

. Mich

ael, T

. Mey

er, Io

wa S

tate

Unive

rsity,

Ames

, IA

1100

hrs

AIAA-2

015-2

963

Non-

Equil

ibrium

Ana

lysis

of

Emiss

ion Sp

ectro

scopy

Dat

a Tak

en

in th

e Fre

estre

am of

the N

ASA

IHF

Arc J

et Fa

cility

M. W

inter,

C. S

riniva

san,

R. Ch

arnigo

, Un

iversi

ty of

Kentu

cky,

Lexin

gton,

Lexin

gton,

KY

1130

hrs

AIAA-2

015-2

964

Quan

titat

ive M

easu

reme

nts o

f Ele

ctron

Num

ber D

ensit

y and

Th

resh

old fo

r Las

er In

duce

d Br

eakd

own

in Ai

rL.

Su, Y

. Wu,

J. Sa

wyer,

Z. Zh

ang,

Unive

rsity

of Te

nnes

see,

Knox

ville,

Kn

oxvil

le, TN

87

Wedn

esda

y, 24

June

201

518

2-TP

-9Ae

roth

ermo

dyna

mics

IIRo

setta

Chair

ed by

: A. M

ARTIN

, Univ

ersity

of Ke

ntuck

y09

00 hr

sAIA

A-201

5-296

5Sh

ock

Radia

tion

Tests

for S

atur

n an

d Ura

nus E

ntry

Pro

bes

B. Cr

uden

, D. B

ogda

noff,

ERC,

Inc.,

Moffe

tt Fie

ld, CA

0930

hrs

AIAA-2

015-2

966

Heat

Tran

sfer M

easu

reme

nts o

n th

e Af

terbo

dy of

Sphe

res i

n Hy

perso

nic

Free

-Fligh

t in

Air a

nd Ca

rbon

Di

oxide

M. W

ilder,

NAS

A Ame

s Res

earch

Cente

r, Mo

ffett

Field,

CA; D

. Bog

dano

ff, D

. Sa

unde

rs, ER

C, Inc

., Mo

ffett

Field,

CA

1000

hrs

AIAA-2

015-2

967

Shap

e Opt

imiza

tion

of a

Blun

t Bo

dy in

Rea

cting

Hyp

erso

nic fl

ow

in Th

erma

l Non

-Equil

ibrium

for

Redu

cing B

oth

Drag

and H

eat

Trans

fer

E. Zis

hka,

R. Ag

arwal,

Was

hingto

n Un

iversi

ty in

St. L

ouis,

St.

Louis

, MO

1030

hrs

AIAA-2

015-2

968

Fugin

e cyc

le th

eory

: pre

dictin

g high

ef

ficien

cy of

the s

uper

multij

et-co

nver

genc

e eng

ine w

orkin

g fro

m sta

rtup t

o hyp

erso

nic sc

ram

mode

K. Na

itoh,

Y. Ta

naka

, T. T

amura

, T.

Okam

oto, Y

. Noji

ma, K

. Yam

agish

i, Wa

seda

Univ

ersity

, Shin

juku,

Japa

n

Wedn

esda

y, 24

June

201

518

3-F3

60-5

09

30 -

1200

hrs

NACA

to N

ASA:

Emba

rking

on th

e Nex

t 100

Year

s of E

xcell

ence

and I

nnov

ation

in A

eron

autic

s and

Bey

ond

Gran

d Ball

room

E

Mode

rator:

Robe

rt Pe

arce,

Direc

tor, S

trateg

y, Arc

hitec

ture &

Analy

sis, A

erona

utics

Rese

arch M

ission

Dire

ctorat

e, NA

SA H

eadq

uarte

rs

Pan

elists

:Da

vid B

owles

Cente

r Dire

ctor (

Actin

g)NA

SA La

ngley

Rese

arch C

enter

Thom

as Ed

ward

sDe

puty

Cente

r Dire

ctor

NASA

Ames

Rsea

rch Ce

nter

Jane

t Kav

andi

Depu

ty Dir

ector

NASA

Glen

n Res

earch

Cente

r

David

McB

ride

Cente

r Dire

ctor

NASA

Arms

trong

Fligh

t Res

earch

Cente

r

Jaiw

on Sh

inAs

sociat

e Adm

inistra

tor, A

erona

utics

Resea

rch M

ission

Direc

torate

NASA

Hea

dqua

rters

Wedn

esda

y, 24

June

201

518

4-LN

CH-2

12

30 -

1400

hrs

Lunc

heon

in th

e Exp

ositio

n Ha

llCh

antill

y Ball

room

East

A tick

et is

requir

ed an

d inc

luded

in th

e con

feren

ce re

gistra

tion f

ee w

here

indica

ted.

Wedn

esda

y, 24

June

201

518

5-AA

-26

Comb

ustio

n No

iseFle

ur-d

e-lis

BCh

aired

by: J

. MEN

DOZA

, Unit

ed Te

chno

logies

Rese

arch C

enter

1400

hrs

AIAA-2

015-2

969

On th

e spe

ctrum

of co

mbus

tion

noise

C. Ta

m, Fl

orida

Stat

e Univ

ersity

, Ta

llaha

ssee,

FL

1430

hrs

AIAA-2

015-2

970

Mode

lling o

f com

busti

on n

oise

spec

trum

using

temp

oral

corre

lation

s of h

eat r

eleas

e rat

e fro

m tu

rbule

nt pr

emixe

d flam

esY.

Liu, U

nivers

ity of

Surr

ey, G

uildfo

rd,

Unite

d King

dom;

T. Ec

hekk

i, Nort

h Caro

lina

State

Univ

ersity

, Rale

igh, N

C

1500

hrs

AIAA-2

015-2

971

Nume

rical

inves

tigat

ion of

co

mbus

tion

noise

gene

ratio

n in

a fu

ll ann

ular c

ombu

stion

cham

ber

T. Liv

ebard

on, C

ERFA

CS, T

oulou

se, F

rance

; S.

More

au, U

nivers

ity of

She

rbroo

ke,

Sherb

rooke

, Can

ada;

T. Po

insot,

CERF

ACS,

To

ulous

e, Fra

nce;

E. Bo

uty, T

urbom

eca,

Borde

s, Fra

nce

1530

hrs

AIAA-2

015-2

972

Trans

fer F

uncti

ons o

f Aco

ustic

, En

tropy

and V

ortic

ity W

aves

in

an A

nnula

r Mod

el Co

mbus

tor a

nd

Nozz

le fo

r the

Pre

dictio

n of

the

Ratio

Betw

een

Indir

ect a

nd D

irect

Comb

ustio

n No

iseW.

Ullri

ch, T

. Satt

elmay

er, Te

chnic

al Un

iversi

ty of

Munic

h, Ga

rching

, Germ

any

1600

hrs

AIAA-2

015-2

973

Effic

ient F

ull 3

D Tu

rbule

nt

Comb

ustio

n No

ise Si

mulat

ion B

ased

on

Stoc

hasti

c Sou

nd So

urce

sF.

Grim

m, G

erman

Aeros

pace

Cente

r (D

LR),

Stutt

gart,

Germ

any;

R. Ew

ert, J

. Die

rke, G

erman

Aeros

pace

Cente

r (DL

R),

Brau

nsch

weig,

Germ

any;

B. N

oll, M

. Aig

ner, G

erman

Aeros

pace

Cente

r (DL

R),

Stutt

gart,

Germ

any

1630

hrs

AIAA-2

015-2

974

A 2D

-axis

ymme

tric a

nalyt

ical

mode

l for

the e

stima

tion

of in

direc

t co

mbus

tion

noise

in n

ozzle

flow

sJ.

Zhen

g, M.

Huet,

ONE

RA, C

hâtillo

n, Fra

nce;

A. Gia

uque

, Nati

onal

Cente

r for S

cienti

fic

Resea

rch (C

NRS)

, Ecul

ly, Fra

nce; F.

Cléro

, ON

ERA,

Châti

llon, F

rance;

S. Du

cruix,

Nati

onal

Cente

r for S

cienti

fic Re

search

(CNR

S),

Châte

nay-M

alabry

, Fran

ce

88

Wedn

esda

y, 24

June

201

518

6-AA

-27

Arra

ys M

ethod

Pan

el Se

ssion

Fleur

-de-

lis A

Chair

ed by

: C. B

AHR,

NASA

-Lang

ley Re

searc

h Cen

ter14

00 hr

sAIA

A-201

5-297

5De

velop

ment

of N

ew W

all-m

ount

ed

and S

trut-m

ount

ed P

hase

d Mi

croph

one A

rrays

for A

cous

tic

Meas

urem

ents

in Clo

sed T

est-

secti

on W

ind Tu

nnels

W. H

orne,

N. B

urnsid

e, NA

SA Am

es

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1430

hrs

AIAA-2

015-2

976

Deco

rrelat

ion of

Aco

ustic

Wav

e Pr

opag

ation

thro

ugh

the S

hear

La

yer i

n Op

en Je

t Wind

Tunn

elD.

Erns

t, C.

Speh

r, T. B

erkefe

ld, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Gött

ingen

, Ge

rman

y

1500

hrs

AIAA-2

015-2

977

An A

ppro

ach

to Es

timat

e the

Re

liabil

ity of

Micr

opho

ne A

rray

Meth

ods

G. H

erold,

E. S

arrad

j, Bran

denb

urg

Unive

rsity

of Te

chno

logy,

Cottb

us,

Germ

any

1530

hrs

AIAA-2

015-2

978

Pleth

arra

ys fo

r Aer

oaco

ustic

Ph

ased

Arra

y App

licat

ions

J. Un

derbr

ink, T

he B

oeing

Comp

any,

Seatt

le, W

A

1600

hrs

AIAA-2

015-2

979

Estim

ating

the s

ound

powe

r ra

diated

by a

nozz

le-ba

sed s

ource

in

a tes

t cell

usin

g a ph

ased

arra

yB.

Teste

r, K. H

ollan

d, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d Kin

gdom

1630

Discu

ssion

Wedn

esda

y, 24

June

201

518

7-AA

-28

Open

Rot

or II

Inve

rnes

sCh

aired

by: W

. DEV

ENPO

RT, V

irgini

a Tec

h14

00 hr

sAIA

A-201

5-298

0Op

en-R

otor

Nois

e Asse

ssmen

t with

CF

D/CA

A Ch

aining

A. Ch

elius

, T. L

e Garr

ec, D

. Minc

u, ON

ERA,

Châti

llon,

Franc

e

1430

hrs

AIAA-2

015-2

981

Flow

Disto

rtion

and N

oise P

rodu

ced

by a

Thru

sting

Rot

or In

gesti

ng a

Plana

r Tur

bulen

t Bou

ndar

y Lay

erD.

Wisd

a, H.

Murr

ay, W

. Alex

ande

r, M.

Nelso

n, W.

Dev

enpo

rt, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA

; S. G

legg,

Florid

a Atla

ntic U

nivers

ity,

Boca

Raton

, FL

1500

hrs

AIAA-2

015-2

982

Comp

utat

ion of

Rot

or N

oise

Gene

ratio

n in

Grid

Turb

ulenc

e Us

ing La

rge-

Eddy

Simu

lation

J. Wa

ng, K

. Wan

g, M.

Wan

g, Un

iversi

ty of

Notre

Dam

e, No

tre D

ame,

IN

1530

hrs

AIAA-2

015-2

983

Broa

dban

d nois

e for

rota

ting

blade

s: an

alysis

of ac

celer

ation

ef

fects

in th

e tim

e and

freq

uenc

y do

mains

S. S

inayo

ko, U

nivers

ity of

Sou

thamp

ton,

South

ampto

n, Un

ited K

ingdo

m

1600

hrs

AIAA-2

015-2

984

A 3D

analy

tical

appr

oach

for O

pen

roto

r Blad

e Vor

tex In

terac

tion(

BVI)

tona

l nois

eS.

More

au, M

. Qua

glia,

Sherb

rooke

Un

iversi

ty, S

herbr

ooke

, Can

ada;

R. Fe

rnand

o, Sa

fran G

roup,

Moiss

y-Cram

ayel,

Fra

nce

1630

hrs

AIAA-2

015-2

985

Analy

tical

Pred

iction

of th

e Pylo

n-Wa

ke Ef

fect o

n the

Tona

l Nois

e ra

diated

by th

e Fro

nt-Ro

tor of

CROR

Pr

opuls

ion Sy

stems

N. Ja

ouan

i, Sog

eti Hi

gh Te

ch, Is

sy Les

Mo

ulinea

ux, F

rance;

M. R

oger,

École

Centr

ale

de Ly

on, L

yon,

France

; T. N

odé-L

anglo

is, Air

bus,

Toulou

se, Fr

ance;

G. Se

rre, S

ogeti

High

Tec

h, Iss

y Les

Moulin

eaux

, Fran

ce

1700

hrs

AIAA-2

015-2

986

Comp

ariso

n of

roto

r nois

e me

asur

emen

t res

ults i

n lar

ge-sc

ale

and s

mall-

scale

anec

hoic

facil

ities

I. Be

lyaev

, V. K

opiev

, R. S

kvort

sov,

I. Pa

nkrat

ov, T

sAGI

, Mos

cow,

Russi

a; V.

Titare

v, Ru

ssian

Acad

emy o

f Scie

nces

, Mo

scow,

Russi

a; M.

Zayts

ev, T

sAGI

, Mo

scow,

Russi

a

Wedn

esda

y, 24

June

201

518

8-AA

-29

Airfr

ame N

oise I

IILa

lique

Chair

ed by

: S. N

OELTI

NG, E

XA14

00 hr

sAIA

A-201

5-298

7An

Asse

ssmen

t of F

lap an

d Main

La

nding

Gea

r Nois

e Aba

temen

t Co

ncep

tsM.

Khorr

ami, W

. Hum

phrey

s, D.

Locka

rd,

NASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA

1430

hrs

AIAA-2

015-2

988

Evalu

ation

of A

irfra

me N

oise

Redu

ction

Conc

epts

via Si

mulat

ions

Using

a La

ttice

Bolt

zman

n Ap

proa

chE.

Fares

, D. C

asali

no, E

xa G

mbH,

St

uttga

rt, G

erman

y; M.

Khorr

ami, N

ASA

Lang

ley Re

searc

h Cen

ter, H

ampto

n, VA

1500

hrs

AIAA-2

015-2

989

A Co

mpar

ative

Stud

y of S

imula

ted

and m

easu

red G

ear-F

lap Fl

ow

Inter

actio

nM.

Khorr

ami, N

ASA L

angle

y Rese

arch C

enter

, Ha

mpton

, VA;

R. Mi

neck,

Self,

Yorkt

own,

VA; E

. Fare

s, Ex

a Gmb

H, Stu

ttgart

, Germ

any;

C. Ya

o, L.

Jenkin

s, NA

SA La

ngley

Resea

rch

Cente

r, Ham

pton,

VA

1530

hrs

AIAA-2

015-2

990

Comp

ariso

n of

Comp

utat

ional

and

Expe

rimen

tal M

icrop

hone

Arra

y Re

sults

for a

n 18

%-Sc

ale A

ircra

ft Mo

del

D. Lo

ckard

, W. H

umph

reys,

M. Kh

orram

i, NA

SA La

ngley

Rese

arch C

enter

, Ham

pton,

VA; E

. Fare

s, D.

Casa

lino,

Exa G

mbH,

St

uttga

rt, G

erman

y; P.

Rave

tta, A

VEC,

Inc.,

Black

sburg

, VA

1600

hrs

AIAA-2

015-2

991

Char

acter

izatio

n of

Flap

Edge

Nois

e Ra

diatio

n fro

m a H

igh-Fi

delity

Ai

rfram

e Mod

elW.

Hum

phrey

s, M.

Khorr

ami, D

. Loc

kard,

D.

Neu

hart,

C. B

ahr, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

1630

hrs

AIAA-2

015-2

992

On th

e Con

necti

on be

twee

n Fla

p Sid

e-Ed

ge N

oise a

nd Ti

p Vor

tex

Dyna

mics

D. Ca

salin

o, E.

Fares

, B. D

uda,

A. Ha

zir,

Exa G

mbH,

Stut

tgart,

Germ

any;

M.

Khorr

ami, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1700

hrs

AIAA-2

015-2

993

Simula

tions

of LA

GOON

land

ing-

gear

nois

e usin

g Lat

tice B

oltzm

ann

Solve

rA.

Seng

issen

, J. G

iret,

Airbu

s, To

ulous

e, Fra

nce;

C. Co

reixa

s, J.

Bous

suge

, CE

RFAC

S, To

ulous

e, Fra

nce

89

Wedn

esda

y, 24

June

201

518

9-AA

-30

Jet N

oise M

easu

reme

nts I

IOb

elisk

ACh

aired

by: D

. JUV

E, Ec

ole Ce

ntrale

de Ly

on14

00 hr

sAIA

A-201

5-299

4Du

al-pla

ne, ti

me-re

solve

d, ste

reo PI

V for

wav

epac

ket e

ducti

on in

a tur

bulen

t su

bson

ic jet

V. Jau

net, P

. Brau

d, F. B

oisson

neau

, P. Jo

rdan,

Natio

nal C

enter

for S

cienti

fic Re

search

(C

NRS)

, Poit

iers,

France

; A. C

avalie

ri, Tec

hnolo

gical

Institu

te of

Aeron

autics

(ITA)

, Sã

o José

dos C

ampo

s, Bra

zil

1430

hrs

AIAA-2

015-2

995

Adap

tatio

n of

the A

zimut

hal

Deco

mpos

ition

Tech

nique

to Je

t No

ise M

easu

erem

ents

of an

Airc

raft

Engin

e in

the G

roun

d Tes

tsV.

Kopie

v, I.

Belya

ev, G

. Fara

noso

v, M.

Zayts

ev, T

sAGI

, Mos

cow,

Russi

a; A.

Aleks

entse

v, Y.

Berse

nev,

OJSC

Av

iadvig

atel, P

erm, R

ussia

; et a

l.

1500

hrs

AIAA-2

015-2

996

On th

e sys

temat

ic er

ror i

n me

asur

emen

ts of

jet n

oise fl

ight

effe

cts u

sing o

pen

jet w

ind tu

nnels

U. M

ichel,

CFD

Softw

are G

mbH,

Berl

in,

Germ

any

1530

hrs

AIAA-2

015-2

997

Role

of N

ozzle

’s Pr

oxim

ity to

Ple

num

Cham

bers

or O

ther

Non

-lin

e-of

-sigh

t Dev

ices o

n Me

asur

ed

Jet N

oise

A. Ka

ron, D

. Dick

ey, K

. Ahu

ja, G

eorgi

a Ins

titute

of Te

chno

logy,

Atlan

ta, G

A

1600

hrs

AIAA-2

015-2

998

Scatte

ring o

f tur

bulen

t-jet

wave

pack

ets by

a sw

ept tr

ailing

edge

S. Pia

ntanid

a, V.

Jaune

t, P. J

ordan

, J. H

uber,

Na

tiona

l Cen

ter fo

r Scie

ntific

Resea

rch (C

NRS)

, Po

itiers,

Fran

ce; A.

Cava

lieri, T

echno

logica

l Ins

titute

of Ae

ronau

tics (I

TA), S

ão Jo

sé

dos C

ampo

s, Bra

zil; W

. Wolf

, Univ

ersity

of

Camp

inas,

Camp

inas,

Brazil

1630

hrs

AIAA-2

015-2

999

Inve

stiga

ting t

he fe

edba

ck pa

th in

a j

et-su

rface

reso

nant

inter

actio

nK.

Zama

n, A.

Faga

n, J.

Bridg

es, C

. Brow

n, NA

SA G

lenn R

esea

rch Ce

nter, C

levela

nd,

OH

Wedn

esda

y, 24

June

201

519

0-AC

D-5

Desig

n of

Unc

onve

ntion

al Ai

rcraf

t Con

figur

ation

sMo

rocco

Chair

ed by

: M. L

OGAN

, NAS

A Lan

gley R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-3

000

An In

vesti

gatio

n int

o the

Des

ign of

an

Effic

ient I

n Gr

ound

Effe

ct Fly

ing

Vehic

le Pla

nfor

mV.

Miroc

hnitc

henk

o, T.

Taka

hash

i, Ariz

ona

State

Univ

ersity

, Tem

pe, A

Z

1430

hrs

AIAA-2

015-3

001

Adva

nced

Gen

eral

Aviat

ion Co

ncep

t Stu

dy fo

r a R

oada

ble A

ircra

ftD.

Lim,

C. Ju

stin,

D. M

avris

, Geo

rgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1500

hrs

AIAA-2

015-3

002

Morp

hing S

trateg

y Des

ign fo

r Va

riable

-Wing

Airc

raft

R. Sh

i, J. P

eng,

Tsing

hua U

nivers

ity,

Beijin

g, Ch

ina

1530

hrs

AIAA-2

015-3

003

A Me

thod

ology

for M

ulti-

Disci

plina

ry A

nalys

is of

the B

ox

Wing

Conc

ept

I. Ro

y Sala

m, C.

Bil,

RMIT

Unive

rsity,

Me

lbourn

e, Au

strali

a

1600

hrs

AIAA-2

015-3

004

The H

oops

on th

e Way

to

a Sup

erso

nic B

usine

ss Je

t (P

erfo

rman

ce D

river

s for

a Co

mmer

cially

Viab

le Pr

oduc

t)L.

Gonz

alez-L

inero,

Embry

-Ridd

le Ae

ronau

tical

Unive

rsity,

Day

tona B

each

, FL

Wedn

esda

y, 24

June

201

519

1-AM

T-11/

GT-1

1Gr

ound

Test

Facil

ity Im

prov

emen

ts II

Obeli

sk B

Chair

ed by

: R. R

HEW,

NAS

A-Lan

gley R

esea

rch Ce

nter a

nd J.

HOP

F, Ae

rospa

ce Te

sting

Allia

nce

1400

hrs

AIAA-2

015-3

005

Lyap

unov

-Bas

ed N

onlin

ear C

ontro

l of

Wind

Tunn

el Su

perso

nic N

ozzle

Co

ntou

rM.

Sad

raey,

Danie

l Web

ster C

olleg

e, Na

shua

, NH

1430

hrs

AIAA-2

015-3

006

Deve

lopme

nt an

d Dem

onstr

ation

of

A Co

ntinu

ous B

eta Sw

eep T

est &

An

alysis

Tech

nique

(CBS

TAT)

Rig

K. Xie

, F. W

ang,

N. Ch

en, L

. Che

n, Q.

Sh

en, C

hina A

cade

my of

Aeros

pace

Ae

rodyn

amics

, Beij

ing, C

hina

1500

hrs

AIAA-2

015-3

007

Wind

Tunn

el Tes

ting o

f Var

iable

Camb

er Co

mplia

nt Wi

ng w

ith M

ultipl

e Lo

ad Ce

ll Test

Fixtu

reL.

Zienta

rski, C

. Mark

s, Un

iversit

y of D

ayton

, Da

yton,

OH; J

. Joo

, Air F

orce R

esearc

h La

borat

ory, W

right-

Patte

rson A

FB, O

H

1530

hrs

AIAA-2

015-3

008

Comp

ariso

n of

Free

jet D

ata

betw

een

a Con

tour

ed an

d Con

ical

Nozz

le in

the A

EDC H

1 Fa

cility

G. H

ammo

ck, A

rnold

Engin

eerin

g De

velop

ment

Comp

lex, A

rnold

AFB,

TN

1600

hrs

Oral

Prese

ntatio

nOv

ervie

w of

Unc

erta

inty A

nalys

is Ac

tivitie

s at N

ASA

Glen

n’s

Aero

prop

ulsion

Facil

ities

J. St

ephe

ns, E

. Hub

bard,

NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA

1630

hrs

AIAA-2

015-3

009

Reac

tivat

ion of

the N

TF 3

000

Ton

Liquid

Nitr

ogen

Tank

from

Amb

ient

Cond

ition

S. D

unn,

NASA

Lang

ley Re

searc

h Cen

ter,

Hamp

ton, V

A

Wedn

esda

y, 24

June

201

519

2-AM

T-12/

GT-1

2Th

e Imp

act o

f PIV

on A

eros

pace

Tech

nolog

y IEd

elweis

sCh

aired

by: S

. BER

ESH,

San

dia N

ation

al La

borat

ories

and K

. LOW

E, Vir

ginia

Tech

1400

hrs

Oral

Prese

ntatio

nAp

plica

tion

of P

artic

le Im

age

Veloc

imetr

y at N

ASA

for R

otor

craft

Rese

arch

(Inv

ited)

L. Je

nkins

, G. Y

amau

chi, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

1430

hrs

Oral

Prese

ntatio

nPI

V for

heli

copt

er ae

rody

nami

cs (In

vited

)M.

Raffe

l, Germ

an Ae

rospa

ce Ce

nter

(DLR

), Co

logne

, Germ

any

1500

hrs

Oral

Prese

ntatio

nTim

e-re

solve

d PIV

in th

e buf

fetin

g re

gime o

f ARI

ANE V

(Inv

ited)

F. Sc

arano

, Delf

t Univ

ersity

of Te

chno

logy,

Delft,

The N

etherl

ands

1530

hrs

Oral

Prese

ntatio

nSu

bson

ic Wa

ke Ch

arac

teriza

tion

of

the O

rion

Caps

ule u

sing P

IV in

the

Ames

UPW

T 11-

foot

Wind

Tunn

el (In

vited

)J.

Heine

ck, N

ASA A

mes R

esea

rch Ce

nter,

Moffe

tt Fie

ld, CA

1600

hrs

Oral

Prese

ntatio

nIn

dustr

ial A

pplic

ation

s of P

IV in

JA

XA La

rge-

Scale

Wind

Tunn

els

(Invit

ed)

H. Ka

to, S

. Koik

e, Ja

pan A

erosp

ace

Explo

ration

Agen

cy (J

AXA)

, Tok

yo, J

apan

1630

hrs

Oral

Prese

ntatio

nRe

cent

App

licat

ions o

f PIV

in La

rge

NRC W

ind Tu

nnels

F. de

Sou

za, N

ation

al Re

searc

h Cou

ncil

Cana

da, O

ttawa

, Can

ada

1700

hrs

Oral

Prese

ntatio

nAp

plica

tions

of P

IV m

easu

reme

nts

in th

e ONE

RA la

rge w

ind tu

nnels

(In

vited

)Y.

Mich

ou, O

NERA

, Cha

mbery

, Fran

ce

90

Wedn

esda

y, 24

June

201

519

3-AP

A-21

Trans

onic

& Su

perso

nic A

erod

ynam

icsSte

mmon

s ACh

aired

by: M

. JUR

KOVIC

H, U

S Air

Force

1400

hrs

AIAA-2

015-3

010

Nume

rical

Study

of Co

unter

flowi

ng

Jet E

ffects

on Su

perso

nic Sl

ende

r-Bo

dy Co

nfigu

ratio

nsB.

Venk

atach

ari, N

ation

al Ins

titute

of Ae

rospa

ce, H

ampto

n, VA

; M. M

ullan

e, Un

iversi

ty of

Alaba

ma, B

irming

ham,

Bir

ming

ham,

AL; G

. Che

ng, U

nivers

ity of

Ala

bama

, Tus

caloo

sa, T

usca

loosa

, AL;

C. Ch

ang,

NASA

Lang

ley Re

searc

h Cen

ter,

Hamp

ton, V

A

1430

hrs

AIAA-2

015-3

011

Flow

Phys

ics of

a Th

ree-

Dime

nsion

al Ro

unde

d Con

tour

Bu

mp in

a Ma

ch 1

.3 Su

perso

nic

Free

-stre

amK.

Lo, K

. Kon

tis, U

nivers

ity of

Glas

gow,

Gla

sgow

, Unit

ed Ki

ngdo

m

1500

hrs

AIAA-2

015-3

012

Supe

rsonic

Air

Flows

Aro

und S

ome

Geom

etrica

l Prim

itives

M. Ko

tov, I

. Kryu

kov,

L. Ru

leva,

S.

Solod

ovnik

ov, S

. Surz

hikov

, Rus

sian

Acad

emy o

f Scie

nces

, Mos

cow,

Russi

a

Wedn

esda

y, 24

June

201

519

4-AP

A-22

VSTO

L/ST

OL A

erod

ynam

icsCa

rpen

ter B

allro

omCh

aired

by: M

. CAL

VERT

, U.S

. Arm

y AMR

DEC

1400

hrs

AIAA-2

015-3

013

The L

IFT! P

rojec

t - M

odula

r, Ele

ctric

Verti

cal L

ift Sy

stem

with

Gro

und

Powe

r Teth

erM.

Duff

y, A.

Sama

ritano

, The

Boe

ing

Comp

any,

Ridley

Park,

PA

1430

hrs

AIAA-2

015-3

014

Nume

rical

Inve

stiga

tion

and

Valid

ation

for O

pen

Roto

r Hov

er

Perfo

rman

ceQ.

Zhao

, C. S

heng

, Univ

ersity

of To

ledo,

Toled

o, OH

Wedn

esda

y, 24

June

201

519

5-AP

A-23

Weap

ons A

erod

ynam

ics: M

issile

/Pro

jectile

/Guid

ed-M

unitio

ns, C

arria

ge an

d Sto

re Se

para

tion

IISte

mmon

s BCh

aired

by: K

. DEN

ISSEN

, San

dia N

ation

al La

bs14

00 hr

sAIA

A-201

5-301

5CF

D Ae

rody

nami

c Cha

racte

rizat

ion

of a

High

Man

euve

rabil

ity A

irfra

meC.

Coyle

, U.S

. Milit

ary Ac

adem

y, We

st Po

int, N

Y; S.

Silto

n, Arm

y Res

earch

La

borat

ory, A

berde

en Pr

oving

Grou

nd, M

D

1430

hrs

AIAA-2

015-3

016

Deve

lopme

nt an

d Vali

datio

n of

a RA

NS-b

ased

Aird

rop S

imula

tion

Appr

oach

S. G

eisba

uer, G

erman

Aeros

pace

Cente

r (D

LR),

Brau

nsch

weig,

Germ

any;

H.

Schm

idt, G

erman

Aeros

pace

Cente

r (DL

R),

Göttin

gen,

Germ

any

1500

hrs

AIAA-2

015-3

017

Cavit

y-Sto

re In

terac

tion

unde

r Su

perso

nic Fr

eestr

eam

Cond

itions

J. Me

rrick,

M. Re

eder,

Air F

orce I

nstitu

te of

Tech

nolog

y, W

right-

Patte

rson A

FB, O

H

1530

hrs

AIAA-2

015-3

018

Load

s and

Aco

ustic

s Pre

dictio

n on

De

ploye

d Wea

pons

Bay

Doo

rsE.

Sheta

, R. H

arris,

CFD

Rese

arch

Corpo

ration

, Hun

tsville

, AL;

E. Lu

ke,

Missi

ssipp

i Stat

e Univ

ersity

, Miss

issipp

i St

ate, M

S; L.

Uke

iley,

Unive

rsity

of Flo

rida,

Gaine

sville

, Gain

esvil

le, FL

Wedn

esda

y, 24

June

201

519

6-AS

E-2Ai

rcraf

t Icin

g and

Atm

osph

eric

Haza

rds

Plum

Blos

som

BCh

aired

by: W

. VAU

GHAN

, Willi

am W

Vaug

han C

onsu

ltant

and J

. OW

ENS,

NAS

A (Re

tired)

1400

hrs

AIAA-2

015-3

019

A mo

del f

or in

-fligh

t ice

accre

tion

base

d on

the e

xact

solut

ion of

the

unste

ady S

tefan

prob

lemG.

Gori

, M. Z

occa

, A. G

uardo

ne, T

echn

ical

Unive

rsity

of Mi

lan, M

ilan,

Italy

1430

hrs

AIAA-2

015-3

020

Quas

i-Uns

teady

Icing

Simu

lation

of

an O

scilla

ting A

irfoil

H. Fo

uladi,

McG

ill Un

iversi

ty, M

ontré

al,

Cana

da; C

. Alia

ga, N

ewme

rical

Tech

nolog

ies In

terna

tiona

l, Mon

tréal,

Ca

nada

; W. H

abas

hi, M

cGill

Unive

rsity,

Mo

ntréa

l, Can

ada

1500

hrs

AIAA-2

015-3

021

Conv

ectiv

e Enh

ance

ment

of Ic

ing

Roug

hnes

s Elem

ents

in Sta

gnat

ion

Regio

n Flo

wsM.

Hug

hes,

S. M

cClai

n, Ba

ylor U

nivers

ity,

Waco

, TX;

M. V

argas

, A. B

roeren

, NAS

A Gle

nn Re

searc

h Cen

ter, C

levela

nd, O

H

1530

hrs

AIAA-2

015-3

022

Sens

or Su

ite D

evelo

pmen

t for

a We

athe

r UAV

J. Ha

thawa

y, A.

Avery

, J. J

acob

, Okla

homa

St

ate U

nivers

ity, S

tillwa

ter, O

K

1600

hrs

AIAA-2

015-3

023

Sens

itivity

Ana

lysis

of W

ake V

ortex

Pa

rame

ters M

easu

red b

y Dop

pler

Lidar

T. Mi

saka

, S. O

baya

shi, T

ohok

u Univ

ersity

, Se

ndai,

Japa

n; A.

Step

han,

F. Ho

lzäpfe

l, T.

Gerz,

Germ

an Ae

rospa

ce Ce

nter (

DLR)

, Ob

erpfaf

fenho

fen, G

erman

y

91

Wedn

esda

y, 24

June

201

519

7-AT

IO-1

8AT

M IV

- Ec

onom

ic/Be

nefit

s Ana

lysis

Ming

Chair

ed by

: S. H

ASAN

, LMI

1400

hrs

AIAA-2

015-3

024

Iden

tifyin

g ben

efit m

echa

nisms

for

Next

Gen

techn

ologie

s and

conc

epts

S. La

ndry,

D. P

eng,

Purdu

e Univ

ersity

, We

st La

fayett

e, IN

1430

hrs

AIAA-2

015-3

025

Asse

ssing

Dep

artu

re Ef

ficien

cy

at U

.S. A

irpor

ts: a

Comp

ariso

n of

Me

thod

sS.

Tsao

, J. D

eArm

on, S

. Agb

olosu

-Amiso

n, A.

Maha

shab

de, M

ITRE C

orpora

tion,

McLe

an, V

A

1500

hrs

AIAA-2

015-3

026

Airfar

e Dete

rmina

nts on

the K

anga

roo

Route

(Aus

tralia

-UK M

arke

t): A

Case

Stu

dy of

the I

nflue

nces

of Air

lines,

All

iances

and A

irpor

tsH.

Yang

, Civil

Aviat

ion Fl

ight U

nivers

ity of

Ch

ina, G

uang

han,

China

1530

hrs

AIAA-2

015-3

027

Conc

ept a

nd Be

nefit

s of P

BN-En

abled

Pa

ralle

l App

roac

h Ope

ratio

nsR.

Maye

r, B. C

row, D

. Zon

derva

n, MI

TRE

Corpo

ration

, McLe

an, V

A; J.

Allerd

ice, F

edera

l Av

iation

Admi

nistra

tion,

Peach

tree C

ity, GA

Wedn

esda

y, 24

June

201

519

8-AT

IO-1

9Te

rmina

l & Su

rface

Ope

ratio

ns IV

Milan

Chair

ed by

: R. C

URRA

N, D

elft T

echn

ical U

nivers

ity of

Tech

nolog

y14

00 hr

sAIA

A-201

5-302

8Op

timiza

tion

of P

ush

Back

Time

Wi

ndow

s Tha

t Ens

ure C

onfli

ct Fr

ee

Ramp

Are

a Airc

raft

Trajec

torie

sJ.

Coup

e, D.

Milu

tinov

ic, U

nivers

ity of

Ca

liforni

a, Sa

nta Cr

uz, S

anta

Cruz,

CA; W

. Ma

lik, U

nivers

ity of

Califo

rnia,

Santa

Cruz

, Mo

ffett

Field,

CA; Y

. Jun

g, NA

SA Am

es

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1430

hrs

AIAA-2

015-3

029

Deve

lopme

nt of

Gen

eric

Grou

nd

Track

s of P

erfo

rman

ce B

ased

Na

vigat

ion O

pera

tions

for F

leet-

Leve

l Airp

ort N

oise A

nalys

isA.

Wilso

n, M.

LeVin

e, J.

Berna

rdo, M

. Kir

by, D

. Mav

ris, G

eorgi

a Ins

titute

of Te

chno

logy,

Atlan

ta, G

A

1500

hrs

AIAA-2

015-3

030

Imple

ment

ing a

Comb

ined A

rriva

l, De

partu

re, a

nd Su

rface

Sche

duler

fo

r a M

etrop

lexF.

Wiel

and,

W. Kr

uege

r, W. P

eng,

Y. Zh

ang,

A. Ty

agi, C

. Ye,

Intell

igent

Autom

ation

, Inc

., Ro

ckvil

le, M

D; et

al.

1530

hrs

AIAA-2

015-3

031

A fra

mewo

rk fo

r the

clas

sifica

tion

and p

riorit

izatio

n of

arriv

al an

d de

partu

re ro

utes

in M

ulti-A

irpor

t Sy

stems

Term

inal M

anoe

uvrin

g Ar

eas

S. S

idirop

oulos

, A. M

ajumd

ar, K.

Han

, W.

Schu

ster, W

. Och

ieng,

Impe

rial C

olleg

e Lo

ndon

, Lon

don,

Unite

d King

dom

Wedn

esda

y, 24

June

201

519

9-AT

IO-2

0Tra

nsfo

rmat

ional

Fligh

t - A

uton

omy I

IMo

net B

allro

omCh

aired

by: B

. ALLE

N, N

ASA L

angle

y Res

earch

Cente

r14

00 hr

sAIA

A-201

5-303

2Us

ing M

ultim

odal

Inpu

t for

Au

tono

mous

Dec

ision

Mak

ing

for U

nman

ned S

ystem

s - “W

hat

it ne

eds i

n or

der t

o evo

lve, is

a hu

man q

uality

. Our

capa

city t

o lea

p be

yond

logic

.” - C

apt.

Kirk

, Sta

r Tre

k: Th

e Mot

ion P

ictur

eJ.

Neila

n, C.

Cross,

H. F

an, W

. Feh

lman

, L.

Hemp

ley, M

. Mott

er, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

; et a

l.

1430

hrs

AIAA-2

015-3

033

Colla

bora

ting w

ith A

uton

omou

s Ag

ents

A. Tru

jillo,

NASA

Lang

ley Re

searc

h Ce

nter, H

ampto

n, VA

; H. F

an, A

nalyt

ical

Mech

anics

Asso

ciates

, Inc

., Ha

mpton

, VA;

L. He

mpley

, C. C

ross,

North

rop G

rumma

n Co

rporat

ion, H

ampto

n, VA

; W. F

ehlm

an,

M. M

otter,

NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A; et

al.

1500

hrs

AIAA-2

015-3

034

A Fle

xible

Fligh

t Con

trol S

ystem

for

Rapid

GNC

and D

istrib

uted

Cont

rol

Deplo

ymen

tP.

Rothh

aar, C

. Cros

s, H.

Fan,

W. Fe

hlman

, L.

Hemp

ley, M

. Mott

er, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

; et a

l.

1530

hrs

AIAA-2

015-3

035

Oper

ating

in “S

trang

e New

Wo

rlds”

and M

easu

ring S

ucce

ss - T

est a

nd Ev

aluat

ion in

Comp

lex

Envir

onme

nts

G. Q

ualls,

C. Cr

oss,

H. Fa

n, W.

Fehlm

an,

L. He

mpley

, M. M

otter,

NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA; e

t al.

1600

hrs

AIAA-2

015-3

036

State

of th

e Art

of A

uton

omou

s Pla

tform

s and

Hum

an-M

achin

e Sy

stems

: Only

a Fo

ol Wo

uld St

and

In th

e Way

of P

rogr

ess

V. Sto

uffer,

LMI, M

cLean

, VA;

K. Go

odrich

, NA

SA La

ngley

Resea

rch Ce

nter, H

ampto

n, VA

92

Wedn

esda

y, 24

June

201

520

0-BA

L-2Ba

lloon

Syste

ms II

Steub

enCh

aired

by: J

. RAN

D, W

inzen

Engin

eerin

g Inc

1400

hrs

AIAA-2

015-3

037

Ballo

on A

spec

t of S

tratEx

Wor

ld Re

cord

Skyd

iveJ.

Nott,

Nott

Tech

nolog

y, Sa

nta B

arbara

, CA

1430

hrs

AIAA-2

015-3

038

Rece

nt Im

prov

emen

ts to

the D

esign

an

d Man

ufac

ture

of H

igh A

ltitud

e Ze

ro-P

ressu

re B

alloo

nsJ.

Marsh

, Colu

mbia

Scien

tific B

alloo

n Fa

cility,

Pales

tine,

TX; M

. Gile

s, Ra

ven

Aeros

tar, S

ulphu

r Spri

ngs,

TX

1500

hrs

AIAA-2

015-3

039

The W

allop

s Arc

Seco

nd P

ointer

- A

Ballo

on B

orne

Fine

Poin

ting S

ystem

D. S

tuchli

k, NA

SA G

odda

rd Sp

ace F

light

Cente

r, Gree

nbelt

, MD

1530

hrs

AIAA-2

015-3

040

Curre

nt St

atus

of a

NASA

High

-Al

titud

e Ball

oon-

Base

d Obs

erva

tory

fo

r Plan

etary

Scien

ceD.

Varga

, NAS

A Glen

n Res

earch

Cente

r, Cle

velan

d, OH

; E. Y

oung

, Sou

thwes

t Re

searc

h Ins

titute,

Bou

lder, C

O

1600

hrs

AIAA-2

015-3

041

Tech

nolog

y Dev

elopm

ent f

or th

e Ex

aVolt

Ant

enna

(EVA

). 1/

20-S

cale

Deplo

ymen

t Tes

tF.

Bagin

ski, G

eorge

Was

hingto

n Univ

ersity

, Wa

shing

ton, D

C; P.

Gorha

m, U

nivers

ity

of Ha

waii,

Hono

lulu,

Hono

lulu,

HI; D

. Fa

irbrot

her, M

. Said

, S. L

ang,

NASA

Wa

llops

Fligh

t Fac

ility,

Wallo

ps Is

land,

VA

1630

hrs

AIAA-2

015-3

042

Shap

e Ana

lysis

of th

e 1/2

0-Sc

ale

ExaV

olt A

nten

na Te

st Ba

lloon

F. Ba

ginsk

i, Geo

rge W

ashin

gton

Unive

rsity,

Was

hingto

n, DC

; K. B

rakke

, Su

sque

hann

a Univ

ersity

, Seli

nsgro

ve, P

A; K.

Zhao

, Geo

rge W

ashin

gton U

nivers

ity,

Wash

ington

, DC

1700

hrs

AIAA-2

015-3

043

An U

nderg

radu

ate St

uden

t Ins

trume

ntatio

n Pro

ject (

USIP)

to

Deve

lop N

ew In

strum

ent T

echno

logy

to Stu

dy th

e Aur

oral

Ionos

phere

and

Strato

sphe

ric O

zone

Laye

r Usin

g Ul

tralig

ht Ba

lloon

Paylo

ads

E. Be

ring,

R. Ga

mblin,

Unive

rsity o

f Hou

ston,

Houst

on, T

X

Wedn

esda

y, 24

June

201

520

1-CF

D-21

Disco

ntinu

ous G

alerk

in Me

thod

sGr

and B

allro

om A

Chair

ed by

: C. S

CHRO

CK, A

ir Firc

e Res

earch

Labo

ratory

and L

. DIO

SADY

, NAS

A Ame

s Res

earch

Cente

r14

00 hr

sAIA

A-201

5-304

4Ge

nera

l elem

ent s

hape

s with

in a t

enso

r-pro

duct

highe

r-ord

er

spac

e-tim

e disc

ontin

uous

-Gale

rkin

form

ulatio

nL.

Diosa

dy, S

. Murm

an, N

ASA A

mes

Rese

arch C

enter

, Moff

ett Fi

eld, C

A

1430

hrs

AIAA-2

015-3

045

High

-ord

er D

iscon

tinuo

us G

alerk

in Me

thod

s App

lied t

o Mult

iphas

e Flo

wsM.

Hen

ry de

Frah

an, E

. Joh

nsen

, Un

iversi

ty of

Mich

igan,

Ann A

rbor, A

nn

Arbor,

MI

1500

hrs

AIAA-2

015-3

046

An Ad

aptiv

e Exp

licit 3

D Di

sconti

nuou

s Ga

lerkin

Solve

r for

Uns

teady

Pr

oblem

sA.

Kirby,

D. M

avrip

lis, Un

iversit

y of W

yomi

ng,

Laram

ie, La

ramie,

WY;

A. Wi

ssink

, Arm

y Av

iation

and M

issile

Resea

rch De

velop

ment

and E

ngine

ering

Cente

r, Moff

ett Fi

eld, C

A

1530

hrs

AIAA-2

015-3

047

A Hy

brid

Reco

nstru

cted

Disco

ntinu

ous G

alerk

in an

d Co

ntinu

ous G

alerk

in me

thod

for

Inco

mpre

ssible

Flow

sA.

Pand

are, H

. Luo

, Nort

h Caro

lina S

tate

Unive

rsity,

Ralei

gh, N

C

Wedn

esda

y, 24

June

201

520

2-CF

D-22

Futu

re of

Fluid

s: Ne

xt G

ener

ation

CFD

(Invit

ed)

Gran

d Ball

room

BCh

aired

by: M

. MAL

IK, N

ASA-L

angle

y Res

earch

Cente

r and

A. KH

ODAD

OUST

, Boe

ing En

ginee

ring O

perat

ions &

Tech

nolog

y14

00 hr

sOr

al Pre

senta

tion

Impa

cting

Des

ign w

ith La

rge E

ddy

Simula

tion

(Invit

ed)

P. Mo

in, S

tanfor

d Univ

ersity

, Stan

ford,

CA; F

. Ham

, Cas

cade

Tech

nolog

ies, I

nc.,

Palo

Alto,

CA

1430

hrs

AIAA-2

015-3

048

Next

-Gen

erat

ion CF

D fo

r Hy

perso

nic an

d Aer

othe

rmal

Flows

(In

vited

)G.

Cand

ler, U

nivers

ity of

Minn

esota

, Mi

nnea

polis,

Minn

eapo

lis, M

N

1500

hrs

AIAA-2

015-3

049

Scali

ng Li

mits

for P

DE-B

ased

Sim

ulatio

n (In

vited

)P.

Fisch

er, U

nivers

ity of

Illino

is, U

rbana

-Ch

ampa

ign, U

rbana

, IL

1530

hrs

AIAA-2

015-3

050

PyFR

: Nex

t-Gen

eratio

n High

-Ord

er

Comp

utatio

nal F

luid D

ynam

ics on

Ma

ny-Co

re Ha

rdwa

re (In

vited

)P. V

incen

t, F. W

itherd

en, A

. Farr

ington

, G.

Ntem

os, B.

Verm

eire,

J. Pa

rk, Im

peria

l Colle

ge

Lond

on, L

ondo

n, Un

ited K

ingdo

m; et

al.

1600

hrs

AIAA-2

015-3

051

Towa

rds h

igh-fi

delity

aero

spac

e de

sign

in th

e age

of ex

treme

scale

su

perco

mput

ing (I

nvite

d)Q.

Wan

g, Ma

ssach

usett

s Ins

titute

of Te

chno

logy,

Camb

ridge

, MA

1630

hrs

AIAA-2

015-3

052

Oppo

rtunit

ies an

d Cha

lleng

es fo

r Mu

lti-Di

scipli

nary

Ana

lysis

and

Optim

izatio

n at

Exas

cale

(Invit

ed)

J. Alo

nso,

Stan

ford U

nivers

ity, S

tanfor

d, CA

1700

hrs

AIAA-2

015-3

053

CFD

for N

ext G

ener

ation

Har

dwar

e: Ex

perie

nces

with

Prox

y App

licat

ions

K. Fra

nko,

T. Fis

her, P

. Lin,

S. B

ova,

Sand

ia Na

tiona

l Lab

orator

ies,

Albuq

uerqu

e, NM

Wedn

esda

y, 24

June

201

520

3-CF

D-23

Para

llel C

ompu

ting a

nd N

ovel

Arch

itectu

res

Plum

Blos

som

ACh

aired

by: L

. LUO

, Nort

h Caro

lina S

tate U

nivers

ity an

d C. S

TONE

, Com

putat

ional

Scien

ce an

d Eng

ineeri

ng14

00 hr

sAIA

A-201

5-305

4Pa

ralle

l Tec

hniqu

es fo

r Nav

ier-

Stoke

s Solv

er ba

sed o

n 4t

h Or

der

Modifi

ed R

unge

-Kut

ta Sc

heme

wi

th TV

DH.

Sha

h, W

ichita

Stat

e Univ

ersity

, W

ichita

, KS

1430

hrs

AIAA-2

015-3

055

Optim

izatio

n of

A Fi

ne-g

raine

d BI

LU by

CUDA

Inter

-bloc

k Sy

nchr

oniza

tion

L. Lu

o, J.

Edwa

rds, H

. Luo

, F. M

ueller

, Nort

h Ca

rolina

State

Unive

rsity,

Raleig

h, NC

1500

hrs

AIAA-2

015-3

056

GPU

Para

lleliz

ation

of a

High

Ord

er

Imme

rsed B

ound

ary M

ethod

Fluid

So

lver

A. Jo

st, J.

Zhan

g, Flo

rida I

nstitu

te of

Tech

nolog

y, Me

lbourn

e, FL

; T. J

acks

on,

Unive

rsity

of Flo

rida,

Gaine

sville

, Ga

inesv

ille, F

L

1530

hrs

AIAA-2

015-3

057

A Hy

brid

CPU-

GPU

Para

llel O

ctree

Di

rect

Simula

tion

Mont

e Car

lo Ap

proa

chR.

Jamb

unath

an, D

. Lev

in, U

nivers

ity of

Illi

nois,

Urba

na-Ch

ampa

ign, U

rbana

, IL

1600

hrs

AIAA-2

015-3

058

High

-Per

form

ance

3D

Multi-

Disci

plina

ry Fl

uid/T

herm

al Pr

edict

ion u

sing C

ombin

ed M

ulti-

Core

/Mult

i-GPG

PU Co

mput

er

Syste

msC.

Ston

e, Co

mputa

tiona

l Scie

nce a

nd

Engin

eerin

g, LLC

, Chic

ago,

IL; R.

Dav

is,

Unive

rsity

of Ca

liforni

a, Da

vis, D

avis,

CA

1630

hrs

AIAA-2

015-3

059

Comp

ariso

n Of

Acce

lerat

ion

Tech

nique

s on

CFD

Open

-Sou

rce

Softw

are f

or A

eros

pace

App

licat

ions

L. Ma

ngan

i, G. R

oman

elli, U

nivers

ity

of Ap

plied

Scie

nces

and A

rts, L

uzern

, Sw

itzerl

and;

A. Ga

ddai,

Tech

nical

Unive

rsity

of Mi

lan, M

ilan,

Switz

erlan

d; E.

Casa

rtelli,

Univ

ersity

of Ap

plied

Scie

nces

an

d Arts

, Luz

ern, S

witze

rland

93

Wedn

esda

y, 24

June

201

520

4-CF

D-24

Desig

n Op

timiza

tion

Cora

lCh

aired

by: L

. TAO

, GE G

lobal

Rese

arch

1400

hrs

AIAA-2

015-3

060

Adjoi

nt-B

ased

Opt

imiza

tion

of a

Hype

rsonic

Inlet

H. Kl

ine, S

tanfor

d Univ

ersity

, Stan

ford,

CA;

F. Pa

lacios

, The

Boe

ing Co

mpan

y, Ev

erett,

WA

; T. E

cono

mon,

J. Alo

nso,

Stan

ford

Unive

rsity,

Stan

ford,

CA

1430

hrs

AIAA-2

015-3

061

Aero

dyna

mic S

hape

Opt

imiza

tion

for N

atur

al La

mina

r Flow

Usin

g a

Discr

ete-A

djoint

App

roac

hR.

Rash

ad, D

. Zing

g, Un

iversi

ty of

Toron

to,

Toron

to, Ca

nada

1500

hrs

AIAA-2

015-3

062

A Co

ntinu

ous S

ensit

ivity

Equa

tion

of A

rbitr

ary H

igh O

rder

C. Be

lley,

A. Ha

y, D.

Pelle

tier, É

cole

Polyt

echn

ique d

e Mon

tréal,

Mon

tréal,

Ca

nada

1530

hrs

AIAA-2

015-3

063

Desig

n opti

miza

tion o

f a hi

gh by

pass

ratio

fan r

otor a

gains

t wate

r inge

stion

S. Qiu

, D. Y

ang,

Aviat

ion In

dustr

y Corp

oratio

n of

China

(AVIC

), Sh

angh

ai, Ch

ina

1600

hrs

AIAA-2

015-3

064

Desig

n an

d Opt

imiza

tion

of a

Supe

rsonic

Bus

iness

Jet

F. Kiy

ici, S

. Arad

ag, T

OBB

Unive

rsity

of Ec

onom

ics an

d Tec

hnolo

gy, A

nkara

, Turk

ey

Wedn

esda

y, 24

June

201

520

5-CF

D-25

Turb

ulent

Flow

Simu

lation

s II

Emer

aldCh

aired

by: F

. VER

GINE

and L

. DUA

N, M

issou

ri Univ

ersity

of S

cienc

e and

Tech

nolog

y14

00 hr

sAIA

A-201

5-306

5In

vesti

gatio

n of

a Tw

injet

Confi

gura

tion

with

and w

ithou

t Flo

w Co

ntro

lK.

Gopa

raju,

D. G

aiton

de, S

. Bha

umik,

Oh

io St

ate U

nivers

ity, C

olumb

us, O

H

1430

hrs

AIAA-2

015-3

066

Nume

rical

Simula

tions

of

Single

and T

ande

m Wh

eels

for

Aero

dyna

mic L

oads

Pre

dictio

nS.

Spa

gnolo

, X. Z

hang

, Z. H

u, D.

Angla

nd,

Unive

rsity

of So

utham

pton,

South

ampto

n, Un

ited K

ingdo

m

1500

hrs

AIAA-2

015-3

067

RANS

Simu

lation

s of a

Chan

nel

Flow

with

a Ne

w Ve

locity

/Pre

ssure

-Gr

adien

t Mod

elS.

Poros

eva,

J. Co

lmen

ares,

Unive

rsity

of Ne

w Me

xico,

Albuq

uerqu

e, Alb

uque

rque,

NM; S

. Murm

an, N

ASA A

mes R

esea

rch

Cente

r, Moff

ett Fi

eld, N

M

1530

hrs

AIAA-2

015-3

068

High

-Fide

lity Co

mput

ation

al As

sessm

ent o

f the

Per

form

ance

of

a Ver

tical

Axis

Wind

Turb

ineJ.

Suda

ni, R.

Pras

ad, M

. Dam

odara

n, Ind

ian In

stitut

e of T

echn

ology

Ga

ndhin

agar,

Ahme

daba

d, Ind

ia

Wedn

esda

y, 24

June

201

520

6-F3

60-6

14

00 -

1630

hrs

The C

halle

nges

of G

reen

Avia

tion

Gran

d Ball

room

E

Mode

rator:

Mart

y Brad

ley, T

echn

ical F

ellow

, Boe

ing Co

mmerc

ial Ai

rplan

es

Pan

elists

:Ri

cky C

urra

nFa

culty

of Ae

rospa

ce En

ginee

ring

Delft

Unive

rsity

of Te

chno

logy

Jay E

. Dry

erDir

ector,

Adva

nced A

ir Veh

icles P

rogram

Offic

e (Ac

ting)

Aeron

autic

s Res

earch

Miss

ion D

irecto

rate

NASA

Hea

dqua

rters

Askin

Isikv

eren

Head

of V

isiona

ry Air

craft

Conc

epts

Bauh

aus L

uftfah

rt

Leslie

Perki

nsDir

ector

, Ene

rgy O

ffice

Air F

orce

Res

earch

Labo

rato

ry

Jean

ne Yu

Envir

onme

ntal D

irecto

rBo

eing C

omme

rcial

Airpla

nes

Wedn

esda

y, 24

June

201

520

7-F3

60-7

/CAS

E-7

1400

- 17

30 h

rsSy

stem

Comp

lexity

: Go

vern

ment

Nee

ds an

d Pra

ctica

l Res

earch

Res

ults

Gran

d Ball

room

D

This

pane

l is ar

range

d arou

nd tw

o app

licatio

n dom

ains -

defen

se sy

stems

and u

nman

ned a

ir sys

tems i

n the

natio

nal a

irspa

ce - a

nd tw

o eng

ineeri

ng pr

actic

e nee

ds - r

apid

syste

m de

velop

ment

and n

ew th

eory

comp

lex sy

stems

engin

eerin

g. Th

e exp

ectat

ion is

that

the au

dienc

e wi

ll tak

e awa

y both

a co

gent

statem

ent o

f nee

ds an

d cha

lleng

es al

ong w

ith a

conc

ise de

script

ion of

new

techn

iques

that

show

prom

ise to

mee

t the

state

d nee

ds an

d cha

lleng

es.

Keyn

ote S

peak

erKr

isten

Bald

win

Princ

ipal D

eputy

DAS

D (S

E), D

epart

ment

of De

fense

Mode

rators

: Fran

k Sern

a, Pri

ncipa

l Dire

ctor, S

trateg

ic Ini

tiativ

es, D

raper

Labo

ratory

and A

nna-M

aria M

cGow

an, A

erona

utics

Rese

arch D

irecto

rate,

NASA

Lang

ley Re

searc

h Cen

ter

Pan

elists

:Je

ffrey

P. H

ollan

dDir

ector

of Re

searc

h and

Dev

elopm

ent a

nd Ch

ief S

cienti

stU.

S. Ar

my Co

rps of

Engin

eers

David

Ney

land

Cons

ultan

t

94

Wedn

esda

y, 24

June

201

520

8-FD

-23

Unste

ady W

ing A

erod

ynam

ics II

IGo

veno

rs Le

cture

Hall

Chair

ed by

: S. Y

ARUS

EVYC

H, U

nivers

ity of

Wate

rloo a

nd H

. LUO

, Van

derbi

lt Univ

ersity

1400

hrs

AIAA-2

015-3

069

Nume

rical

Simula

tion

of Ci

rcular

Cy

linde

rs an

d Wing

Secti

ons i

n Un

stead

y Mot

ionA.

Gros

s, J.

Zhou

, New

Mex

ico S

tate

Unive

rsity,

Las C

ruces

, NM;

H. F

asel,

Un

iversi

ty of

Arizo

na, T

ucso

n, AZ

1430

hrs

AIAA-2

015-3

070

The e

ffect

of th

e blad

e cho

rd le

ngth

on

the a

erod

ynam

ics of

the M

AV

scale

cyclo

idal p

rope

ller u

nder

ho

verin

g sta

tus

Y. Hu

, H. Z

hang

, Nort

hwes

tern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

1500

hrs

AIAA-2

015-3

071

Unste

ady T

hick A

irfoil

Aero

dyna

mics:

Ex

perim

ents,

Comp

utatio

n, an

d Th

eory

D. Gre

enbla

tt, Tec

hnion

--Israe

l Instit

ute of

Tec

hnolo

gy, Ha

ifa, Is

rael; C

. Rum

sey, N

ASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA;

H. Mu

eller-V

ahl, T

echnio

n--Isr

ael In

stitute

of

Techn

ology,

Haifa

, Israe

l; C. S

tangfe

ld,

Techn

ical U

nivers

ity of

Berlin

, Berl

in, Ge

rman

y

1530

hrs

AIAA-2

015-3

072

Impa

ct of

a Vo

rtica

l Gus

t on

the

Aero

dyna

mics

of a

Finite

Asp

ect-

Ratio

Wing

R. Go

rdnier

, M. V

isbal,

Air F

orce R

esea

rch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH

1600

hrs

AIAA-2

015-3

073

Trans

ient E

ncou

nter

s of a

NA

CA00

12 W

ing w

ith a

Strea

mwise

-Orie

nted

Vorte

xD.

Garm

ann,

M. V

isbal,

Air F

orce R

esea

rch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH

1630

hrs

AIAA-2

015-3

074

Flow

Visua

lizat

ion an

d For

ce

Meas

urem

ents

on A

cceler

ated

Re

volvi

ng Fl

at P

lates

at Lo

w Re

ynold

s Num

bers

M. Pe

rcin,

B. va

n Oud

heus

den,

Delft

Unive

rsity

of Te

chno

logy,

Delft,

The

Nethe

rland

s

Wedn

esda

y, 24

June

201

520

9-FD

-24

Boun

dary

Laye

r Tra

nsitio

n: R

ecep

tivity

and C

ontro

lSa

pphir

eCh

aired

by: E

. WHI

TE, T

exas

A&M

Unive

rsity

and A

. CHO

U, N

ASA L

angle

y Res

earch

Cente

r14

00 hr

sAIA

A-201

5-307

5On

the E

ffect

of Sm

all St

eps o

n Pr

e-tra

nsitio

nal S

tream

wise

Elon

gated

Str

eaks

A. Se

scu, M

ississ

ippi S

tate U

nivers

ity,

Missi

ssipp

i Stat

e, MS

; M. A

fsar, I

mperi

al Co

llege

Lond

on, L

ondo

n, Un

ited K

ingdo

m;

V. Sa

ssanis

, Miss

issipp

i Stat

e Univ

ersity

, Mi

ssissi

ppi S

tate,

MS

1430

hrs

AIAA-2

015-3

076

Time-

Freq

uenc

y Ana

lysis

of

Boun

dary

Laye

r Ins

tabil

ities

Gene

rated

by Fr

eestr

eam

Lase

r Pe

rturb

ation

sA.

Chou

, NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A; S.

Sch

neide

r, Purd

ue

Unive

rsity,

Wes

t Lafa

yette

, IN

1500

hrs

AIAA-2

015-3

077

Nume

rical

Simula

tion o

f Hyp

erso

nic

Boun

dary

-Laye

r Ins

tabil

ity in

a Re

al Ga

s with

Two-

Dime

nsion

al Su

rface

Rou

ghne

ssC.

Morte

nsen

, X. Z

hong

, Univ

ersity

of

Califo

rnia,

Los A

ngele

s, Lo

s Ang

eles,

CA

1530

hrs

AIAA-2

015-3

078

Lead

ing-Ed

ge R

ecep

tivity

to

Acou

stic W

aves

for H

igh-S

peed

Flo

ws ov

er a

Blun

t Wed

geA.

Cerm

inara,

N. S

andh

am, U

nivers

ity

of So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1600

hrs

AIAA-2

015-3

079

Swep

t-Wing

Bou

ndar

y-La

yer

Rece

ptivi

ty to

Stea

dy Fr

ee-S

tream

Di

sturb

ance

sH.

Kurz,

M. K

loker,

Univ

ersity

of S

tuttga

rt,

Stutt

gart,

Germ

any

1630

hrs

AIAA-2

015-3

080

Delay

ing tr

ansit

ion in

rota

ting

boun

dary

-laye

r flow

sP.

Griffi

ths, U

nivers

ity of

Birm

ingha

m,

Birmi

ngha

m, U

nited

King

dom;

S. G

arrett

, Un

iversi

ty of

Leice

ster, L

eices

ter, U

nited

Kin

gdom

; S. S

tephe

n, Un

iversi

ty of

New

South

Wale

s, Sy

dney

, Aus

tralia

Wedn

esda

y, 24

June

201

521

0-FD

-25

1400

- 17

30 h

rsFlo

w Co

ntro

l Tec

hnolo

gies -

Bar

riers/

Chall

enge

s to T

ech

Trans

ition

Topa

z

Chair

ed by

: G. D

ALE,

Air Fo

rce Re

searc

h Lab

orator

y and

D. S

MITH

, Air F

orce O

ffice o

f Scie

ntific

Rese

arch A

FOSR

The s

essio

n will

focus

on th

e hurd

les to

tran

sition

ing flo

w co

ntrol

techn

ology

to pl

atform

s bas

ed on

majo

r cas

e stud

ies. P

anel

memb

ers w

ill pre

sent

lesso

ns le

arned

and r

ecom

mend

ation

s on fl

ow co

ntrol

techn

ology

tran

sition

s (ap

prox.

15 m

inutes

each

), co

verin

g both

succe

ssful

and u

nsuc

cessf

ul tra

nsitio

ns. A

mod

erated

Q&A

sessi

on w

ill fol

low th

e pres

entat

ions.

Sessi

on ou

tcome

is in

tende

d to o

ffer a

path

forwa

rd to

foster

ing m

ore te

chno

logy t

ransit

ion fo

r flow

contr

ol.Mo

derat

or: Lo

u Catt

afesta

, Emi

nent

Scho

lar an

d Prof

esso

r, Flor

ida S

tate U

nivers

ity

Pane

lists:

Edwa

rd W

halen

Flow

Contr

ol Ac

tuatio

n Man

ager

Boein

g Res

earch

and T

echn

ology

Rich

ard W

lezien

Profes

sor a

nd Ch

air of

Aeros

pace

Engin

eerin

gIow

a Stat

e Univ

ersity

Rona

ld Jo

slin

Progra

m Of

ficer

Offic

e of N

aval

Rese

arch

Fay C

ollier

Projec

t Man

ager

NASA

Envir

onme

ntally

Resp

onsib

le A v

iation

95

Wedn

esda

y, 24

June

201

521

1-FD

-26

Turb

ulenc

e Sim

ulatio

nsSe

nato

rs Le

cture

Hall

Chair

ed by

: P. S

PALA

RT, B

oeing

Comm

ercial

Airpl

anes

and E

. JOH

NSEN

, Univ

ersity

of M

ichiga

n14

00 hr

sAIA

A-201

5-308

1A

nume

rical

study

of tu

rbule

nce

in bo

xes w

ith n

o-sli

p wall

s and

of

vary

ing vo

lume-

to-su

rface

ratio

sE.

John

sen,

Unive

rsity

of Mi

chiga

n, An

n Arbo

r, Ann

Arbo

r, MI;

P. Mo

vahe

d, Un

iversi

ty of

Illino

is, U

rbana

-Cham

paign

, Ur

bana

, IL;

D. D

owlin

g, Un

iversi

ty of

Mich

igan,

Ann A

rbor, A

nn Ar

bor, M

I

1430

hrs

AIAA-2

015-3

082

Surfa

ce R

ough

ness

Effe

cts in

Hy

perso

nic Tu

rbule

nt B

ound

ary

Laye

rsJ.

Pogg

ie, Ai

r Forc

e Res

earch

Labo

ratory

, W

right-

Patte

rson A

FB, O

H

1500

hrs

AIAA-2

015-3

083

Appli

catio

n of

the W

ray-

Agar

wal

Mode

l to C

ompr

essib

le Flo

wsT.

Wray

, R. A

garw

al, W

ashin

gton

Unive

rsity

in St

. Lou

is, S

t. Lo

uis, M

O

1530

hrs

AIAA-2

015-3

084

Tetra

hedr

al-Me

sh Si

mulat

ion of

Tu

rbule

nt Fl

ows w

ith th

e Spa

ce-

Time C

onse

rvat

ive Sc

heme

sC.

Chan

g, NA

SA La

ngley

Rese

arch C

enter

, Ha

mpton

, VA;

B. Ve

nkata

chari

, Nati

onal

Institu

te of

Aeros

pace

, Ham

pton,

VA; G

. Ch

eng,

Unive

rsity

of Ala

bama

, Tus

caloo

sa,

Tusca

loosa

, AL

Wedn

esda

y, 24

June

201

521

2-MA

O-6

Emer

ging M

ethod

s II

Madr

idCh

aired

by: B

. MES

MER,

Unive

rsity

of Ala

bama

and J

. HICK

EN, R

ensse

laer P

olytec

hnic

Institu

te14

00 hr

sAIA

A-201

5-308

5In

creas

ing Fe

asibi

lity of

the S

elf-

Orga

nizing

Map

as a

Desig

n To

ol th

roug

h a N

ovel

Conv

erge

nce

Heur

istic

T. Ric

hards

on, E

. Wine

r, Iow

a Stat

e Un

iversi

ty, Am

es, I

A

1430

hrs

AIAA-2

015-3

086

Inco

rpor

ation

of Co

uplin

g Stre

ngth

Mo

dels

in a V

alue-

base

d Sys

tems

Engin

eerin

g fra

mewo

rk fo

r op

timiza

tion

H. Ka

nnan

, E. T

ibor, I

owa S

tate U

nivers

ity,

Ames

, IA;

B. M

esme

r, Univ

ersity

of

Alaba

ma, H

untsv

ille, H

untsv

ille, A

L; C.

Bloeb

aum,

Iowa

Stat

e Univ

ersity

, Ame

s, IA

1500

hrs

AIAA-2

015-3

087

SUAV

E: An

Ope

n-So

urce

En

viron

ment

for M

ulti-F

idelity

Co

ncep

tual

Vehic

le De

sign

T. Lu

kacz

yk, A

. Wen

dorff

, M. C

olonn

o, T.

Econ

omon

, J. A

lonso

, Stan

ford U

nivers

ity,

Stan

ford,

CA; T

. Orra

, Emb

raer, S

ão Jo

sé

dos C

ampo

s, Br

azil;

et al.

1530

hrs

AIAA-2

015-3

088

A Fu

ll-Sp

ace M

ethod

with

Mat

rix

Aggr

egat

es fo

r Stre

ss-Co

nstra

ined

Struc

tura

l Opt

imiza

tion

G. Ke

nned

y, Ge

orgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1600

hrs

AIAA-2

015-3

089

Redu

cing I

nduc

ed D

rag a

nd

Mane

uver

Load

s by A

ctive

Ae

roela

stic A

ltera

tion

J. Lin

, Con

trol R

esea

rch Co

rporat

ion,

Lexin

gton,

MA

1630

hrs

AIAA-2

015-3

090

Integ

rated

Mult

idisci

plina

ry A

ircra

ft De

sign

Proc

ess S

uppo

rted b

y a

Dece

ntra

l MDO

Fram

ewor

kF.

Daou

d, S.

Dein

ert, R

. Maie

rl, Ö.

Pe

tersso

n, Air

bus,

Manc

hing,

Germ

any

Wedn

esda

y, 24

June

201

521

3-MA

O-7

Meta

mode

ling I

Manc

heste

rCh

aired

by: S

. CHO

WDH

URY,

Missi

ssipp

i Stat

e Univ

ersity

and P

. PIPE

RNI,

Bomb

ardier

Inc

1400

hrs

AIAA-2

015-3

091

A Me

thod

ology

to Cr

eate

Appr

oxim

ate M

odels

of Lo

ad

Enve

lopes

Und

er U

ncer

taint

yD.

Ranc

ourt,

S. G

hosh

, D. M

avris

, Geo

rgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA;

S.

Cogg

on, A

irbus

, Filto

n, Un

ited K

ingdo

m

1430

hrs

AIAA-2

015-3

092

Princ

ipal C

ompo

nent

Analy

sis As

sisted

Su

rroga

te Mo

delin

g (PC

A-SM

) of

Corre

lated

Load

s for

Unc

ertain

ty An

alysis

of D

esign

Load

Enve

lopes

S. Gh

osh, D

. Ran

court,

D. Ma

vris,

Georg

ia Ins

titute

of Tec

hnolo

gy, At

lanta,

GA; S

. Co

ggon

, Airb

us, Fi

lton,

Unite

d King

dom

1500

hrs

AIAA-2

015-3

093

Auxil

iary A

ir In

let D

esign

: Non

-Lin

earit

y, Su

rroga

te Mo

delin

g and

Opt

imiza

tion

Aspe

ctsA.

Lomb

ardi, L

. San

tos, E

mbrae

r, São

Jo

sé do

s Cam

pos,

Braz

il; D.

Ferra

ri, Te

chno

logica

l Insti

tute o

f Aero

nauti

cs (IT

A), S

ão Jo

sé do

s Cam

pos,

Braz

il

1530

hrs

AIAA-2

015-3

094

HDMR

-bas

ed Su

rroga

te Mo

del f

or

High

Dim

ensio

nal A

erod

ynam

ic De

sign

Prob

lems

Z. Ga

o, C.

Wang

, Nort

hwes

tern

Polyt

echn

ical U

nivers

ity, X

i’an,

China

1600

hrs

AIAA-2

015-3

095

A Se

quen

tial M

axim

in La

tin

Hype

rcube

Samp

ling M

ethod

And

Its

App

licat

ion to

Airc

raft

Desig

nD.

Wu,

T. Lo

ng, Y

. Wan

g, L.

Liu, B

eijing

Ins

titute

of Te

chno

logy,

Beijin

g, Ch

ina

96

Wedn

esda

y, 24

June

201

521

4-MS

T-9Ai

rfram

e Dam

age a

nd H

ealth

Mon

itorin

gTra

verti

neCh

aired

by: V

. MUK

HOPA

DHYA

Y, NA

SA La

ngley

Rese

arch C

enter

1400

hrs

AIAA-2

015-3

096

Comp

osite

Stru

cture

Mod

eling

an

d Ana

lysis

of A

dvan

ced A

ircra

ft Fu

selag

e Con

cept

sV.

Mukh

opad

hyay

, M. S

oroka

ch, N

ASA

Lang

ley Re

searc

h Cen

ter, H

ampto

n, VA

1430

hrs

AIAA-2

015-3

097

Nume

rical

Simula

tion

and A

nalys

is of

the A

ircra

ft Pil

ot Se

at Im

pact

Resis

tanc

eX.

Zhan

g, X.

Jinw

u, M.

Li, B

eihan

g Un

iversi

ty, B

eijing

, Chin

a; Y.

Ren,

Huna

n Un

iversi

ty, Ch

angs

ha, C

hina

1500

hrs

AIAA-2

015-3

098

Sens

itivity

Analy

sis to

ward

s Pr

obab

ilistic

Re-En

try M

odeli

ng of

Sp

acecr

aft an

d Spa

ce De

bris

P. Meh

ta, Un

iversit

y of S

trathc

lyde,

Glasgo

w,

Unite

d King

dom;

A. W

alker,

Los A

lamos

Na

tiona

l Labo

ratory

, Los

Alamo

s, NM

; M.

Brown

, Univ

ersity

of N

ew So

uth W

ales a

t the

Austr

alian D

efence

Force

Acad

emy,

Canb

erra,

Austr

alia; E

. Minis

ci, M.

Vasile

, Univ

ersity

of

Strath

clyde

, Glas

gow,

Unite

d King

dom

1530

hrs

AIAA-2

015-3

099

A Ve

hicle

Mana

geme

nt En

d-to

-End

Testi

ng an

d Ana

lysis

Platfo

rm fo

r Va

lidat

ion of

Miss

ion an

d Fau

lt Ma

nage

ment

Algo

rithm

s to R

educ

e Ri

sk fo

r NAS

A’s Sp

ace L

aunc

h Sy

stem

L. Tre

vino,

J. Pa

tterso

n, D.

Teare

, S.

John

son,

NASA

Mars

hall S

pace

Fligh

t Ce

nter, H

untsv

ille, A

L

Wedn

esda

y, 24

June

201

521

5-MS

T-10

Sens

or an

d Com

munic

ation

s Sys

tems

Wyeth

Chair

ed by

: J. Z

AMBR

ANO

and Y

. CHE

NG, A

VIC Co

mputi

ng Te

chniq

ue Re

searc

h Ins

titute

1400

hrs

AIAA-2

015-3

100

Simula

tion/

Optim

izatio

n Mo

delin

g fo

r Rob

ust S

atell

ite D

ata U

nit fo

r Ai

rbor

ne N

etwor

kJ.

Zamb

rano,

O. Ye

ste-O

jeda,

R. La

ndry,

Un

iversi

ty of

Québ

ec, M

ontré

al, Ca

nada

1430

hrs

AIAA-2

015-3

101

Para

llel I

mage

Deta

il Enh

ance

ment

Fo

r Rea

l-tim

e App

licat

ions

Y. Ch

eng,

W. N

iu, Av

iation

Indu

stry C

orpora

tion

of Ch

ina (A

VIC),

Xi’an

, Chin

a; Z.

Zhai,

No

rthwe

stern

Polyt

echnic

al Un

iversit

y, Xi’

an,

China

; L. Z

hang

, Avia

tion I

ndust

ry Co

rporat

ion

of Ch

ina (A

VIC),

Xi’an

, Chin

a

1500

hrs

AIAA-2

015-3

102

The K

ey al

gorit

hm R

esea

rch of

En

hanc

ed Vi

sion

Syste

m Ba

se on

Em

bedd

ed P

arall

el Co

mput

ingX.

Jian

chun

, Avia

tion I

ndus

try Co

rporat

ion

of Ch

ina (A

VIC),

Xi’an

, Chin

a

Wedn

esda

y, 24

June

201

521

6-TP

-10/

PDL-1

0Pla

sma C

ompu

tatio

nal M

ethod

s II

Miro

Chair

ed by

: K. S

TEPH

ANI,

Unive

rsity

of Illi

nois

at Ur

bana

-Cham

paign

and T

. MOE

LLER,

Unive

rsity

of Te

nnes

see S

pace

Insti

tute

1400

hrs

AIAA-2

015-3

103

Comp

utat

ional

Simula

tions

of TP

3 Ar

c-Jet

Facil

ity Fl

owT.

Gokc

en, E

RC, I

nc.,

Moffe

tt Fie

ld, CA

; J.

Balbo

ni, N

ASA A

mes R

esea

rch Ce

nter,

Moffe

tt Fie

ld, CA

; A. A

lunni,

ERC,

Inc.,

Moffe

tt Fie

ld, CA

1430

hrs

AIAA-2

015-3

104

Simula

tion o

f Plas

ma Fl

ow Co

ntrol:

A N

ew Co

mputa

tiona

lly Ef

ficien

t Ap

proa

chB.

Paren

t, Pusa

n Nati

onal

Unive

rsity,

Busan

, So

uth Ko

rea; S

. Mach

eret, P

urdue

Unive

rsity,

West

Lafay

ette,

IN; M

. Shn

eider,

Princ

eton

Unive

rsity,

Prince

ton, N

J

1500

hrs

AIAA-2

015-3

105

MG-lo

cal-P

CA M

ethod

for t

he

Redu

ction

of a

Collis

ional-

Radia

tive

Argo

n Pla

sma M

echa

nism

A. Be

llema

ns, T

. Mag

in, vo

n Kárm

án

Institu

te for

Fluid

Dyn

amics

, Rho

de-Sa

int-

Genè

se, B

elgium

; G. D

egrez

, A. P

arente

, Un

iversi

ty of

Brus

sels,

Brus

sels,

Belg

ium

1530

hrs

AIAA-2

015-3

106

Redu

ced-

Orde

r Mod

els of

Low-

Temp

erat

ure G

as D

ischa

rges

in

Glow

Mod

eE.

Cisne

ros, L

. Mas

sa, U

nivers

ity of

Texa

s, Arl

ington

, Arlin

gton,

TX

1600

hrs

AIAA-2

015-3

107

Enth

alpy C

hara

cteriz

ation

and

Asse

ssmen

t of C

oppe

r Cat

alysis

De

termi

natio

n in

Indu

ctive

ly Co

upled

Plas

ma Fa

cility

A. Vil

adeg

ut, vo

n Kárm

án In

stitut

e for

Fluid

Dyna

mics,

Rhod

e-Sain

t-Gen

èse,

Belgi

um

1630

hrs

AIAA-2

015-3

108

Nume

rical

Simula

tion

of Tw

o-Di

mens

ional

Struc

ture

of G

low

Disch

arge

in M

olecu

lar H

ydro

gen

S. S

urzhik

ov, D

. Stor

ozhe

v, Ru

ssian

Ac

adem

y of S

cienc

es, M

osco

w, Ru

ssia

97

Wedn

esda

y, 24

June

201

521

7-TP

-11

Aero

ther

mody

nami

cs III

Rose

ttaCh

aired

by: T

. LAM

, The

Aeros

pace

Corpo

ration

1400

hrs

AIAA-2

015-3

109

Glob

al Ae

rohe

ating

Mea

sure

ment

s of

Shoc

k-Sh

ock

Inter

actio

ns on

a Sw

ept C

ylind

erM.

Mas

on, S

. Berr

y, NA

SA La

ngley

Re

searc

h Cen

ter, H

ampto

n, VA

1430

hrs

AIAA-2

015-3

110

Aero

ther

mody

nami

c Cha

racte

ristic

s of

16-

22 k

m/s E

arth

Entry

C. Jo

hnsto

n, NA

SA La

ngley

Rese

arch

Cente

r, Ham

pton,

VA; A

. Bran

dis, E

RC,

Inc.,

Moffe

tt Fie

ld, CA

1500

hrs

AIAA-2

015-3

111

Radia

tive H

eatin

g on

the A

fter-

Body

of M

artia

n En

try Ve

hicles

A. Br

andis

, B. C

ruden

, T. W

hite,

D.

Saun

ders,

ERC,

Inc.,

Moffe

tt Fie

ld, CA

; C.

John

ston,

NASA

Lang

ley Re

searc

h Cen

ter,

Hamp

ton, V

A

1530

hrs

AIAA-2

015-3

112

Coup

led Fl

ow, R

adiat

ion, a

nd Ab

lation

Sim

ulatio

ns of

Atmo

sphe

ric En

try

Vehic

les us

ing th

e Hyb

rid St

atisti

cal

Narro

w Ba

nd M

odel

J. Sc

oggin

s, L.

Souca

sse, v

on Ká

rmán

Instit

ute

for Fl

uid Dy

nami

cs, Rh

ode-S

aint-G

enèse

, Be

lgium;

P. Riv

iere,

A. So

ufian

i, Écol

e Cen

trale

de Pa

ris, Pa

ris, Fr

ance;

T. M

agin,

von K

ármán

Ins

titute

for Fl

uid Dy

nami

cs, Rh

ode-S

aint-

Genè

se, Be

lgium

Wedn

esda

y, 24

June

201

521

8-NW

-7

1530

- 16

00 h

rsNe

twor

king C

offe

e Bre

akCh

antill

y Ball

room

East

Wedn

esda

y, 24

June

201

521

9-RL

A-2

1530

- 17

00 h

rsRi

sing L

eade

rs in

Aero

spac

e: Le

ader

ship

Exch

ange

/Spe

ed N

etwor

king

Metro

polita

n Ba

llroo

m

Get y

our q

uesti

ons a

nswe

red!

Senio

r Men

tors w

ill inc

lude:

Russ

Alth

ofCh

ief En

ginee

rRa

ytheo

n Miss

ile S

ystem

s

Cees

Bil

Profes

sor, R

oyal

Melbo

urne I

nstitu

te of

Tech

nolog

y

Dave

Bow

lesCe

nter D

irecto

r (Ac

ting)

NASA

Lang

ley Re

searc

h Cen

ter

Ed Fe

ltrop

Engin

eer S

pecia

listCe

ssna A

ircraf

t Com

pany

Susa

n Go

rton

Rotar

y Wing

Proje

ctNA

SA La

ngley

Rese

arch C

enter

Peter

Har

twich

Engin

eerin

g Man

ager

Boein

g Defe

nse,

Spac

e and

Sec

urity

Janic

e Kav

andi

Depu

ty Dir

ector

NASA

Glen

n Res

earch

Cente

r

Jeff

Jeps

onSe

nior M

ulti-D

iscipl

ined E

ngine

er I

Rayth

eon M

issile

Sys

tems

Sama

ntha

A. M

agill

Acad

emic

Affair

s and

Inclu

sion &

Dive

rsity

Hond

a Airc

raft C

ompa

ny

Sand

y Mag

nus

Exec

utive

Dire

ctor

AIAA

David

McB

ride

Cente

r Dire

ctor

NASA

Arms

trong

Fligh

t Res

earch

Cente

r

Char

les Sm

ithCe

nter D

irecto

r (Ac

ting)

NASA

Ames

Rese

arch C

enter

John

Valas

ekPro

fessor

/Dire

ctor, V

ehicle

Syste

ms &

Contr

ol La

borat

oryTe

xas A

&M U

nivers

ity

Wedn

esda

y, 24

June

201

522

0-LE

C-3

1630

- 17

30 h

rsAe

rody

nami

cs Aw

ard L

ectu

reCh

antill

y Ball

room

Wes

t

Still T

rying

to U

nders

tand A

ircraf

t Vort

ices

Russe

ll M. C

ummi

ngs

Profes

sor o

f Aero

nauti

csDe

partm

ent o

f Aero

nauti

csU.

S. Ai

r Forc

e Aca

demy

Wedn

esda

y, 24

June

201

522

1-LE

C-4

1730

- 18

30 h

rsAe

roac

ousti

cs Le

cture

Chan

tilly B

allro

om W

est

Fan B

roadb

and N

oise G

enera

tion a

nd Su

ppres

sion

Edma

ne En

viaAe

roaco

ustic

s Bran

chNA

SA G

lenn R

esea

rch Ce

nter

98

Wedn

esda

y, 24

June

201

522

2-LE

C-5

1730

- 18

30 h

rsTh

ermo

phys

ics A

ward

Lectu

reGr

and B

allro

om E

Aerod

ynam

ics an

d Hea

t Tran

sfer in

Gas T

urbine

Cooli

ng-Re

cent A

dvan

cesSu

mant

a Ach

arya

Ring C

hair &

Profe

ssor

Mech

anica

l Eng

ineeri

ng D

epart

ment

Unive

rsity

of Me

mphis

Wedn

esda

y, 24

June

201

522

3-BA

NQ-1

19

00 -

2030

hrs

Aero

acou

stics

Awar

ds R

ecep

tion

and B

anqu

etIm

peria

l Ball

room

The A

eroac

ousti

cs Aw

ards R

ecep

tion a

nd B

anqu

et wi

ll beg

in wi

th a c

ash b

ar so

cial p

eriod

at 1

900

hrs, f

ollow

ed by

the a

wards

cerem

ony a

nd ba

nque

t whe

re the

AIAA

and C

EAS

Aeroa

cous

tics A

wards

will

be pr

esen

ted.

The w

inner

of the

Aeroa

cous

tics S

tuden

t Pap

er Co

mpeti

tion a

lso w

ill be

reco

gnize

d. Ple

ase j

oin us

and c

elebra

te the

achie

veme

nts of

your

peers

.Tic

kets

will b

e ava

ilable

at on

site

as sp

ace i

s ava

ilable

.

Thur

sday

Thur

sday

, 25

June

201

522

4-SB

-4

0730

- 08

00 h

rsSp

eake

rs’ B

riefin

gSe

ssion

Roo

ms

Thur

sday

, 25

June

201

522

5-PL

NRY-4

08

00 -

0900

hrs

Plena

ry K

eyno

teCh

antill

y Ball

room

Wes

t

DHS’s

Persp

ective

s on C

ybers

ecurity

in Av

iation

Greg

ory J

. Tou

hill

Depu

ty As

sistan

t Sec

retary

for O

ffice o

f Cyb

ersec

urity

and C

ommu

nicati

ons

Depa

rtmen

t of H

omela

nd S

ecuri

ty

Thur

sday

, 25

June

201

522

6-AA

-31

Inter

ior N

oise

Edelw

eiss

Chair

ed by

: N. A

GARW

AL, B

oeing

Defe

nse,

Spac

e & S

ecuri

ty09

00 hr

sOr

al Pre

senta

tion

Poro

elasti

c Aco

ustic

Meta

Mat

erial

s (In

vited

)C.

Fulle

r, Virg

inia P

olytec

hnic

Institu

te an

d Stat

e Univ

ersity

, Blac

ksbu

rg, VA

1000

hrs

AIAA-2

015-3

113

Low

Freq

uenc

y Nois

e Red

uctio

n Us

ing P

oro-

Elasti

c Aco

ustic

Me

tama

terial

sA.

Slagle

, C. F

uller, V

irginia

Polyt

echnic

Ins

titute

and S

tate U

nivers

ity, Bl

acksbu

rg, VA

1030

hrs

AIAA-2

015-3

114

Identi

ficati

on of

sour

ces of

noise

in th

e ca

bin an

d the

defin

ition o

f the

loca

l pa

ssage

of so

und e

nerg

y thr

ough

fus

elage

based

on th

e resu

lts of

in-

flight

meas

urem

ents

of the

Supe

rjet

R. Ab

drashi

tov, S

ukho

i Civil

Aircr

aft Co

mpan

y, Mo

scow,

Russi

a; A.

Golub

ev, Ts

AGI,

Zhuk

ovsky

, Russ

ia

1100

hrs

AIAA-2

015-3

115

Fuse

lage E

xcita

tion

Durin

g Cru

ise

Fligh

t Con

dition

s: Me

asur

emen

t an

d Pre

dictio

n of

Pre

ssure

Poin

t Sp

ectra

A. Kla

bes,

M. H

err, C

. App

el, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Brau

nsch

weig,

Ge

rman

y; M.

Bou

haj, A

irbus

Ope

ration

s Gm

bH, H

ambu

rg, G

erman

y

1130

hrs

AIAA-2

015-3

116

Effe

ct of

pres

sure

grad

ients

on

turb

ulent

boun

dary

laye

r vor

tical

struc

ture

s and

wall

-pre

ssure

flu

ctuat

ions

M. Al

aoui,

X. G

loerfe

lt, Pa

ris In

stitut

e of

Tech

nolog

y, Pa

ris, F

rance

; O. C

ollery

, M.

Etche

ssaha

r, Airb

us, T

oulou

se, F

rance

1200

hrs

AIAA-2

015-3

117

Effe

ct of

pres

sure

grad

ients

on

turb

ulent

boun

dary

laye

r nois

e and

wa

ll-pr

essu

re fl

uctu

ation

sE.

Cohe

n, X.

Gloe

rfelt,

Paris

Insti

tute o

f Te

chno

logy,

Paris

, Fran

ce

99

Thur

sday

, 25

June

201

522

7-AA

-32

Jet N

oise M

easu

reme

nts I

IIFle

ur-d

e-lis

ACh

aired

by: D

. PAP

AMOS

CHOU

, Univ

ersity

of Ca

liforni

a Irvi

ne09

00 hr

sAIA

A-201

5-311

8In

stalle

d jet-

flap i

mping

emen

t to

nal n

oise

J. La

wren

ce, R

. Self

, Univ

ersity

of

South

ampto

n, So

utham

pton,

Unite

d Kin

gdom

0930

hrs

AIAA-2

015-3

119

Noise

mea

sure

ment

s of h

igh as

pect

ratio

distr

ibuted

exha

ust s

ystem

sJ.

Bridg

es, M

. Wern

et, N

ASA G

lenn

Rese

arch C

enter

, Clev

eland

, OH

1000

hrs

AIAA-2

015-3

120

Meas

urem

ents

and P

redic

tions

of

the N

oise f

rom

Thre

e-Str

eam

Jets

B. H

ende

rson,

S. Le

ib, N

ASA G

lenn

Rese

arch C

enter

, Clev

eland

, OH

1030

hrs

AIAA-2

015-3

121

Flow

Field

and A

cous

tic

Inve

stiga

tions

of th

e Lau

nch

Vehic

le En

viron

ment

durin

g Lift

-off

K. Na

taraja

n, L.

Venk

atakri

shna

n, Na

tiona

l Ae

rospa

ce La

borat

ories

, Ban

galor

e, Ind

ia

1100

hrs

AIAA-2

015-3

122

An Ex

perim

ental

Stud

y of C

oaxia

l Jets

Us

ing Ac

ousti

c PIV

and L

DA M

ethod

s (C

oJeN

)C.

Mead

, Aero

Acou

stics,

Ltd., E

lstead

, Unit

ed

Kingd

om; C

. Wrig

hton,

Qineti

Q, Fa

rnboro

ugh,

Unite

d King

dom;

K. Br

itchfor

d, Ro

lls-Ro

yce

Group

plc,

Derby

, Unit

ed Ki

ngdo

m

1130

hrs

AIAA-2

015-3

123

Expe

rimen

tal a

nd n

umer

ical s

tudy

of

the n

oise g

ener

ation

in an

ou

tflow

butte

rfly v

alve

A. Ch

auvin

, Y. P

asco

, M. S

anjos

e, G.

Lo

bel, A

. Mars

an, S

. More

au, U

nivers

ity of

Sh

erbroo

ke, S

herbr

ooke

, Can

ada;

et al.

Thur

sday

, 25

June

201

522

8-AA

-33

Jet N

oise M

odeli

ng II

Fleur

-de-

lis B

Chair

ed by

: C. B

ROW

N, N

ASA G

lenn R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-3

124

Nonli

near

inter

actio

n an

alysis

of

subs

onic

jet in

stabil

ities w

ith fo

rced

eigen

mode

s usin

g PSE

M. It

asse

, J. B

razier

, O. L

éon,

G. Ca

salis,

ON

ERA,

Toulo

use,

Franc

e

0930

hrs

AIAA-2

015-3

125

Linea

r Sta

bility

Impli

catio

ns of

Me

an Fl

ow Va

riatio

ns in

Turb

ulent

Je

ts Iss

uing f

rom

Serra

ted N

ozzle

sA.

Sinha

, Ind

ian In

stitut

e of T

echn

ology

Bo

mbay

, Mum

bai, I

ndia;

T. Co

lonius

, Ca

liforni

a Ins

titute

of Te

chno

logy,

Pasa

dena

, CA

1000

hrs

AIAA-2

015-3

126

On th

e Com

paris

on of

the L

ong

Pene

tratio

n Mo

de (L

PM) S

uper

sonic

Co

unter

flowi

ng Je

t to t

he

Supe

rsonic

Scre

ech

Jet

R. Fa

rr, NA

SA M

arsha

ll Spa

ce Fl

ight

Cente

r, Hun

tsville

, AL;

C. Ch

ang,

NASA

La

ngley

Rese

arch C

enter

, Ham

pton,

VA; J

. Jo

nes,

AI Sig

nal R

esea

rch, I

nc.,

Hunts

ville,

AL

; N. D

ough

erty,

ERC,

Inc.,

Hunts

ville,

AL

1030

hrs

AIAA-2

015-3

127

Theo

retic

al Mo

dellin

g Of

Broa

dban

d Sho

ck A

ssocia

ted N

oise

in As

ymme

tric J

etsA.

Kalya

n, S.

Karab

asov

, Que

en M

ary

Unive

rsity

of Lo

ndon

, Lon

don,

Unite

d Kin

gdom

1100

hrs

AIAA-2

015-3

128

Empir

ical M

odels

for t

he Sh

ieldin

g an

d Refl

ectio

n of

Jet M

ixing

Nois

e by

a Su

rface

C. Br

own,

NASA

Glen

n Res

earch

Cente

r, Cle

velan

d, OH

1130

hrs

AIAA-2

015-3

129

Comp

utatio

nal m

odell

ing of

jet-w

ing

intera

ction

: the e

ffect

of as

ymme

tries

fro

m the

jet in

flow

cond

itions

and

the w

ingV.

Semi

letov,

Que

en M

ary Un

iversit

y of

Lond

on, L

ondo

n, Un

ited K

ingdo

m; P.

Yako

vlev,

North

-Easte

rn Fe

deral

Unive

rsity,

Yaku

tsk,

Russi

a; S.

Karab

asov,

Quee

n Mary

Unive

rsity

of Lo

ndon

, Lon

don,

Unite

d King

dom;

G.

Faran

osov,

V. Ko

piev,

TsAGI,

Mosc

ow, R

ussia

1200

hrs

AIAA-2

015-3

130

Refra

ction

Effe

ct in

Corre

lation

Mo

del o

f Qua

drup

ole N

oise S

ource

s in

Turb

ulent

Jet

V. Ko

piev,

S. Ch

ernys

hev,

TsAGI

, Mos

cow,

Ru

ssia

Thur

sday

, 25

June

201

522

9-AA

-34

CAA

Nume

rical

Tech

nique

s III

Inve

rnes

sCh

aired

by: S

. ARU

NAJAT

ESAN

, San

dia N

ation

al La

bs09

00 hr

sAIA

A-201

5-313

1A

study

of ac

cura

cy on

num

erica

l me

thod

s for

non

unifo

rm m

eshe

s (In

vited

)F.

Hu, O

ld Do

minio

n Univ

ersity

, Norf

olk,

VA; A

. Fern

ando

, Norf

olk S

tate U

nivers

ity,

Norfo

lk, VA

0930

hrs

AIAA-2

015-3

132

Aero

acou

stic C

alcula

tions

of th

e 30

P30N

High

-lift A

irfoil

using

Hyb

rid

RANS

/LES

meth

ods:

Mode

ling a

nd

Grid

Reso

lution

Effec

tsM.

Terra

col, E

. Man

oha,

ONER

A, Ch

âtillon

, Fra

nce; M

. Mura

yama

, K. Y

amam

oto, J

apan

Ae

rospa

ce Ex

plorat

ion Ag

ency

(JAXA

), Tok

yo,

Japan

1000

hrs

AIAA-2

015-3

133

A dir

ect-h

ybrid

meth

od fo

r co

mput

ation

al ae

roac

ousti

csM.

Sch

lottke

, H. C

heng

, V. P

auz,

M.

Meink

e, W.

Sch

roede

r, RW

TH Aa

chen

Un

iversi

ty, Aa

chen

, Germ

any

1030

hrs

AIAA-2

015-3

134

Hybr

id Ma

cCor

mack

-type

Sche

mes

for C

ompu

tatio

nal A

eroa

cous

tics

S. Ya

zdan

i, D. H

ixon,

Unive

rsity

of To

ledo,

Toled

o, OH

1100

hrs

AIAA-2

015-3

135

Deve

lopme

nt of

comp

ressib

le lar

ge-

eddy

simula

tions

comb

ining

high

-or

der s

chem

es an

d wall

mod

eling

S. Le

Bras,

CERF

ACS,

Toulou

se, Fr

ance;

H.

Denia

u, ON

ERA,

Toulou

se, Fr

ance;

C. Bo

gey,

École

Centr

ale de

Lyon

, Ecul

ly, Fra

nce; G

. Da

viller,

CERF

ACS,

Toulou

se, Fr

ance

100

Thur

sday

, 25

June

201

523

0-AA

-35

Airfr

ame N

oise I

VLa

lique

Chair

ed by

: T. V

AN D

E VEN

, Gulf

strea

m09

00 hr

sAIA

A-201

5-313

6In

fluen

ce of

Span

wise

Bou

ndar

y Co

nditio

ns on

Slat

Nois

e Sim

ulatio

nsD.

Lock

ard, M

. Cho

udha

ri, P.

Bunin

g, NA

SA

Lang

ley Re

searc

h Cen

ter, H

ampto

n, VA

0930

hrs

AIAA-2

015-3

137

LEISA

2: an

expe

rimen

tal da

tabas

e for

the

valid

ation

of nu

meric

al pr

edict

ions

of sla

t uns

teady

flow

and n

oise

E. Ma

noha

, ONE

RA, C

hâtillo

n, Fra

nce; M

. Po

tt-Polle

nske,

Germ

an Ae

rospa

ce Ce

nter

(DLR

), Bra

unsch

weig,

Germ

any

1000

hrs

AIAA-2

015-3

138

Expe

rimen

tal s

tudy

of th

e effe

ct of

a s

mall 2

D ex

cresce

nce p

laced

on

the s

lat co

ve su

rface

of an

airfo

il on

its a

cous

tic n

oise

F. Am

aral, D

. Sou

za, C

. Pag

ani, M

. Me

deiro

s, Un

iversi

ty of

São P

aulo,

São

Jo

sé do

s Cam

pos,

Braz

il

1030

hrs

AIAA-2

015-3

139

Slat N

oise P

redic

tion

using

Hyb

rid

RANS

-LES m

ethod

s on

Struc

ture

d an

d Uns

tructu

red G

rids

N. As

hton,

Unive

rsity

of Ma

nche

ster,

Manc

heste

r, Unit

ed Ki

ngdo

m; A.

Wes

t, CD

-adap

co, L

ondo

n, Un

ited K

ingdo

m; F.

Me

ndon

ca, S

elf, L

ondo

n, Un

ited K

ingdo

m

1100

hrs

AIAA-2

015-3

140

Larg

e-Sc

ale St

udies

on Sl

at N

oise

Redu

ction

M. H

err, M

. Pott

-Polle

nske

, R. E

wert,

B.

Dirk

, J. S

iebert

, J. D

elfs,

Germ

an

Aeros

pace

Cente

r (DL

R), B

rauns

chwe

ig,

Germ

any;

et al.

1130

hrs

AIAA-2

015-3

141

Study

on N

oise G

ener

ation

from

Sla

t Tra

cks U

sing a

High

-Lift

Wing

Mo

del

M. M

uraya

ma, Y

. Yok

okaw

a, Y.

Ito, K

. Ya

mamo

to, T.

Taka

ishi, H

. Ura,

Japa

n Ae

rospa

ce Ex

plorat

ion Ag

ency

(JAX

A),

Mitak

a, Ja

pan

1200

hrs

AIAA-2

015-3

142

On th

e Nois

e Gen

erat

ion of

Kr

uege

r Lea

ding E

dge D

evice

sM.

Pott-P

ollen

ske,

J. W

ild, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Brau

nsch

weig,

Ge

rman

y

Thur

sday

, 25

June

201

523

1-AA

-36

Gene

ral A

cous

tics I

IIOb

elisk

ACh

aired

by: C

. SCH

RAM

0900

hrs

AIAA-2

015-3

143

Expe

rimen

tal A

pplic

ation

of

Aero

acou

stic T

ime-

Reve

rsal

A. Mi

mani,

D. M

oreau

, C. D

oolan

, Un

iversi

ty of

Adela

ide, A

delai

de, A

ustra

lia

0930

hrs

AIAA-2

015-3

144

Expe

rimen

tal I

nves

tigat

ion of

the

Unste

ady P

ressu

re on

a Hy

drof

oil

due t

o the

Inge

stion

of Tu

rbule

nce

and H

ydro

-elas

tic M

otion

M. Ca

tlett,

J. An

derso

n, Na

val S

urfac

e Wa

rfare

Cente

r, Wes

t Beth

esda

, MD

1000

hrs

AIAA-2

015-3

145

An Ex

perim

enta

l Stu

dy of

Co

mpos

ite M

ater

ials f

or th

e Des

ign

of Q

uiet U

AVs

J. Ca

llicoa

t, R.

Gaeta

, J. J

acob

, Okla

homa

St

ate U

nivers

ity, S

tillwa

ter, O

K

1030

hrs

AIAA-2

015-3

146

On th

e Rele

vanc

e of C

onve

ction

Ef

fects

for a

Lase

r-Gen

erat

ed

Soun

d Sou

rceK.

Rossi

gnol,

J. D

elfs,

L. Ro

ssian

, F.

Bode

n, Ge

rman

Aeros

pace

Cente

r (DL

R),

Brau

nsch

weig,

Germ

any

1100

hrs

AIAA-2

015-3

147

Flow

Noise

Gen

erat

ion of

Cylin

ders

with

Soft

Poro

us Co

ver

T. Ge

yer, E

. Sarr

adj, G

. Hero

ld,

Bran

denb

urg U

nivers

ity of

Tech

nolog

y, Co

ttbus

, Germ

any

1130

hrs

AIAA-2

015-3

148

An ex

perim

enta

l inve

stiga

tion

of

wall p

ressu

re fl

uctu

ation

s ben

eath

pr

essu

re gr

adien

tsE.

Salze

, C. B

ailly,

O. M

arsde

n, E.

Jond

eau,

D. Ju

ve, É

cole

Centr

ale de

Lyon

, Ec

ully,

Franc

e

Thur

sday

, 25

June

201

523

2-AC

D-6

0900

- 12

00 h

rsCo

ncep

tual

Aircr

aft D

esign

Wor

king G

roup

(CAD

WG21

) Pan

elWy

eth

Chair

ed by

: W. A

NEMA

AT, D

ARco

rporat

ion an

d T. T

AKAH

ASHI

, Ariz

ona S

tate U

nivers

ity

The N

eed o

f Com

munit

y-Acce

pted P

ublic

Doma

in /

Open

Sourc

e Sizi

ng Co

des

P

aneli

sts:

Clif D

avis

Lock

heed

Mart

in Ae

ronau

tics

Jaso

n We

lstea

dNA

SA La

ngley

Joaq

uim M

artin

sUn

iversi

ty of

Mich

igan

Mark

Pag

eDZ

YNE T

echn

ologie

sSte

ve K

omad

inaNo

rthrop

-Grum

man

Rob M

cDon

aldCa

lPoly

Thur

sday

, 25

June

201

523

3-AP

A-25

Appli

ed CF

D &

Nume

rical

Corre

lation

s with

Expe

rimen

tal D

ata I

IISte

mmon

s BCh

aired

by: K

. ABD

OL-HA

MID,

NAS

A Lan

gley R

esea

rch Ce

nter a

nd A.

SCL

AFAN

I, Bo

eing E

ngine

ering

Ope

ration

s & Te

chno

logy

0900

hrs

AIAA-2

015-3

149

Time-A

ccura

te Un

stead

y Pres

sure

Lo

ads S

imula

ted fo

r the

Spac

e Lau

nch

Syste

m at

Wind

Tunn

el Co

nditio

nsS.

Alter,

G. Br

auckm

ann,

W. Kl

eb, C

. Stre

ett,

C. Gla

ss, D.

Schu

ster, N

ASA L

angle

y Rese

arch

Cente

r, Ham

pton,

VA

0930

hrs

AIAA-2

015-3

150

Cont

inuou

s Rad

ial Je

t in

Annu

lar

Cros

s-flow

P. Ra

jput,

I. Ka

lkhora

n, NY

U Po

lytec

hnic

Scho

ol of

Engin

eerin

g, Br

ookly

n, NY

1000

hrs

AIAA-2

015-3

151

Simula

tion

of a

Flapp

ing W

ing U

AV

using

a Co

upled

CFD-

Cont

rol T

ool

J. Ge

der, R

. Ram

amurt

i, K. V

iswan

ath, N

aval

Resea

rch La

borat

ory, W

ashing

ton, D

C

1030

hrs

AIAA-2

015-3

152

Outpu

t-Bas

ed Ad

aptiv

e Mesh

ing

Appli

ed to

Spac

e Lau

nch S

ystem

Bo

oster

Sepa

ratio

n Ana

lysis

D. Da

lle, Sc

ience

and T

echno

logy C

orpora

tion,

Moffe

tt Field

, CA;

S. Ro

gers,

NAS

A Ame

s Re

search

Cente

r, Moff

ett Fi

eld, C

A

1100

hrs

AIAA-2

015-3

153

Impr

ovem

ent o

f CFD

resu

lts of

NAS

A CR

M by

on-lin

e mesh

defor

matio

n us

ing m

odal

analy

sis of

a wi

ngP. V

rchota

, A. P

racha

r, Aero

space

Resea

rch an

d Tes

t Esta

blishm

ent, P

rague

, Cze

ch Re

public

101

Thur

sday

, 25

June

201

523

4-AP

A-26

Unma

nned

, Bio-

Insp

ired,

Solar

Pow

ered

Aer

ial Ve

hicle

Desig

ns II

Carp

enter

Ball

room

Chair

ed by

: M. O

L, US

Air F

orce R

esea

ch La

borat

ory an

d A. M

ITTAL

, The

Univ

ersity

of Te

nnes

see a

t Cha

ttano

oga

0900

hrs

AIAA-2

015-3

154

Dyna

mica

l Cha

racte

rizat

ion of

a Bi

o-In

spire

d Wing

with

Pas

sively

Ac

tuat

ed Ed

ges

C. Pla

nck,

F. Sia

la, J.

Libu

rdy, O

regon

St

ate U

nivers

ity, C

orvall

is, O

R

0930

hrs

AIAA-2

015-3

155

Nume

rical

Simula

tion

of a

Flapp

ing

Wing

in A

nsys

-Flue

nt B

ased

on th

e Fr

uit Fl

y Wing

Kine

matic

sB.

Niet

o, X.

Alfon

so, K

. Bas

to, J.

Esco

bar,

Unive

rsity

of Sa

n Bue

nave

ntura,

Bog

ota,

Colom

bia

1000

hrs

AIAA-2

015-3

156

Aero

dyna

mics

of So

uthe

rn H

awke

r Dr

agon

fly: A

eshn

a cya

nea

S. S

rigrar

om, C

. Thip

yopa

s, Ka

setsa

rt Un

iversi

ty, B

angk

ok, T

haila

nd

1030

hrs

AIAA-2

015-3

157

Deve

lopme

nt an

d Ana

lysis

of G

ull

Insp

ired U

AV Fl

appin

g Wing

D. Ku

mar, T

. Goy

al, S

. Vem

uri, P

. Moh

ite,

S. Ka

mle,

Indian

Insti

tute o

f Tec

hnolo

gy

Kanp

ur, Ka

npur,

India

1100

hrs

AIAA-2

015-3

158

Deve

lopme

nt an

d Aer

o-str

uctu

ral

Analy

sis of

Ligh

t and

Stro

ng

Carb

on Fi

ber-C

NT/P

P Hu

mming

bird

Insp

ired M

AV W

ings

D. Ku

mar, S

. Kum

ar, T.

Goy

al, P.

Moh

ite,

S. Ka

mle,

Indian

Insti

tute o

f Tec

hnolo

gy

Kanp

ur, Ka

npur,

India

Thur

sday

, 25

June

201

523

5-AP

A-27

Airfo

il/Wi

ng/C

onfig

urat

ion A

erod

ynam

icsSte

mmon

s CCh

aired

by: A

. MCC

OMAS

, TLG

Aeros

pace

and J

. GUG

LIELM

O, B

oeing

Defe

nse,

Spac

e & S

ecuri

ty09

00 hr

sAIA

A-201

5-315

9Im

prov

ed St

all P

redic

tion

for

Swep

t Wing

s Usin

g Low

-Ord

er

Aero

dyna

mics

P. Ho

sanga

di, R.

Paul,

A. Go

palar

athna

m,

North

Carol

ina St

ate Un

iversit

y, Ra

leigh,

NC

0930

hrs

AIAA-2

015-3

160

Mode

ling a

nd P

redic

tion

of

the C

rossfl

ow Tr

ansit

ion U

sing

Trans

ition

Trans

port

Equa

tions

J. Sa

, S. P

ark, K

onku

k Univ

ersity

, Seo

ul,

South

Korea

; K. C

ho, K

orea U

nivers

ity

of Sc

ience

and T

echn

ology

, Dae

jeon,

South

Korea

; K. J

ung,

Agen

cy fo

r Defe

nse

Deve

lopme

nt, D

aejeo

n, So

uth Ko

rea

1000

hrs

AIAA-2

015-3

161

On th

e res

ulting

aero

dyna

mic

loss o

f com

binat

ions o

f loc

alize

d su

rface

roug

hnes

s pat

ches

on a

turb

ine bl

ade

P. Gil

ge, K

. Mull

eners

, Leib

niz U

nivers

ity,

Hann

over,

Germ

any

1030

hrs

AIAA-2

015-3

162

Aero

-Pro

pulsi

ve Co

uplin

g of a

n Em

bedd

ed, D

istrib

uted

Pro

pulsi

on

Syste

mM.

Kerho

, Roll

ing H

ills Re

searc

h Co

rporat

ion, E

l Seg

undo

, CA

1100

hrs

AIAA-2

015-3

163

Aero

dyna

mic P

erfo

rman

ce of

the

Adap

tive N

acell

e Inle

tF.

Majić

, G. E

fraim

sson,

C. O’

Reilly

, Roy

al Ins

titute

of Te

chno

logy (

KTH)

, Stoc

kholm

, Sw

eden

1130

hrs

AIAA-2

015-3

164

Comp

utat

ional

Asse

ssmen

t of

Rain

fall E

ffects

on A

ircra

ft Ae

rody

nami

c Cha

racte

ristic

sH.

Sha

rma,

S. H

arshe

, S. V

ekari

a, M.

Sin

gh, M

. Dam

odara

n, Ind

ian In

stitut

e of

Tech

nolog

y Gan

dhina

gar, A

hmed

abad

, Ind

ia; B

. Kho

o, Na

tiona

l Univ

ersity

of

Singa

pore,

Sing

apore

, Sing

apore

Thur

sday

, 25

June

201

523

6-AP

A-28

Unste

ady A

erod

ynam

ics I

Stemm

ons A

Chair

ed by

: K. K

ARA,

Khali

fa Un

iversi

ty of

Scien

ce, T

echn

ology

& Re

searc

h and

J. RA

ULED

ER, T

echn

ical U

nivers

ity of

Mun

ich09

00 hr

sAIA

A-201

5-316

5Me

asur

emen

ts of

Dyn

amic

Inter

face

Betw

een

Ship

and

Helic

opter

Air

Wake

sC.

Fried

man,

Georg

e Was

hingto

n Un

iversi

ty, W

ashin

gton,

DC; M

. Sny

der,

U.S.

Nav

al Ac

adem

y, An

napo

lis, M

D

0930

hrs

AIAA-2

015-3

166

An Ex

perim

enta

l Stu

dy of

Add

ed

Mass

on a

Plung

ing A

irfoil

Os

cillat

ing w

ith H

igh Fr

eque

ncies

at

High

Ang

les of

Atta

ckM.

Zaka

ria, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA;

D. Pe

reira,

Univ

ersity

of S

ão Pa

ulo, S

ão

Paulo

, Braz

il; S.

Raga

b, M.

Hajj

, Virg

inia

Polyt

echn

ic Ins

titute

and S

tate U

nivers

ity,

Black

sburg

, VA;

F. Ma

rques

, Univ

ersity

of

São P

aulo,

São

Paulo

, Braz

il

1000

hrs

AIAA-2

015-3

167

Expe

rimen

tal-B

ased

Unifi

ed

Unste

ady N

onlin

ear A

erod

ynam

ic Mo

delin

g For

Two-

Dime

nsion

al Ai

rfoils

M. Za

karia

, Virg

inia P

olytec

hnic

Institu

te an

d Stat

e Univ

ersity

, Blac

ksbu

rg, VA

; H.

Taha

, Univ

ersity

of Ca

liforni

a, Irv

ine,

Irvine

, CA;

M. H

ajj, A

. Hus

sein,

Virg

inia

Polyt

echn

ic Ins

titute

and S

tate U

nivers

ity,

Black

sburg

, VA

1030

hrs

AIAA-2

015-3

168

Expe

rimen

tal D

ynam

ic Sta

ll stu

dy

on a

low R

eyno

lds n

umbe

r airf

oilS.

Algo

zino,

J. Ma

rañon

Di L

eo, J

. De

lnero,

G. C

apitti

ni, N

ation

al Un

iversi

ty of

La Pl

ata, L

a Plat

a, Arg

entin

a

1100

hrs

AIAA-2

015-3

169

Unste

ady A

erod

ynam

ic Mo

delin

g of

Roll

ing P

arac

hutes

Usin

g the

In

dicial

Meth

odM.

Gho

reysh

i, U.S

. Air F

orce A

cade

my,

Color

ado S

pring

s, CO

; K. B

ergero

n, Arm

y Re

searc

h, De

velop

ment

and E

ngine

ering

Co

mman

d, Na

tick,

MA; J

. Seid

el, A.

Lo

fthou

se, R

. Cum

ming

s, U.

S. Ai

r Forc

e Ac

adem

y, Co

lorad

o Spri

ngs,

CO

1130

hrs

AIAA-2

015-3

170

Subs

onic

Indic

ial A

erod

ynam

ics

for U

nstea

dy Lo

ads C

alcula

tion

via

Nume

rical

and A

nalyt

ical

Meth

ods:

a Pre

limina

ry A

ssessm

ent

M. Ri

ghi, Z

urich

Univ

ersity

of Ap

plied

Sc

ience

s, W

intert

hur, S

witze

rland

; M.

Berci

, Univ

ersity

of Le

eds,

Leed

s, Un

ited

Kingd

om; J

. Koc

h, Zu

rich U

nivers

ity of

Ap

plied

Scie

nces

, Wint

erthu

r, Swi

tzerla

nd

1200

hrs

AIAA-2

015-3

171

Imple

ment

ation

of Vo

rtex-

type

Gu

st Mo

del T

hrou

gh B

ound

ary

Cond

itions

E. Elj

ack,

I. AlQ

adi, K

ing Ab

dulaz

iz Un

iversi

ty, Je

edah

, Sau

di Ara

bia

102

Thur

sday

, 25

June

201

523

7-AS

E-3Ai

rcraf

t Wak

e Tur

bulen

ce I

(Invit

ed)

Plum

Blos

som

BCh

aired

by: M

. PRU

IS, N

orthw

est R

esea

rch As

socia

tes In

c and

N. A

HMAD

, NAS

A Lan

gley R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-3

172

Use o

f Sim

ple M

odels

to D

eterm

ine

Wake

Vorte

x Ca

tegor

ies fo

r New

Ai

rcraf

t (In

vited

)J.

Hallo

ck, D

epart

ment

of Tra

nspo

rtatio

n, Ca

mbrid

ge, M

A; G.

Gree

ne, J

. Titts

worth

, P.

Stran

de, F

edera

l Avia

tion A

dmini

strati

on,

Wash

ington

, DC;

F. Wa

ng, D

epart

ment

of Tra

nspo

rtatio

n, Ca

mbrid

ge, M

A

0930

hrs

AIAA-2

015-3

173

Multi-

Mode

l Ens

emble

Wak

e Vor

tex

Pred

iction

(Inv

ited)

S. Ko

erner,

Germ

an Ae

rospa

ce Ce

nter (

DLR)

, Ob

erpfaf

fenho

fen, G

erman

y; N.

Ahma

d, NA

SA La

ngley

Resea

rch Ce

nter, H

ampto

n, VA

; F. Ho

lzäpfe

l, Germ

an Ae

rospa

ce Ce

nter

(DLR

), Ob

erpfaf

fenho

fen, G

erman

y; R.

VanV

alken

burg,

NAS

A Lan

gley R

esearc

h Ce

nter, H

ampto

n, VA

1000

hrs

AIAA-2

015-3

174

Wind

Impa

ct on

Sing

le Vo

rtice

s and

Co

unter

-Rot

ating

Vorte

x Pa

irs in

Gr

ound

Pro

ximity

(Inv

ited)

F. Ho

lzäpfe

l, N. T

chipe

v, A.

Step

han,

Germ

an Ae

rospa

ce Ce

nter (

DLR)

, Ob

erpfaf

fenho

fen, G

erman

y

1030

hrs

AIAA-2

015-3

175

Sens

itivity

Ana

lysis

of A

ircra

ft En

coun

ters w

ith D

efor

med W

ake

Vorti

ces (

Invit

ed)

D. B

ieniek

, R. L

uckn

er, Te

chnic

al Un

iversi

ty of

Berlin

, Berl

in, G

erman

y

1100

hrs

AIAA-2

015-3

176

Asse

ssmen

t of W

akeM

od 4

: A N

ew

Stand

alone

Wak

e Vor

tex A

lgorit

hm

for E

stima

ting C

ircula

tion

Stren

gth

and P

ositio

n (In

vited

)D.

Jaco

b, Co

heren

t Res

earch

Grou

p, Or

mond

Bea

ch, F

L; D.

Lai, M

. Prui

s, D.

De

lisi, N

orthW

est R

esea

rch As

socia

tes,

Redm

ond,

WA

1130

hrs

AIAA-2

015-3

177

Obse

rvat

ions o

f Wak

e Vor

tices

from

Up

ward

Look

ing P

ulsed

Dop

pler

Lidar

Dat

a (In

vited

)M.

Pruis

, D. D

elisi,

Nort

hWes

t Res

earch

As

socia

tes, R

edmo

nd, W

A; D.

Jaco

b, Co

heren

t Res

earch

Grou

p, Or

mond

Be

ach,

FL

Thur

sday

, 25

June

201

523

8-AT

IO-2

1En

Rou

te Op

erat

ions

Milan

Chair

ed by

: M. K

OCH,

NAS

A Lan

gley R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-3

178

Cont

rolle

r Wor

kload

-bas

ed

Calcu

lation

of M

onito

r Aler

t Pa

rame

ters f

or En

Rou

te Se

ctors

B. M

arr, K

. Lind

say,

MITR

E Corp

oratio

n, Mc

Lean

, VA

0930

hrs

AIAA-2

015-3

179

Optim

izatio

n of

the C

ruise

Reg

ime

of Fl

ight A

irplan

e Tra

jecto

ry u

sing

Deter

minis

tic A

lgorit

hms

M. G

autie

r, R. B

otez,

Unive

rsity

of Qu

ébec

, Mon

tréal,

Cana

da

1000

hrs

AIAA-2

015-3

180

Can

grou

nd-b

ased

sepa

ratio

n ac

comm

odat

e ver

y high

en ro

ute

traffi

c dem

and a

s well

as ad

vanc

ed

self-

sepa

ratio

n?H.

Blom

, B. B

akke

r, Nati

onal

Aeros

pace

La

borat

ory (N

LR),

Amste

rdam,

The

Nethe

rland

s

Thur

sday

, 25

June

201

523

9-AT

IO-2

2AT

M V -

Per

form

ance

Asse

ssmen

tMo

rocco

Chair

ed by

: D. D

ELAU

RENT

IS, Pu

rdue U

nivers

ity09

00 hr

sAIA

A-201

5-318

1Ve

rifyin

g Req

uired

Comm

unica

tion

Perfo

rman

ce in

Air

Traffi

c Ma

nage

ment

D. Ze

ng, J

. Gon

da, M

ITRE C

orpora

tion,

McLe

an, V

A

0930

hrs

AIAA-2

015-3

182

Meth

odolo

gy to

Defi

ne D

elive

ry

Accu

racy

Und

er Cu

rrent

Day

ATC

Oper

ation

sS.

Sha

rma,

J. Ro

binso

n III,

NASA

Ames

Re

searc

h Cen

ter, M

offett

Field

, CA

1000

hrs

AIAA-2

015-3

183

Inve

stiga

tion

of Co

nnec

tivity

: De

finitio

n, A

pplic

ation

, and

Fo

rmula

tion

L. Bo

wers,

L. M

ocku

s, S.

Tama

skar,

D.

DeLa

urenti

s, Pu

rdue U

nivers

ity, W

est

Lafay

ette,

IN

1030

hrs

AIAA-2

015-3

184

Regio

nal S

ky Tr

ansit

B. S

eeley

, CAF

E Fou

ndati

on, S

anta

Rosa

, CA

1100

hrs

AIAA-2

015-3

185

An A

irpor

t Asse

ssmen

t App

roac

h in

the C

once

ptua

l Des

ign St

age

M. W

eiss,

N. D

zikus

, Germ

an Ae

rospa

ce

Cente

r (DL

R), H

ambu

rg, G

erman

y

1130

hrs

AIAA-2

015-3

186

Mode

ling a

Ram

p Are

a Sup

port

Syste

mA.

Wing

, W. F

elder,

R. Cl

outie

r, Stev

ens

Institu

te of

Tech

nolog

y, Ho

boke

n, NJ

1200

hrs

AIAA-2

015-3

187

Fram

ewor

k De

velop

ment

for

Perfo

rman

ce Ev

aluat

ion of

the

Futu

re N

ation

al Ai

rspac

e Sys

temM.

Has

san,

A. Pa

yan,

H. Pf

aend

er, D

. Ma

vris,

E. Ga

rcia,

J. Sc

hutte

, Geo

rgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

Thur

sday

, 25

June

201

524

0-AT

IO-2

3Tra

nsfo

rmat

ional

Fligh

t - El

ectri

c Pro

pulsi

onMo

net B

allro

omCh

aired

by: S

. GIN

N, N

ASA

0900

hrs

Oral

Prese

ntatio

nHE

IST LE

APTe

ch In

strum

enta

tion

Desig

n, D

evelo

pmen

t, an

d Init

ial

Resu

ltsT.

Foste

r, Emp

irical

Syste

ms Ae

rospa

ce,

Inc.,

Pismo

Bea

ch, C

A

0930

hrs

Oral

Prese

ntatio

nLE

APTe

ch H

EIST P

ower

Arch

itectu

re

and T

estin

gS.

Clark

e, Y.

Lin, A

. Sam

uel, K

. Pa

patha

kis, N

ASA A

rmstr

ong F

light

Rese

arch C

enter

, Edw

ards,

CA

1000

hrs

AIAA-2

015-3

188

Comp

ariso

n of

CFD

and

Expe

rimen

tal R

esult

s of t

he

LEAP

Tech

Dist

ribut

ed El

ectri

c Pr

opuls

ion B

lown

Wing

A. St

oll, J

oby A

viatio

n, Sa

nta Cr

uz, C

A

1030

hrs

AIAA-2

015-3

189

A Co

ncep

tual

Appr

oach

to Fl

ight-

Traini

ng M

ission

and C

ost A

nalys

is of

an A

ll-Ele

ctric

Aircr

aft E

quipp

ed

with

Reg

ener

ative

Ener

gy D

evice

sM.

Olso

n, Ge

orgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

1100

hrs

AIAA-2

015-3

190

Optim

al Pr

opell

er P

itch

Sche

dulin

g an

d Pro

pelle

r--Ai

rfram

e Mat

ching

fo

r Con

cept

ual D

esign

R. Mc

Dona

ld, Ca

liforni

a Poly

techn

ic St

ate

Unive

rsity,

San

Luis

Obisp

o, CA

1130

hrs

AIAA-2

015-3

191

Mode

ling a

nd Te

st of

the E

fficie

ncy

of El

ectro

nic Sp

eed C

ontro

llers

for

Brus

hless

DC M

otor

sC.

Gree

n, R.

McDo

nald,

Califo

rnia

Polyt

echn

ic St

ate U

nivers

ity, S

an Lu

is Ob

ispo,

CA

103

Thur

sday

, 25

June

201

524

1-CF

D-26

Unstr

uctu

red H

igh-O

rder

Meth

ods I

IIGr

and B

allro

om A

Chair

ed by

: R. H

ARRIS

, CFD

Rese

arch C

orpora

tion a

nd B

. JOL

LY, U

S Air

Force

0900

hrs

AIAA-2

015-3

192

Deve

lopme

nt of

Verte

x-Ce

nter

ed,

High

-Ord

er Sc

heme

s and

Im

pleme

ntat

ion in

FUN3

DH.

Yang

, R. H

arris,

CFD

Rese

arch

Corpo

ration

, Hun

tsville

, AL

0930

hrs

AIAA-2

015-3

193

A co

mpac

t high

orde

r finit

e volu

me

meth

od fo

r hyp

erbo

lic co

nser

vatio

n law

s on

unstr

uctu

red g

rids

Q. W

ang,

Y. Re

n, Tsi

nghu

a Univ

ersity

, Be

ijing,

China

; W. L

i, Sun

Yat-S

en

Unive

rsity,

Gua

ngzh

ou, C

hina

1000

hrs

AIAA-2

015-3

194

Loca

lly-D

efine

d High

-Res

olutio

n Sc

heme

for S

hock

-Cap

turin

g Pr

oblem

s on U

nstru

cture

d Car

tesian

Gr

idsY.

Tama

ki, T.

Imam

ura, U

nivers

ity of

To

kyo,

Toky

o, Ja

pan

1030

hrs

AIAA-2

015-3

195

High

-Ord

er Co

mpre

ssible

Flow

Sim

ulatio

ns w

ith th

e Uns

tructu

red

Spec

tral D

iffer

ence

Meth

odF.

Morei

ra, C.

Brev

iglier

i, Tec

hnolo

gical

Institu

te of

Aeron

autic

s (ITA

), Sã

o Jo

sé do

s Cam

pos,

Braz

il; J.

Azev

edo,

Aeron

autic

s and

Spa

ce In

stitut

e (IAE

), Sã

o Jo

sé do

s Cam

pos,

Braz

il

1100

hrs

AIAA-2

015-3

196

A new

high

-orde

r uns

tructu

red

nume

rical

schem

e for

larg

e edd

y sim

ulatio

nZ.

Xu, U

nivers

ity of

Scien

ce an

d Tech

nolog

y, He

fei, C

hina;

Q. Zh

ao, C

hinese

Acad

emy o

f Sc

iences

, Beiji

ng, C

hina;

Q. Lin

, Univ

ersity

of

Scien

ce an

d Tech

nolog

y, He

fei, C

hina;

J. Xu

, Ch

inese

Acad

emy o

f Scie

nces,

Beijin

g, Ch

ina

Thur

sday

, 25

June

201

524

2-CF

D-27

Curre

nt Tr

ends

in CF

D Re

sear

ch II

(Inv

ited)

Gran

d Ball

room

BCh

aired

by: H

. HUY

NH, N

ASA G

lenn R

esea

rch Ce

nter a

nd Z.

WAN

G, U

nivers

ity of

Kans

as09

00 hr

sOr

al Pre

senta

tion

Theo

retic

al As

pects

of H

igh-O

rder

Flu

x Re

cons

tructi

on Sc

heme

s (In

vited

)P.

Vince

nt, Im

peria

l Coll

ege L

ondo

n, Lo

ndon

, Unit

ed Ki

ngdo

m

0930

hrs

AIAA-2

015-3

197

Well P

osed

Pro

blems

and B

ound

ary

Cond

itions

in Co

mput

ation

al Flu

id Dy

nami

cs (In

vited

)J.

Nords

trom,

Link

öping

Univ

ersity

, Lin

köpin

g, Sw

eden

1000

hrs

AIAA-2

015-3

198

Oppo

rtunit

ies fo

r effi

cient

high-o

rder

me

thods

based

on th

e sum

matio

n-by-

parts

prop

erty (

Invite

d)J.

Hicke

n, Re

nssela

er Po

lytech

nic In

stitute

, Tro

y, NY

; D. D

el Re

y Fern

ánde

z, D.

Zingg

, Un

iversit

y of T

oronto

, Toro

nto, C

anad

a

1030

hrs

Oral

Prese

ntatio

nRo

le of

Entro

py-R

esidu

al in

High

-Or

der N

umeri

cal M

ethod

s for

Gas

-Dy

nami

cs Ca

lculat

ions:

Shoc

k Dete

ctor

and A

dapta

tion I

ndica

tor (I

nvite

d)M.

Ihme

, Y. L

v, Sta

nford

Unive

rsity,

Stanfo

rd,

CA

1100

hrs

Oral

Prese

ntatio

nLa

rge E

ddy S

imula

tions

of

Turb

ulent

Flow

s Usin

g Di

scont

inuou

s High

Ord

er M

ethod

s (In

vited

)Z.

Wang

, Univ

ersity

of Ka

nsas

, Law

rence

, La

wren

ce, K

S

1130

hrs

AIAA-2

015-3

199

Multi-

dimen

siona

l Lim

iting S

trateg

y fo

r High

er-o

rder

CFD

Meth

ods -

Pr

ogre

ss an

d Issu

e (In

vited

)C.

Kim, S

eoul

Natio

nal U

nivers

ity, S

eoul,

So

uth Ko

rea; J

. Park

, Imp

erial

Colle

ge

Lond

on, L

ondo

n, Un

ited K

ingdo

m

Thur

sday

, 25

June

201

524

3-CF

D-28

Inco

mpre

ssible

and L

ow Sp

eed F

lows

Plum

Blos

som

ACh

aired

by: M

. YU,

Univ

ersity

of M

arylan

d, Ba

ltimore

Coun

ty an

d R. R

AJAG

OPAL

AN, I

owa S

tate U

nivers

ity09

00 hr

sAIA

A-201

5-320

0Hi

gh-O

rder

Stra

nd G

rid M

ethod

s fo

r Low

Mac

h an

d Inc

ompr

essib

le Flo

wsJ.

Thorn

e, A.

Katz,

Utah

Stat

e Univ

ersity

, Lo

gan,

UT

0930

hrs

AIAA-2

015-3

201

An Ex

plicit

Pre

ssure

-Bas

ed

Algo

rithm

for I

ncom

pres

sible

Flows

D. G

arrick

, R. R

ajago

palan

, Iow

a Stat

e Un

iversi

ty, Am

es, I

A

1000

hrs

AIAA-2

015-3

202

A Tu

rbule

nt Lo

w-Sp

eed

Prec

ondit

ioner

for U

nstea

dy Fl

ows

Abou

t Wind

Turb

ine A

irfoil

sR.

Djedd

i, K. E

kici, U

nivers

ity of

Te

nnes

see,

Knox

ville,

Knox

ville,

TN

1030

hrs

AIAA-2

015-3

203

Comp

ariso

n of

Pre

ssure

-Bas

ed

Rung

e-Ku

tta Sc

heme

s for

Uns

teady

In

comp

ressi

ble Fl

ows

M. Fi

schels

, R. R

ajago

palan

, Iow

a Stat

e Un

iversi

ty, Am

es, I

A

1100

hrs

AIAA-2

015-3

204

Apply

ing N

on-R

eflec

ting B

ound

ary

Cond

itions

in P

ressu

re-B

ased

So

lvers

V. Iva

nov,

B. M

akaro

v, AN

SYS,

Inc.,

Le

bano

n, NH

1130

hrs

AIAA-2

015-3

205

Gene

ralis

ed SI

MPLE

-Bas

ed P

ressu

re

Corre

ction

Meth

od fo

r Uns

tructu

red

Co-lo

cated

Grid

sV.

Przulj

, Rica

rdo S

oftwa

re, S

horeh

am by

Se

a, Un

ited K

ingdo

m

1200

hrs

AIAA-2

015-3

206

Robu

stness

to In

accu

rate

Initia

l Co

nditio

ns in

Low

Mach

Preco

nditio

ned

Dens

ity-B

ased

Meth

ods

C. Fa

lcão,

Unive

rsity o

f Rio

Grand

e do S

ul,

Porto

Aleg

re, Br

azil;

F. Med

eiros,

Milita

ry Ins

titute

of En

ginee

ring (

IME),

Rio d

e Jan

eiro,

Brazil;

L. Al

ves,

Flumi

nese

Fede

ral Un

iversit

y (U

FF),

Niteró

i, Braz

il

Thur

sday

, 25

June

201

524

4-CF

D-29

High

-Spe

ed an

d Rea

cting

Flow

sCo

ral

Chair

ed by

: G. C

ANDL

ER, U

nivers

ity of

Minn

esota

and B

. RAT

HAKR

ISHNA

N, G

E Glob

al Re

searc

h09

00 hr

sAIA

A-201

5-320

7LE

S of r

eacti

ng m

ixing

laye

rs:

influe

nce o

f infl

ow co

nditio

ns an

d he

at re

lease

A. Ka

rtha,

P. Su

bbare

ddy,

G. Ca

ndler

, Un

iversi

ty of

Minn

esota

, Minn

eapo

lis,

Minn

eapo

lis, M

N; P.

Dim

otakis

, Cali

fornia

Ins

titute

of Te

chno

logy,

Pasa

dena

, CA

0930

hrs

AIAA-2

015-3

208

A Prio

ri Ana

lysis o

f a Co

mpres

sible

Flame

let M

odel

using

RANS

Data

for a

Du

al-Mo

de Sc

ramj

et Co

mbus

torJ.

Quinla

n, T.

Drozd

a, NA

SA La

ngley

Resea

rch

Cente

r, Ham

pton,

VA; J

. McD

aniel,

Unive

rsity

of Vir

ginia,

Charl

ottesv

ille, C

harlo

ttesvi

lle,

VA; G

. Laca

ze, J

. Oefe

lein, S

andia

Nati

onal

Labo

ratori

es, Liv

ermore

, CA

1000

hrs

AIAA-2

015-3

209

Nume

rical

Inve

stiga

tions

of P

ulsed

Fu

el In

jectio

n int

o Sup

erso

nic

Cros

sflow

N. W

illiam

s, R.

Thom

pson

, T. M

oelle

r, Un

iversi

ty of

Tenn

esse

e, Tu

llaho

ma,

Tulla

homa

, TN

1030

hrs

AIAA-2

015-3

210

Ignit

ion Ch

arac

terist

ics in

Spat

ially

Zero

-, On

e- an

d Two

-Dim

ensio

nal

Lami

nar E

thyle

ne Fl

ames

M. Ev

ans,

P. Me

dwell

, Z. T

ian, U

nivers

ity

of Ad

elaide

, Ade

laide

, Aus

tralia

; A.

Frasso

ldati,

A. Cu

oci, A

. Stag

ni, Te

chnic

al Un

iversi

ty of

Milan

, Mila

n, Ita

ly

1100

hrs

AIAA-2

015-3

211

IDDE

S sim

ulatio

n of

supe

rsonic

co

mbus

tion

using

flam

elet

mode

ling

H. W

ang,

Y. Pia

o, J.

Niu, T

singh

ua

Unive

rsity,

Beij

ing, C

hina

1130

hrs

AIAA-2

015-3

212

Thre

e Dim

ensio

nal F

low A

nalys

is of

a C

avity

-Bas

ed Sc

ramj

et Co

mbus

tor

R. Ro

uzba

r, S. E

yi, M

iddle

East

Tech

nical

Unive

rsity,

Anka

ra, Tu

rkey

104

Thur

sday

, 25

June

201

524

5-CF

D-30

Inflo

w Tu

rbule

nce f

or W

all-B

ound

ed LE

S (In

vited

)Em

erald

Chair

ed by

: N. B

ISEK,

Air Fo

rce Re

seac

h Lab

orator

y and

L. TA

O, G

E Glob

al Re

searc

h09

00 hr

sAIA

A-201

5-321

3An

Ove

rview

of Tu

rbule

nt In

flow

Boun

dary

Cond

itions

for L

arge

Ed

dy Si

mulat

ions (

Invit

ed)

N. D

hama

nkar,

G. B

laisd

ell, P

urdue

Un

iversi

ty, W

est L

afaye

tte, I

N; A.

Lyrin

tzis,

Embry

-Ridd

le Ae

ronau

tical

Unive

rsity,

Da

ytona

Bea

ch, F

L

0930

hrs

AIAA-2

015-3

214

A Co

unter

-Flow

Force

Bas

ed M

ethod

to

Gen

erat

e Equ

ilibriu

m Tu

rbule

nt

Inflo

w Co

nditio

ns (I

nvite

d)D.

Gait

onde

, M. W

aindim

, M. A

dler, O

hio

State

Univ

ersity

, Colu

mbus

, OH

1000

hrs

AIAA-2

015-3

215

Gene

ratin

g Syn

theti

c In

homo

gene

ous T

urbu

lence

from

RA

NS St

atist

ics (I

nvite

d)P.

Batte

n, U.

Gold

berg,

O. P

eroom

ian, S

. Ch

akrav

arthy

, Meta

comp

Tech

nolog

ies,

Inc.,

Agou

ra Hil

ls, CA

1030

hrs

Q&A P

anel

Discu

ssion

Thur

sday

, 25

June

201

524

6-FD

-27

Turb

ulenc

e Ana

lysis

Gove

nors

Lectu

re H

allCh

aired

by: Z

. ZHE

NG, T

he U

nivers

ity of

Kans

as an

d S. S

ILTON

, US

Army R

esea

rch La

borat

ory09

00 hr

sAIA

A-201

5-321

6Sin

gle an

d Mult

iple-

Point

Ana

lysis

of Ve

locity

Fluc

tuat

ions i

n a

Deto

natio

n-Tu

rbule

nce I

nter

actio

nS.

Hus

sein,

F. Lu

, Univ

ersity

of Te

xas,

Arling

ton, A

rlingto

n, TX

0930

hrs

AIAA-2

015-3

217

Nonli

near

Time

Serie

s Ana

lysis

of

Veloc

ity ov

er N

ACA

2412

Thre

e-Di

mens

ional

Wing

Usin

g Lar

ge

Eddy

Simu

lation

Dat

aP.

Chak

rabort

y, A.

Roy,

Indian

Insti

tute o

f Te

chno

logy K

harag

pur, K

olkata

, Ind

ia

1000

hrs

AIAA-2

015-3

218

Ther

mal n

on-e

quilib

rium

effe

cts in

tu

rbule

nt co

mpre

ssible

shea

r flow

sA.

Nevil

le, I.

Nom

pelis,

P. S

ubba

reddy

, G.

Cand

ler, U

nivers

ity of

Minn

esota

, Mi

nnea

polis,

Minn

eapo

lis, M

N

Thur

sday

, 25

June

201

524

7-FD

-28

0900

- 12

30 h

rsTra

nsitio

n Op

en Fo

rum

Sapp

hire

Chair

ed by

: H. R

EED,

Texa

s A&M

Univ

ersity

Thur

sday

, 25

June

201

524

8-FD

-29

Flow

Cont

rol -

Aer

odyn

amics

Sena

tors

Lectu

re H

allCh

aired

by: H

. DON

G, U

nivers

ity of

Virg

inia a

nd E.

WHA

LEN,

Boe

ing En

ginee

ring O

perat

ions &

Tech

nolog

y09

00 hr

sAIA

A-201

5-321

9Th

ree-

dimen

siona

l Con

trol v

ia Ma

ss In

jectio

n fo

r Sup

pres

sion

of Ca

vity

Oscil

lation

sY.

Zhan

g, N.

Arora

, Y. S

un, L

. Catt

afesta

, K.

Taira

, Flor

ida S

tate U

nivers

ity,

Talla

hasse

e, FL

; L. U

keile

y, Un

iversi

ty of

Florid

a, Ga

inesv

ille, G

aines

ville,

FL

0930

hrs

AIAA-2

015-3

220

Prop

ulsive

Per

form

ance

and V

ortex

In

terac

tions

of M

ultipl

e Tan

dem

Foils

Pitc

hing I

n Lin

eC.

Yuan

, G. L

iu, Y.

Ren,

H. D

ong,

Unive

rsity

of Vir

ginia,

Charl

ottes

ville,

Ch

arlott

esvil

le, VA

1000

hrs

AIAA-2

015-3

221

On th

e Effe

ct of

Rigi

d Swe

pt

Surfa

ce W

aves

on Tu

rbule

nt D

rag

M. D

eniso

n, Na

tiona

l Insti

tute o

f Ae

rospa

ce, H

ampto

n, VA

; S. W

ilkins

on,

P. Ba

lakum

ar, N

ASA L

angle

y Res

earch

Ce

nter, H

ampto

n, VA

1030

hrs

AIAA-2

015-3

222

Cont

rol o

f Toll

mien

-Sch

licht

ing

Wave

s Usin

g Piez

oelec

trica

lly

Drive

n Os

cillat

ing Su

rface

H. D

ell’O

rso, B

. Tun

a, M.

Amita

y, Re

nsse

laer P

olytec

hnic

Institu

te, Tr

oy, N

Y

105

Thur

sday

, 25

June

201

524

9-FT

-1Fli

ght T

estin

gOb

elisk

BCh

aired

by: K

. GAR

MAN,

Fede

ral Av

iation

Admi

nistra

tion a

nd J.

BRA

NDON

, NAS

A-Lan

gley R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-3

223

A Fr

amew

ork

for A

pplyi

ng th

e OO

DA Lo

op to

Miss

ion Co

ntro

l Ro

om Ex

ecut

ionJ.

Newc

amp,

U.S.

Air F

orce A

cade

my,

Color

ado S

pring

s, CO

0930

hrs

AIAA-2

015-3

224

Curre

nt H

yper

sonic

and S

pace

Ve

hicle

Fligh

t Tes

t Ins

trume

ntat

ion

Chall

enge

sJ.

Sprav

ka, T

. Jorr

is, 4

12th

Test

Wing

, Ed

wards

AFB,

CA

1000

hrs

AIAA-2

015-3

225

Stall/

Spin

Fligh

t Tes

t Tec

hniqu

es

with

COTS

Mod

el Ai

rcraf

t and

Fligh

t Da

ta Sy

stems

R. Bu

nge,

F. Mu

nera

Savin

o, I.

Kroo,

Stan

ford U

nivers

ity, S

tanfor

d, CA

1030

hrs

AIAA-2

015-3

226

Grou

nd M

inimu

m Co

ntro

l Spe

ed

(VMC

G) Te

sting

of Tr

ansp

ort

Aircr

aft

P. Bo

lds-M

ooreh

ead,

V. Ch

aney

, The

Bo

eing C

ompa

ny, S

eattle

, WA;

T. Lu

tz, S

. Va

ux, A

irbus

, Tou

louse

, Fran

ce

1100

hrs

AIAA-2

015-3

227

Later

al-Di

recti

onal

Aero

dyna

mic

Mode

l Ide

ntifi

catio

n of

a Sin

gle-

Engin

e Pro

pelle

r Airc

raft

Using

Pa

rtial

Orth

ogon

al Le

ast S

quar

esJ.

Zane

tte, B

razilia

n Air F

orce,

São

José

dos C

ampo

s, Br

azil;

F. Alm

eida,

Tech

nolog

ical In

stitut

e of A

erona

utics

(ITA)

, São

José

dos C

ampo

s, Br

azil

Thur

sday

, 25

June

201

525

0-LTA

-1Lig

hter

-than

-Air

Syste

ms &

Tech

nolog

ies I

Steub

enCh

aired

by: R

. VAN

TREU

REN

0900

hrs

AIAA-2

015-3

228

Desig

n an

d Con

trol o

f a M

ulti-

vecto

red T

hrus

t Airs

hipL.

Chen

, Y. W

en, H

. Zho

u, X.

Wan

g, P.

Zhou

, D. D

uan,

Shan

ghai

Jiao T

ong

Unive

rsity,

Sha

ngha

i, Chin

a

0930

hrs

AIAA-2

015-3

229

Nume

rical

Feas

ibility

Ana

lysis

of

the E

xtra

-ligh

t Weig

ht St

ructu

re

Tens

airity

on La

rge A

irship

sA.

Suño

l, T. Y

ang,

D. Vu

cinic,

Vrije

Un

iversi

teit B

russe

l, Brus

sels,

Belg

ium

1000

hrs

AIAA-2

015-3

230

Comp

utat

ional

Mode

lling o

f Ae

rody

nami

c Cha

racte

ristic

s of

Airsh

ips in

Arb

itrar

y Mot

ionA.

Kano

ria, K

. Pan

chal,

R. D

ongre

, M.

Damo

daran

, Ind

ian In

stitut

e of T

echn

ology

Ga

ndhin

agar,

Ahme

daba

d, Ind

ia

1030

hrs

AIAA-2

015-3

231

Distu

rban

ce R

ejecti

on B

ased

Pa

th Fo

llowi

ng Co

ntro

l for

A

Strat

osph

eric

Airsh

ip wi

th A

ctuat

or

Satu

ratio

nK.

Yan,

Z. Zh

eng,

M. Zh

u, Z.

Wu,

Beiha

ng

Unive

rsity,

Beij

ing, C

hina

1100

hrs

AIAA-2

015-3

232

A Lo

ng En

dura

nce,

High

ly Ma

neuv

erab

le, Co

llabo

rativ

e, Un

mann

ed A

irbor

ne Sy

stem

W. Ki

ng, D

. Lan

drum,

J. Al

corn,

A.

Jarze

mbsk

i, Univ

ersity

of Al

abam

a, Hu

ntsvil

le, H

untsv

ille, A

L

Thur

sday

, 25

June

201

525

1-MA

O-8

Meta

mode

ling I

IMa

nche

ster

Chair

ed by

: B. R

OTH,

Wall

a Wall

a Univ

and J

. HICK

EN, R

ensse

laer P

olytec

hnic

Institu

te09

00 hr

sAIA

A-201

5-323

3Ad

aptiv

e Swi

tching

of Va

riable

-Fid

elity

Mod

els in

Pop

ulatio

n-ba

sed

Optim

izatio

n Al

gorit

hms

A. Me

hman

i, Syra

cuse

Univ

ersity

, Sy

racus

e, NY

; S. C

howd

hury,

A. M

essa

c, Mi

ssissi

ppi S

tate U

nivers

ity, M

ississ

ippi

State

, MS

0930

hrs

AIAA-2

015-3

234

Larg

e-sca

le CF

D Op

timiza

tion

base

d on

the F

FD P

aram

etriza

tion

using

the M

ultipo

int A

ppro

ximat

ion

Meth

od in

an H

PC En

viron

ment

Y. Ko

rolev

, V. T

oropo

v, Qu

een M

ary

Unive

rsity

of Lo

ndon

, Lon

don,

Unite

d Kin

gdom

; S. S

hahp

ar, Ro

lls-Ro

yce G

roup

plc, D

erby,

Unite

d King

dom

1000

hrs

AIAA-2

015-3

235

Adap

tive V

ariab

le-Fid

elity

Ae

rody

nami

c Ana

lysis

and D

esign

fo

r Tail

less A

ircra

ft un

der M

odel-

Form

Unc

erta

inty

Y. Jo

, J. P

ark, C

. Och

eltree

, J. C

hoi, S

. Ch

oi, P.

Raj, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA; e

t al.

1030

hrs

AIAA-2

015-3

236

Study

of H

ybrid

Rad

ial B

asis

Func

tion

for D

esign

Opt

imiza

tion

Prob

lems

R. Sh

i, L. L

iu, T.

Long

, J. L

iu, B

eijing

Ins

titute

of Te

chno

logy,

Beijin

g, Ch

ina

Thur

sday

, 25

June

201

525

2-MA

O-9

Shap

e and

Topo

logy I

Madr

idCh

aired

by: J

. MAR

TINS,

Univ

ersity

of M

ichiga

n and

R. KO

LONA

Y, Air

Force

Rese

arch L

abora

tory/

RQVC

/WPA

FB09

00 hr

sAIA

A-201

5-323

7No

nintru

sive C

ontin

uum

Sens

itivity

An

alysis

for A

erod

ynam

ic Sh

ape

Optim

izatio

nM.

Kulka

rni, R

. Can

field,

M. P

atil, V

irgini

a Po

lytec

hnic

Institu

te an

d Stat

e Univ

ersity

, Bla

cksb

urg, V

A

0930

hrs

AIAA-2

015-3

238

Thre

e-Di

mens

ional

Piece

wise

-Co

ntinu

ous C

lass-S

hape

Tra

nsfo

rmat

ion of

Wing

sE.

Olso

n, NA

SA La

ngley

Rese

arch C

enter

, Ha

mpton

, VA

1000

hrs

AIAA-2

015-3

239

Multi-

objec

tive s

hape

optim

izatio

n of

aircr

aft c

abin

vent

ilatio

n co

mpon

ents

using

adjoi

nt CF

DT.

Köthe

, S. H

erzog

, C. W

agne

r, Germ

an

Aeros

pace

Cente

r (DL

R), G

ötting

en,

Germ

any

1030

hrs

AIAA-2

015-3

240

Deve

lopme

nt of

a Con

sisten

t Di

screte

Adjoi

nt So

lver in

an Ev

olving

Ae

rody

nami

c Desi

gn Fr

amew

ork

T. Alb

ring,

M. Sa

geba

um, N

. Gau

ger, T

echnic

al Un

iversit

y of K

aisers

lauter

n, Ka

isersla

utern,

Ge

rman

y

1100

hrs

AIAA-2

015-3

241

The R

esea

rch on

Geo

metry

Mo

delin

g Meth

od B

ased

on Th

ree-

dimen

siona

l CST

Par

amete

rizat

ion

Tech

nolog

yH.

Su,

L. Gu

, C. G

ong,

North

weste

rn Po

lytec

hnica

l Univ

ersity

, Xi’a

n, Ch

ina

1130

hrs

AIAA-2

015-3

242

Conc

urre

nt Su

bspa

ce O

ptim

izatio

n De

sign

of H

yper

sonic

Cruis

e Veh

icle

C. Jin

g, S.

Yuan

-pei, C

hina A

erody

nami

cs Re

searc

h and

Dev

elopm

ent C

enter

, Mi

anya

ng, C

hina

106

Thur

sday

, 25

June

201

525

3-MS

T-11

Aircr

aft S

ystem

s Des

ign, V

erifi

catio

n an

d Vali

datio

nTra

verti

neCh

aired

by: G

. CHA

TTER

JI, N

ASA A

mes R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-3

243

ADDA

M: A

n Ob

ject O

rient

ed D

ata

Mode

l for

an A

ircra

ft De

sign

Envir

onme

nt in

MAT

LAB

S. H

erbst,

M. H

ornun

g, Te

chnic

al Un

iversi

ty of

Munic

h, Mu

nich,

Germ

any

1000

hrs

AIAA-2

015-3

245

Dyna

mic m

odel

upda

ting o

f a s

imula

tion c

asing

based

on

expe

rimen

tal m

odal

para

meter

sB.

Jie, Q

. Mei,

C. Zh

ang,

Aviat

ion In

dustr

y Co

rporat

ion of

China

(AVIC

), Zh

uzho

u, Ch

ina

Thur

sday

, 25

June

201

525

4-NW

-8

0900

- 09

30 h

rsNe

twor

king C

offe

e Bre

akCh

antill

y Ball

room

East

Thur

sday

, 25

June

201

525

5-PD

L-12

Aero

-Opt

ics P

lasma

Diag

nosti

csMi

roCh

aired

by: R

. MILE

S, Pr

inceto

n Univ

ersity

and M

. REN

NIE,

Unive

rsity

of No

tre D

ame

0900

hrs

AIAA-2

015-3

246

Aero

-Opti

cal M

easu

remen

ts of

High

-Ma

ch Su

perso

nic Bo

unda

ry La

yers

S. Go

rdeye

v, M.

Renn

ie, Un

iversit

y of N

otre

Dame

, Notr

e Dam

e, IN;

A. Ca

in, In

nova

tive

Techn

ology

Applic

ation

s Com

pany,

LLC,

Chest

erfield

, MO;

T. Ha

yden

, U.S.

Air F

orce

Acad

emy,

Color

ado S

pring

s, CO

0930

hrs

AIAA-2

015-3

247

Non-

intru

sive V

elocit

y and

Den

sity

Meas

urem

ents

in Su

bson

ic Tu

rbule

nt B

ound

ary L

ayer

J. So

ntag,

S. G

ordey

ev, U

nivers

ity of

Notr

e Da

me, N

otre D

ame,

IN

1000

hrs

AIAA-2

015-3

248

Nume

rical

Inve

stiga

tion

of

Aero

-Opt

ical D

istor

tions

over

a He

misp

here

-on-

Cylin

der T

urre

t wi

th G

aps

E. Ma

thews

, K. W

ang,

M. W

ang,

E. Ju

mper,

Univ

ersity

of N

otre D

ame,

Notre

Da

me, I

N

1030

hrs

AIAA-2

015-3

249

Char

acter

izatio

n of

Flow

Cont

rol

Actu

ator

s Bas

ed on

Spar

k Di

schar

ge P

lasma

s Usin

g Par

ticle

Imag

e Velo

cimetr

yB.

Sing

h, M.

Belm

ouss,

S. B

ane,

Purdu

e Un

iversi

ty, W

est L

afaye

tte, I

N

1100

hrs

AIAA-2

015-3

250

Inve

stiga

tion

of sh

ock

/ tu

rbule

nt

boun

dary

inter

actio

n un

stead

iness

with

vario

us ob

struc

tions

for a

ero-

optic

sM.

Whit

e, Oh

io Ae

rospa

ce In

stitut

e, Da

yton,

OH; M

. Visb

al, Ai

r Forc

e Res

earch

La

borat

ory, W

right-

Patte

rson A

FB, O

H

Thur

sday

, 25

June

201

525

6-TP

-12

Deta

iled M

olecu

lar P

roce

ss Mo

delin

gRo

setta

Chair

ed by

: R. W

AGNI

LD, S

andia

Nati

onal

Labo

ratori

es an

d T. S

CHWA

RTZE

NTRU

BER,

Unive

rsity

of Mi

nnes

ota09

00 hr

sAIA

A-201

5-325

1Vib

ratio

nal R

elaxa

tion

and

Disso

ciatio

n of

Oxy

gen

in Mo

lecule

-At

om Co

llision

sD.

Andri

enko

, I. B

oyd,

Unive

rsity

of Mi

chiga

n, An

n Arbo

r, Ann

Arbo

r, MI

0930

hrs

AIAA-2

015-3

252

Maste

r Equ

ation

Stud

y of

Vibra

tiona

l and

Rot

ation

al Re

laxat

ion of

Oxy

gen

D. An

drien

ko, I

. Boy

d, Un

iversi

ty of

Mich

igan,

Ann A

rbor, A

nn Ar

bor, M

I

1000

hrs

AIAA-2

015-3

253

Char

acter

izatio

n of

Vibr

ation

al an

d Ro

tatio

nal E

nerg

y Tra

nsfe

r in

N 2-N2

Disso

ciativ

e Coll

ision

s Usin

g the

Qu

asicl

assic

al Tra

jecto

ry M

ethod

J. Be

nder,

P. Va

lentin

i, I. N

ompe

lis, T.

Sc

hwart

zentr

uber,

G. C

andle

r, Univ

ersity

of

Minn

esota

, Minn

eapo

lis, M

innea

polis,

MN

1030

hrs

AIAA-2

015-3

254

Dire

ct mo

lecula

r sim

ulatio

n of

high

-temp

erat

ure n

itrog

en

disso

ciatio

n du

e to b

oth

N-N2

and

N2-N

2 co

llision

sP.

Valen

tini, T

. Sch

wartz

entru

ber,

J. Be

nder,

G. C

andle

r, Univ

ersity

of

Minn

esota

, Minn

eapo

lis, M

innea

polis,

MN

Thur

sday

, 25

June

201

525

7-F3

60-8

09

30 -

1200

hrs

The I

mpac

t of P

artic

le Im

age V

elocim

etry o

n Ae

rosp

ace T

echn

ology

Gran

d Ball

room

E

Mode

rator:

Stev

en B

eresh

, Dist

inguis

hed M

embe

r of t

he Te

chnic

al St

aff, S

andia

Nati

onal

Labo

ratori

es

P

aneli

sts:

Rona

ld J.

Adria

nRe

gent’

s Prof

essor

and I

ra A.

Fulto

n Prof

essor

of Me

chanic

al an

d Aero

space

En

ginee

ring

Arizo

na S

tate U

nivers

ity

Susa

n Go

rton

Projec

t Man

ager,

Revo

lution

ary Ve

rtical

Lift Te

chnolo

gy Pr

oject

NASA

Lang

ley Re

searc

h Cen

ter

Fulvi

o Sca

rano

Full P

rofes

sor a

nd Ch

air of

Aerod

ynam

icsDe

lft Un

iversi

ty of

Tech

nolog

y

Migu

el Vis

bal

Princi

pal R

esearc

h Aero

space

Engin

eer a

nd Te

am Le

ader

of Mu

ltidisc

iplina

ry Co

mputa

tiona

l Aero

dyna

mics,

Aeros

pace

Syste

ms Di

rector

ateAir

Force

Rese

arch L

abora

tory

107

Thur

sday

, 25

June

201

525

8-LN

CH-3

12

30 -

1400

hrs

Awar

ds Lu

nche

on: C

elebr

ating

Ach

ievem

ents

in Ai

rcraf

t and

Atm

osph

eric

Syste

msCh

antill

y Ball

room

Wes

t

A tick

et is

requir

ed an

d inc

luded

in th

e con

feren

ce re

gistra

tion f

ee w

here

indica

ted.

Thur

sday

, 25

June

201

525

9-AA

-37

Land

ing G

ear N

oise

Edelw

eiss

Chair

ed by

: T. S

PALT,

NAS

A Lan

gley R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-3

255

Aero

acou

stic S

imula

tions

of a

Nose

La

nding

Gea

r usin

g FUN

3D on

Po

intwi

se U

nstru

cture

d Grid

sV.

Vatsa

, M. K

horra

mi, N

ASA L

angle

y Re

searc

h Cen

ter, H

ampto

n, VA

; J. R

hoad

s, Po

intwi

se, I

nc.,

Fort

Worth

, TX;

D.

Lock

ard, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1430

hrs

AIAA-2

015-3

256

Nose

land

ing ge

ar fl

ow an

d nois

e pr

edict

ions o

n un

struc

ture

d grid

us

ing a

cell-

cent

ered

Nav

ier-S

toke

s co

deF.

De La

Puen

te, L.

San

ders,

F. Vu

illot,

E. Ma

noha

, ONE

RA, C

hâtill

on, F

rance

1500

hrs

AIAA-2

015-3

257

The E

ffect

of Fl

ow Ci

rculat

ion on

th

e Sca

tterin

g of L

andin

g Gea

r No

iseT.

Heffe

rnon,

D. An

gland

, X. Z

hang

, M.

Smi

th, U

nivers

ity of

Sou

thamp

ton,

South

ampto

n, Un

ited K

ingdo

m

1530

hrs

AIAA-2

015-3

258

The E

ffect

of St

rut G

eome

try on

the

Inter

-Whe

el Flo

w fo

r a Tw

o-Wh

eel

Land

ing G

ear

P. Mc

Carth

y, A.

Ekme

kci, U

nivers

ity of

To

ronto,

Toron

to, Ca

nada

1600

hrs

AIAA-2

015-3

259

Desig

n of q

uieter

land

ing ge

ars

throu

gh la

ttice-B

oltzm

ann C

FD

simula

tions

T. Ro

ugier,

Safra

n Grou

p, Vé

lizy-Vi

llacou

blay,

France

; Q. B

ouvy,

Safra

n Grou

p, Glo

uceste

r, Un

ited K

ingdo

m; D.

Casal

ino, J

. App

elbau

m,

Exa G

mbH,

Stuttg

art, G

erman

y; C.

Kleinc

laus,

Exa G

mbH,

Munic

h, Ge

rman

y

Thur

sday

, 25

June

201

526

0-AA

-38

Fluid-

Struc

ture

Inter

actio

nFle

ur-d

e-lis

ACh

aired

by: J

. ALO

NSO-

MIRA

LLES,

UTC

Aeros

pace

Sys

tems

1400

hrs

AIAA-2

015-3

260

A fa

st nu

meric

al fra

mewo

rk

for a

cous

tic sc

atter

ing by

3D

poro

elasti

c plat

esW.

Wolf

, Univ

ersity

of Ca

mpina

s, Ca

mpina

s, Br

azil;

A. Ca

valie

ri, Te

chno

logica

l Insti

tute o

f Aero

nauti

cs (IT

A), S

ão Jo

sé do

s Cam

pos,

Braz

il

1430

hrs

AIAA-2

015-3

261

Noise

Pro

duce

d by F

abric

and W

ire

Mesh

Cove

red P

anels

in Lo

w-Sp

eed

Anec

hoic

Wind

Tunn

elsW.

Alex

ande

r, W. D

even

port,

Virg

inia

Polyt

echn

ic Ins

titute

and S

tate U

nivers

ity,

Black

sburg

, VA

1500

hrs

AIAA-2

015-3

262

Acou

stic s

catte

ring b

y finit

e co

mpos

ite pl

ates

A. Ca

valie

ri, M.

Don

adon

, Tec

hnolo

gical

Institu

te of

Aeron

autic

s (ITA

), Sã

o Jos

é do

s Cam

pos,

Braz

il; W.

Wolf

, Univ

ersity

of

Camp

inas,

Camp

inas,

Braz

il

1530

hrs

AIAA-2

015-3

263

Expe

rimen

tal I

nves

tigat

ion of

Flow

-In

duce

d Pan

el Vib

ratio

ns at

Cruis

e Ma

ch N

umbe

rT.

Berke

feld,

C. Sp

ehr, K

. Ehre

nfried

, S.

Haxte

r, Germ

an Ae

rospa

ce Ce

nter (

DLR)

, Gö

ttinge

n, Ge

rman

y; S.

Kroe

ber, D

aimler

AG

, Stut

tgart,

Germ

any

1600

hrs

AIAA-2

015-3

264

Rod-

Airfo

il Int

erac

tion

Noise

Re

ducti

on U

sing L

eadin

g Edg

e Se

rratio

nsW.

Chen

, W. Q

iao, L

. Wan

g, F.

Tong

, No

rthwe

stern

Polyt

echn

ical U

nivers

ity,

Xi’an

, Chin

a; X.

Wan

g, St

ate Ke

y La

borat

ory of

Aerod

ynam

ics, M

ianya

ng,

China

1630

hrs

AIAA-2

015-3

265

Comp

ariso

n of

Ana

lytica

l, Nu

meric

al, an

d Exp

erim

enta

l Re

sults

for U

nstea

dy A

erof

oil

Inter

actio

n No

iseL.

Ayton

, Univ

ersity

of Ca

mbrid

ge,

Camb

ridge

, Unit

ed Ki

ngdo

m; J.

Gill,

Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom;

N. P

eake

, Univ

ersity

of

Camb

ridge

, Cam

bridg

e, Un

ited K

ingdo

m

Thur

sday

, 25

June

201

526

1-AA

-39

Fluid

Acou

stic P

heno

mena

Fleur

-de-

lis B

Chair

ed by

: K. A

HUJA

, Geo

rgia I

nstitu

te of

Tech

nolog

y14

00 hr

sAIA

A-201

5-326

6No

n-lin

ear S

ystem

Iden

tifica

tion

Tech

nique

s for

Dete

rmina

tion

of th

e Aco

ustic

Pro

perti

es of

Pe

rfora

tesH.

Bod

en, R

oyal

Institu

te of

Tech

nolog

y (K

TH),

Stoc

kholm

, Swe

den

1430

hrs

AIAA-2

015-3

267

Vorte

x Sc

atter

ing Ef

fects

on

Acou

stic W

ave P

ropa

gatio

nG.

Ke, W

. Li, Z

. Zhe

ng, U

nivers

ity of

Ka

nsas

, Law

rence

, Law

rence

, KS

1500

hrs

AIAA-2

015-3

268

Nume

rical

Inve

stiga

tion

of th

e Re

fracti

on Ef

fects

by Je

t Flow

s in

Anec

hoic

Wind

Tunn

els, w

ith

Appli

catio

n to

NAS

A/La

RC Q

uiet

Flow

Facil

ityS.

Redo

nnet,

J. B

ulte,

ONER

A, Ch

âtillo

n, Fra

nce

1530

hrs

AIAA-2

015-3

269

On th

e mec

hanis

ms of

nois

e re

ducti

on in

aero

foil-

turb

ulenc

e int

erac

tion

by u

sing w

avy l

eadin

g ed

ges

S. H

aeri,

J. Kim

, P. J

osep

h, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d Kin

gdom

1600

hrs

AIAA-2

015-3

270

Noise

Radia

tion f

rom

a Cyli

ndric

al Em

bossm

ent Im

merse

d in T

urbu

lent

Boun

dary

Laye

r Flow

B. Bry

an, S

. Gleg

g, Flo

rida A

tlanti

c Univ

ersity,

Bo

ca Ra

ton, F

L; M.

Awast

hi, W

. Alex

ande

r, W.

Deve

nport

, Virg

inia Po

lytech

nic In

stitute

and

State

Unive

rsity,

Blacks

burg,

VA

108

Thur

sday

, 25

June

201

526

2-AA

-40

Adva

nced

Testi

ng Te

chniq

ues

Inve

rnes

sCh

aired

by: J

. UND

ERBR

INK

1400

hrs

AIAA-2

015-3

271

Optim

izatio

n of

Micr

opho

ne

Loca

tions

for A

cous

tic Li

ner

Impe

danc

e Edu

ction

M. Jo

nes,

W. W

atson

, NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA; J

. Ju

ne, U

nivers

ity of

Flori

da, G

aines

ville,

Ga

inesv

ille, F

L

1430

hrs

AIAA-2

015-3

272

Adva

nced

Bac

kgro

und S

ubtra

ction

Ap

plied

to A

eroa

cous

tic W

ind

Tunn

el Te

sting

C. Ba

hr, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA;

W. H

orne,

NASA

Ames

Re

searc

h Cen

ter, M

offett

Field

, CA

1500

hrs

AIAA-2

015-3

273

Redu

cing t

he Ef

fect o

f Tra

nsdu

cer

Moun

t Indu

ced N

oise o

n Aero

acou

stic

Wind

Tunn

el Tes

ting D

ata w

ith a

New

Trans

ducer

Mou

nt De

sign

A. He

rron,

D. Re

ed, D

. Nan

ce, N

ASA M

arsha

ll Sp

ace Fl

ight C

enter

, Hun

tsville

, AL

1530

hrs

AIAA-2

015-3

274

Beam

form

ing-b

ased

nois

e lev

el de

reve

rber

ation

solut

ion fo

r S1M

A so

nic w

ind-tu

nnel

: metr

ology

, me

thod

ology

and v

alida

tion

F. Me

ry, O

NERA

, Mod

ane,

Franc

e; R.

Davy

, V. F

leury,

J. B

ulte,

M. Re

y, ON

ERA,

Châti

llon,

Franc

e

1600

hrs

AIAA-2

015-3

275

Impe

danc

e edu

ction

of pe

rfora

ted

plates

at lo

w Sto

uhal

numb

ers an

d hig

h bias

flow

Mac

h num

ber

V. Po

pie, E

. Piot

, ONE

RA, T

oulou

se, Fr

ance;

S.

Torde

ux, F

rench

Natio

nal In

stitute

for R

esearc

h in

Comp

uter S

cience

and C

ontro

l (INR

IA), P

au,

France

; F. Si

mon,

ONER

A, Tou

louse,

Fran

ce

1630

hrs

AIAA-2

015-3

276

Effect

s of H

ologr

am D

istan

ce an

d Re

gular

izatio

n Tech

nique

s on V

ariou

s Me

thods

of N

earfi

eld Ac

ousti

c Ho

logra

phy A

pplie

d to B

uildin

g Le

akag

e Dete

ction

/Qua

ntific

ation

K. Ch

elliah

, G. R

aman

, R. M

uehle

isen,

Illinois

Ins

titute

of Tec

hnolo

gy, Ch

icago

, IL

Thur

sday

, 25

June

201

526

3-AA

-41

CAA

Nume

rical

Tech

nique

s IV

Laliq

ueCh

aired

by: P

. MOR

RIS, P

enns

ylvan

ia St

ate U

nivers

ity14

00 hr

sAIA

A-201

5-327

7Pe

rform

ance

of th

e DGM

for t

he

Linea

rized

Euler

Equa

tions

With

No

n-Un

iform

Mea

n-Flo

wM.

Willi

amsch

en, G

. Gab

ard, U

nivers

ity

of So

utham

pton,

South

ampto

n, Un

ited

Kingd

om

1430

hrs

AIAA-2

015-3

278

Towa

rds C

AA B

ased

Aco

ustic

Wind

Tu

nnel

Corre

ction

s for

Rea

listic

Sh

ear L

ayer

sJ.

Jiao,

J. De

lfs, J

. Dier

ke, G

erman

Ae

rospa

ce Ce

nter (

DLR)

, Brau

nsch

weig,

Ge

rman

y

1500

hrs

AIAA-2

015-3

279

High

-Ord

er H

ybrid

Cell-

Cent

ered

Me

thod

for C

ompu

tatio

nal

Aero

acou

stics

M. W

ang,

R. Fa

ttah,

D. An

gland

, X.

Zhan

g, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom

1530

hrs

AIAA-2

015-3

280

A Sp

ectra

l-BEM

Form

ulatio

n fo

r Co

mpac

t Sou

rces A

eroa

cous

tics

G. B

ernard

ini, R

oma T

re Un

iversi

ty, Ro

me,

Italy;

C. Te

sta, I

talian

Insti

tute f

or Na

val

Hydro

dyna

mic R

esea

rch an

d Ship

Mod

el Ba

sin, R

ome,

Italy;

M. G

enna

retti,

Roma

Tre

Univ

ersity

, Rom

e, Ita

ly

1600

hrs

AIAA-2

015-3

281

A Sta

bilise

d High

-Ord

er Fi

nite

Eleme

nt M

odel

for t

he Li

near

ised

Euler

Equa

tions

K. Ha

mich

e, H.

Béri

ot, S

iemen

s, Le

uven

, Be

lgium

; G. G

abard

, Univ

ersity

of

South

ampto

n, So

utham

pton,

Unite

d Kin

gdom

Thur

sday

, 25

June

201

526

4-AA

-42

Fan

Broa

dban

d Nois

e Pre

dictio

nOb

elisk

ACh

aired

by: E

. ENV

IA, N

ASA G

lenn R

esea

rch Ce

nter

1400

hrs

AIAA-2

015-3

282

Harm

onic

and B

road

band

Se

para

tion

of N

oise f

rom

a Sma

ll Du

cted F

anA.

Truon

g, D.

Papa

mosch

ou, U

nivers

ity of

Ca

liforni

a, Irv

ine, I

rvine

, CA

1430

hrs

AIAA-2

015-3

283

Furth

er In

vesti

gatio

ns In

to a

Low-

Orde

r Mod

el of

Fan

Broa

dban

d No

iseS.

Grac

e, Bo

ston U

nivers

ity, B

oston

, MA

1500

hrs

Pane

lFa

n Bro

adba

nd N

oise P

redict

ion Pa

nel

E. En

via, N

ASA G

lenn R

esearc

h Cen

ter, C

levela

nd, O

H; J.

Coup

land,

Unive

rsity o

f Sou

thamp

ton, S

outha

mpton

, Unit

ed Ki

ngdo

m

Thur

sday

, 25

June

201

526

5-AC

D-7

Aircr

aft S

ubsy

stems

, Int

egra

tion,

and A

rchite

cture

sWy

ethCh

aired

by: P

. RAJ

, Virg

inia P

olytec

hnic

Institu

te an

d Stat

e Univ

ersity

and E

. DIG

IROLA

MO, L

ockh

eed M

artin

Aeron

autic

s14

00 hr

sAIA

A-201

5-328

4An

Inno

vativ

e All-

Activ

e Hyb

rid

Actu

ation

Syste

mT.

Röbe

n, RW

TH Aa

chen

Univ

ersity

, Aa

chen

, Germ

any

1430

hrs

AIAA-2

015-3

285

Dyna

mic R

econfi

gura

tion m

echan

ism

for D

istrib

uted I

ntegr

ated M

odula

r Av

ionics

Syste

mQ.

Gu,

G. W

ang,

J. W

u, M.

Wan

g, Ch

ina

Natio

nal A

erona

utica

l Rad

io Ele

ctron

ics

Rese

arch I

nstitu

te, S

hang

hai, C

hina

1500

hrs

AIAA-2

015-3

286

Deve

lopme

nt of

an In

tegra

ted

UAS f

or A

gricu

ltura

l Ima

ging

Appli

catio

nsN.

Goli

, B. L

andru

m, U

nivers

ity of

Ala

bama

, Hun

tsville

, Hun

tsville

, AL

1530

hrs

AIAA-2

015-3

287

Major

Airc

raft

Subs

ystem

Effe

cts on

Ga

s Tur

bine P

erfo

rman

ce in

Mor

e Ele

ctric

Aircr

aft A

rchite

cture

sM.

Ozc

an, I

. Cha

krabo

rty, D

. Mav

ris,

Georg

ia Ins

titute

of Te

chno

logy,

Atlan

ta,

GA

1600

hrs

AIAA-2

015-3

288

Desig

n an

d Buil

d of S

warm

Qu

adro

tor U

AVs a

t UGS

S. S

rigrar

om, H

. Lin,

Z. S

aw, J

. Zha

ng,

C. Lim

, Univ

ersity

of G

lasgo

w, S

ingap

ore,

Singa

pore

109

Thur

sday

, 25

June

201

526

6-AM

T-13/

GT-1

3Th

e Imp

act o

f PIV

on A

eros

pace

Tech

nolog

y II

Topa

zCh

aired

by: S

. BER

ESH,

San

dia N

ation

al La

borat

ories

and K

. LOW

E, Vir

ginia

Tech

1400

hrs

Oral

Prese

ntatio

nUs

e of P

IV to

anch

or co

mput

ation

al an

alysis

of fr

ee sh

ear a

nd w

all

boun

ded fl

ows (

Invit

ed)

D. G

aiton

de, O

hio S

tate U

nivers

ity,

Colum

bus,

OH

1430

hrs

Oral

Prese

ntatio

nSy

nerg

istic

Inter

actio

ns of

High

-Re

solut

ion CF

D an

d PIV

to R

evea

l Co

mplex

Uns

teady

Flow

Phy

sics

(Invit

ed)

M. V

isbal,

Air F

orce R

esea

rch La

borat

ory,

Wrig

ht-Pa

tterso

n AFB

, OH

1500

hrs

Oral

Prese

ntatio

nPI

V unc

erta

inty:

how

good

are P

IV

meas

urem

ents?

(Inv

ited)

A. Sc

iacch

itano

, F. S

caran

o, De

lft Un

iversi

ty of

Tech

nolog

y, De

lft, Th

e Ne

therla

nds

1530

hrs

Oral

Prese

ntatio

nTo

mogr

aphic

and t

ime-

reso

lved

PIV:

Addin

g dim

ensio

ns to

flow

dia

gnos

tics (

Invit

ed)

K. Ly

nch,

F. Sc

arano

, Delf

t Univ

ersity

of

Tech

nolog

y, De

lft, Th

e Neth

erlan

ds

1600

hrs

Oral

Prese

ntatio

nPI

V App

licat

ions i

n Su

perso

nic

Comb

ustio

n Wi

nd Tu

nnels

at A

FRL

(Invit

ed)

S. Pe

ltier, C

. Cart

er, Ai

r Forc

e Res

earch

La

borat

ory, W

right-

Patte

rson A

FB, O

H

1630

hrs

Oral

Prese

ntatio

nPIV

in ga

s tur

bine c

ombu

stion

ch

ambe

rs: N

ew in

sights

into

flow

phys

ics an

d its

impo

rtanc

e for

co

mbus

tor de

velop

ment

M. St

ohr, I

. Box

x, O.

Lamm

el, K.

Obe

rleith

ner,

C. Arn

dt, W

. Meie

r, Germ

an Ae

rospa

ce Ce

nter

(DLR

), Stu

ttgart

, Germ

any

1700

hrs

Oral

Prese

ntatio

nA

Tribu

te to

Ron

Adr

ian: T

hree

De

cade

s of P

IV In

nova

tion

(Invit

ed)

S. G

ogine

ni, S

pectr

al En

ergies

, LLC

, Da

yton,

OH

Thur

sday

, 25

June

201

526

7-AP

A-29

Inno

vativ

e Aer

odyn

amic

Conc

epts

& De

signs

Carp

enter

Ball

room

Chair

ed by

: V. B

HAGW

ANDI

N, U

S Arm

y Res

earch

Labo

ratory

and J

. LAT

Z, No

rthrop

Grum

man A

erosp

ace S

ystem

s14

00 hr

sAIA

A-201

5-328

9Ev

aluat

ion of

Ada

ptive

Comp

liant

Tra

iling E

dge T

echn

ology

S. W

akay

ama,

The B

oeing

Comp

any,

Hunti

ngton

Bea

ch, C

A; E.

Whit

e, Th

e Bo

eing C

ompa

ny, B

erkele

y, MO

1430

hrs

AIAA-2

015-3

290

Deter

mina

tion o

f Sect

ion Ae

rody

nami

c Op

eratin

g Con

dition

on W

ings a

nd

Rotor

Blad

es Fro

m Le

ading

-Edge

Pr

essur

e Mea

surem

ents

A. Sa

ini, A.

Gopa

larath

nam,

Nort

h Caro

lina

State

Unive

rsity,

Raleig

h, NC

1500

hrs

AIAA-2

015-3

291

Para

metri

c Stu

dy of

Box

-Wing

Ae

rody

nami

cs fo

r Mini

mum

Drag

Und

er St

abilit

y and

Ma

neuv

erab

ility C

onstr

aints

S. An

drews

, R. P

erez,

Roya

l Milit

ary

Colle

ge of

Cana

da, K

ingsto

n, Ca

nada

1530

hrs

AIAA-2

015-3

292

Optim

izatio

n of

the A

erod

ynam

ic Pe

rform

ance

of R

egion

al an

d Wide

-Bo

dy-C

lass B

lende

d Wing

-Bod

y Ai

rcraf

tT.

Reist

, D. Z

ingg,

Unive

rsity

of To

ronto,

To

ronto,

Cana

da

1600

hrs

AIAA-2

015-3

293

A no

vel a

erod

ynam

ic su

rface

for

redir

ectin

g the

boun

dary

laye

rE.

Sahe

by, G

. Hua

ng, W

. Qiao

, W. T

ang,

Nanji

ng U

nivers

ity of

Aeron

autic

s and

As

trona

utics,

Nan

jing,

China

Thur

sday

, 25

June

201

526

8-AP

A-30

Low

Spee

d, Lo

w Re

ynold

s Num

ber A

erod

ynam

icsGr

and B

allro

om A

Chair

ed by

: Z. Y

ANG,

Wrig

ht St

ate U

nivers

ity an

d A. J

ONES

, Univ

ersity

of M

arylan

d14

00 hr

sAIA

A-201

5-329

4Nu

meric

al inv

estig

ation

of fi

nite-

aspe

ct ra

tio pl

ate fl

ows i

n gr

ound

ef

fect

A. Me

dina,

R. Sin

gh, A

rmy R

esea

rch

Labo

ratory

, Abe

rdeen

Prov

ing G

round

, MD

1430

hrs

AIAA-2

015-3

295

Prop

ulsion

of a

Plung

ing Fl

exibl

e Ai

rfoil u

sing a

Torsi

on Sp

ring M

odel

N. Ar

ora, A

. Gup

ta, In

dian I

nstitu

te of

Tech

nolog

y Delh

i, New

Delh

i, Ind

ia; H

. Ao

no, J

apan

Aeros

pace

Explo

ration

Agen

cy

(JAXA

), Sa

gami

hara,

Japa

n; W.

Shy

y, Ho

ng Ko

ng U

nivers

ity of

Scie

nce a

nd

Tech

nolog

y, Cle

ar Wa

ter B

ay, H

ong K

ong

1500

hrs

AIAA-2

015-3

296

Blad

e Elem

ent M

omen

tum

Mode

ling o

f Low

-Re S

mall U

AS

Electr

ic Pr

opuls

ion Sy

stems

M. M

cCrin

k, J.

Greg

ory, O

hio S

tate

Unive

rsity,

Colum

bus,

OH

1530

hrs

AIAA-2

015-3

297

Stere

osco

pic P

IV an

alysis

on ro

tary

pla

tes in

burst

ingA.

Medin

a, Arm

y Res

earch

Labo

ratory

, Ab

erdee

n Prov

ing G

round

, MD;

A. Jo

nes,

Unive

rsity

of Ma

rylan

d, Co

llege

Park,

Co

llege

Park,

MD

Thur

sday

, 25

June

201

526

9-AP

A-31

Vorti

cal/V

ortex

Flow

Stemm

ons B

Chair

ed by

: M. J

URKO

VICH,

US

Air Fo

rce an

d T. D

OUVIL

LE, T

LG Ae

rospa

ce, L

LC.

1400

hrs

AIAA-2

015-3

298

Near

Gro

und A

ircra

ft Wa

ke

Dissi

patio

n wi

th O

bsta

cles

C. Wa

ng, J

. Sch

luter,

Nan

yang

Te

chno

logica

l Univ

ersity

, Sing

apore

, Sin

gapo

re

1430

hrs

AIAA-2

015-3

299

Effe

cts of

Spinn

ing M

otion

on th

e Tra

pped

Vorte

x Co

mbus

tors

S. Ch

en, R

. Chu

e, J.

Schlu

ter, N

anya

ng

Tech

nolog

ical U

nivers

ity, S

ingap

ore,

Singa

pore;

S. Y

u, Sin

gapo

re Ins

titute

of Te

chno

logy,

Singa

pore,

Sing

apore

1500

hrs

AIAA-2

015-3

300

Trailin

g Vor

tex-In

duce

d Loa

ds

Durin

g Clos

e Enc

ount

ers i

n Cr

uise

M. M

ende

nhall

, D. L

esieu

tre, N

ielse

n En

ginee

ring &

Rese

arch,

Inc.,

Santa

Clara

, CA

; M. K

elly,

NASA

Lang

ley Re

searc

h Ce

nter, H

ampto

n, VA

1530

hrs

AIAA-2

015-3

301

Simula

ting A

ircra

ft Wa

ke Vo

rtice

s wi

th O

VERF

LOW

D. S

chau

erham

er, S

. Rob

inson

, Univ

ersity

of

Califo

rnia,

Davis

, Dav

is, CA

1600

hrs

AIAA-2

015-3

302

Inve

stiga

tion

of pr

opell

er in

duce

d gr

ound

vorti

ces b

y num

erica

l and

ex

perim

enta

l meth

ods

Y. Ya

ng, L

. Veld

huis,

G. E

itelbe

rg, D

elft

Unive

rsity

of Te

chno

logy,

Delft,

The

Nethe

rland

s

110

Thur

sday

, 25

June

201

527

0-AP

A-32

Unste

ady A

erod

ynam

ics II

Stemm

ons A

Chair

ed by

: E. F

ELTR

OP, T

he Ce

ssna A

ircraf

t Com

pany

and K

. VAN

DEN,

USA

F14

00 hr

sAIA

A-201

5-330

3Ef

fect

of B

endin

g-Os

cillat

ions o

n a S

tream

wise

-Orie

nted

Vorte

x In

terac

tion

C. Ba

rnes,

M. V

isbal,

Air F

orce R

esea

rch

Labo

ratory

, Wrig

ht-Pa

tterso

n AFB

, OH;

G.

Hua

ng, W

right

State

Univ

ersity

, Da

yton,

OH

1430

hrs

AIAA-2

015-3

304

Comp

lex ae

ro-e

ngine

inta

ke du

cts

and d

ynam

ic dis

torti

onD.

Mac

Manu

s, N.

Chier

eghin

, D. G

il Prie

to,

P. Za

chos

, Cran

field

Unive

rsity,

Cran

field,

Un

ited K

ingdo

m

1500

hrs

AIAA-2

015-3

305

Flow

disto

rtion

mea

sure

ment

s in

conv

oluted

aero

engin

e int

akes

P. Za

chos

, D. M

acMa

nus,

N. Ch

iereg

hin,

Cranfi

eld U

nivers

ity, C

ranfie

ld, U

nited

Kin

gdom

1530

hrs

AIAA-2

015-3

306

Larg

e Edd

y Sim

ulatio

ns of

Su

perso

nic Je

t Flow

s for

Ae

roac

ousti

c App

licat

ions

C. Ju

nque

ira-Ju

nior, S

. Yam

ouni,

Te

chno

logica

l Insti

tute o

f Aero

nauti

cs (IT

A), S

ão Jo

sé do

s Cam

pos,

Braz

il; J.

Azev

edo,

Aeron

autic

s and

Spa

ce In

stitut

e (IA

E), S

ão Jo

sé do

s Cam

pos,

Braz

il; W.

Wo

lf, Un

iversi

ty of

Camp

inas,

Camp

inas,

Braz

il

1600

hrs

AIAA-2

015-3

307

Unste

ady A

erod

ynam

ics

Simula

tions

of a

Seda

n-Ty

pe R

oad

Vehic

le du

ring S

inuso

idal S

teerin

g In

put

T. Na

kash

ima,

Y. Mo

rikaw

a, Hir

oshim

a Un

iversi

ty, H

igash

i-Hiro

shim

a, Ja

pan;

M.

Tsubo

kura,

Hok

kaido

Univ

ersity

, Sap

poro,

Ja

pan;

Y. Ok

ada,

T. No

uzaw

a, Ma

zda

Motor

Corpo

ration

, Aki

Gun,

Japa

n

1630

hrs

AIAA-2

015-3

308

Coup

led 6

DoF m

otion

and

Aero

dyna

mics

Simula

tion

of R

oad

Vehic

les in

Cros

swind

gusts

H. Is

hioka

, Hok

kaido

Univ

ersity

, Sap

poro,

Ja

pan;

K. On

ishi, R

IKEN

Adva

nced

Insti

tute

for Co

mputa

tiona

l Scie

nce,

Kobe

, Jap

an;

K. Na

kasa

to, N

issan

Moto

r Corp

oratio

n, Yo

koha

ma, J

apan

; T. N

akas

hima,

Hiros

hima U

nivers

ity, H

igash

i-Hiro

shim

a, Ja

pan;

M. Ts

ubok

ura, H

okka

ido U

nivers

ity,

Sapp

oro, J

apan

1700

hrs

AIAA-2

015-3

309

An U

nstea

dy A

erod

ynam

ic Mo

del

base

d on

the L

eadin

g-Ed

ge

Stagn

ation

Poin

tV.

Surya

kuma

r, Y. B

abba

r, T. S

trgan

ac,

Texa

s A&M

Univ

ersity

, Coll

ege S

tation

, TX;

A.

Mang

alam,

Tao o

f Sys

tems I

ntegra

tion,

Inc.,

Hamp

ton, V

A

Thur

sday

, 25

June

201

527

1-AP

A-33

Flow

Cont

rol A

pplic

ation

s & D

emon

strat

ions (

Activ

e & P

assiv

e) II

ISte

mmon

s CCh

aired

by: C

. TILM

ANN,

Air F

orce R

esea

ch La

borat

ory an

d S. S

ILTON

, US

Army R

esea

rch La

borat

ory14

00 hr

sAIA

A-201

5-331

0Na

nose

cond

-SDB

D Ac

tuat

ion ov

er a

Conic

al Fo

rebo

dy at

Wind

Spee

d 72

m/s a

nd A

ngle

of A

ttack

45

degr

eeJ.

Wang

, H. L

i, X. M

eng,

D. Zh

ang,

North

weste

rn Po

lytec

hnica

l Univ

ersity

, Xi’

an, C

hina;

F. Liu

, S. L

uo, U

nivers

ity of

Ca

liforni

a, Irv

ine, I

rvine

, CA

1430

hrs

AIAA-2

015-3

311

Comp

utat

ional

Evalu

ation

of Fl

ow

Cont

rol f

or En

hanc

ed Co

ntro

l Au

thor

ity af

a Ve

rtica

l Tail

A. Sh

milov

ich, Y

. Yad

lin, E

. Wha

len, T

he

Boein

g Com

pany

, Hun

tingto

n Bea

ch, C

A

1500

hrs

AIAA-2

015-3

312

Tech

nique

s for

the D

esign

of A

ctive

Flo

w Co

ntro

l Sys

tems i

n He

avy

Vehic

lesD.

Mano

salva

s, T.

Econo

mon,

F. Pala

cios,

A. Jam

eson,

Stanfo

rd Un

iversit

y, Sta

nford,

CA

1530

hrs

AIAA-2

015-3

313

Expe

rimen

tal in

vesti

gatio

n of P

assiv

e Lo

ad Re

ducti

on un

der d

ynam

ic infl

ow

cond

itions

U. Co

rdes,

K. Hu

fnage

l, C. T

ropea

, Tech

nical

Unive

rsity o

f Darm

stadt,

Darm

stadt,

Germ

any;

G. Ka

mpers

, M. H

ölling

, J. P

einke

, Univ

ersity

of

Olden

burg,

Olde

nburg

, Germ

any

1600

hrs

AIAA-2

015-3

314

Plenu

m de

sign

for c

ompa

ct flu

idic

effe

ctors

J. Ch

ard, A

. Llop

is-Pas

cual,

W. C

rowthe

r, Un

iversi

ty of

Manc

heste

r, Man

ches

ter,

Unite

d King

dom

Thur

sday

, 25

June

201

527

2-AS

E-4Ai

rcraf

t Wak

e Tur

bulen

ce II

(Inv

ited)

Plum

Blos

som

BCh

aired

by: Z

. ZHE

NG, T

he U

nivers

ity of

Kans

as an

d M. P

RUIS,

Nort

hwes

t Res

earch

Asso

ciates

Inc

1400

hrs

AIAA-2

015-3

315

Effe

ct of

Atm

osph

eric

Shee

ts an

d Lay

ers N

ear t

he G

roun

d on

Wake

Vorte

x Tra

nspo

rt an

d Dec

ay

(Invit

ed)

M. Pr

uis, D

. Deli

si, N

orthW

est R

esea

rch

Asso

ciates

, Red

mond

, WA;

D. Ja

cob,

Cohe

rent R

esea

rch G

roup,

Ormo

nd

Beac

h, FL

1430

hrs

AIAA-2

015-3

316

Fast-

time W

ake V

ortex

Mod

el Pr

edict

ions C

ompa

red w

ith

Obser

vatio

ns Be

hind L

andin

g Airc

raft

Near

the G

roun

d (Inv

ited)

M. Pr

uis, D

. Delis

i, Nort

hWest

Resea

rch

Assoc

iates,

Redm

ond,

WA; D

. Jaco

b, Co

heren

t Re

search

Grou

p, Or

mond

Beach

, FL;

D. La

i, No

rthWe

st Re

search

Assoc

iates,

Redm

ond,

WA 15

00 hr

sAIA

A-201

5-331

7Wi

nd an

d EDR

Mea

surem

ents

with

Scann

ing D

opple

r LID

ARs f

or

Prep

aring

Futur

e Wea

ther D

epen

dent

Sepa

ratio

n Con

cepts

(Invit

ed)

L. Th

obois

, R. K

rishna

murth

y, S.

Loae

c, J.

Cario

u, Leo

sphere

, Orsa

y, Fra

nce; A

. Dolfi

-Bo

uteyre

, M. V

alla, O

NERA

, Pala

iseau

, Fran

ce

1530

hrs

AIAA-2

015-3

318

Evalu

ation

of Fa

st-Tim

e Wak

e Mo

dels

using

Den

ver 2

006

Field

Expe

rimen

t Dat

aN.

Ahma

d, NA

SA La

ngley

Rese

arch

Cente

r, Ham

pton,

VA; M

. Prui

s, No

rthWe

st Re

searc

h Asso

ciates

, Sea

ttle, W

A

1600

hrs

AIAA-2

015-3

319

Aero

dyna

mic S

imula

tion

of W

ake

Enco

unter

for A

ircra

ft Clo

se

Form

ation

Ope

ratio

ns (I

nvite

d)A.

He, Z

. Zhe

ng, U

nivers

ity of

Kans

as,

Lawr

ence

, Law

rence

, KS

111

Thur

sday

, 25

June

201

527

3-AS

E-5At

mosp

heric

and S

pace

Envir

onme

nts

Plum

Blos

som

ACh

aired

by: W

. VAU

GHAN

, Willi

am W

Vaug

han C

onsu

ltant

and R

. SCU

LLY, N

ASA

1400

hrs

AIAA-2

015-3

320

Light

ning P

rotec

tion

for t

he O

rion

Spac

e Veh

icle

R. Sc

ully,

NASA

John

son S

pace

Cente

r, Ho

uston

, TX

1430

hrs

AIAA-2

015-3

321

Adva

nced

Spac

ecra

ft Sy

stems

Em

ulatio

n fo

r Spa

ce En

viron

ment

Qu

alific

ation

Testi

ngH.

Ruma

nn, B

astio

n Tec

hnolo

gies,

Inc.,

Hous

ton, T

X

1500

hrs

AIAA-2

015-3

322

Inve

stiga

tion

of th

e Imp

act o

f Su

rface

Blen

ding a

nd U

ltrav

iolet

Radia

tion

Expo

sure

on El

asto

mer

Seal

Leak

Rat

e Per

form

ance

for

Spac

e Sea

l App

licat

ions

S. Ta

ylor, U

nivers

ity of

Toled

o, To

ledo,

OH;

J. Ma

ther, C

. Dan

iels,

Unive

rsity

of Ak

ron,

Akron

, OH

1530

hrs

AIAA-2

015-3

323

Elasto

mer S

eal P

erfo

rman

ce af

ter

Terre

strial

Ultr

aviol

et Ra

diatio

n Ex

posu

reC.

Danie

ls, J.

Math

er, H

. Orav

ec, U

nivers

ity

of Ak

ron, A

kron,

OH; S

. Tay

lor, U

nivers

ity

of To

ledo,

Toled

o, OH

; P. D

unlap

, NAS

A Gle

nn Re

searc

h Cen

ter, C

levela

nd, O

H

1600

hrs

AIAA-2

015-3

324

Ener

gy-A

ware

Pat

h Op

timiza

tion

for P

ersis

tent S

ampli

ng of

Seve

re

Storm

sW.

Silv

a, E.

Frew,

Univ

ersity

of Co

lorad

o, Bo

ulder,

Bou

lder, C

O

1630

hrs

AIAA-2

015-3

325

Ride

Qua

lity W

ithin

Trail A

ircra

ft In

Fo

rmat

ion Fl

ight

W. O

kolo,

A. D

ogan

, Univ

ersity

of Te

xas,

Arling

ton, A

rlingto

n, TX

; W. B

lake,

Air

Force

Rese

arch L

abora

tory,

Wrig

ht-Pa

tterso

n AFB

, OH

1700

hrs

AIAA-2

015-3

326

Math

emat

ical M

odell

ing fo

r Car

bon

Diox

ide Eq

uivale

nt P

redic

tion

of

Gree

nhou

se G

ases

Emitt

ed fr

om a

Small

Scale

Turb

ojet E

ngine

Y. Ş

öhret

, T. K

arako

c, An

adolu

Univ

ersity

, Es

kiseh

ir, Tu

rkey;

N. Ka

rakoç

, Osm

anga

zi Un

iversi

ty, Es

kiseh

ir, Tu

rkey

Thur

sday

, 25

June

201

527

4-AT

IO-2

4UA

S Int

egra

tion

& Op

erat

ions I

Ming

Chair

ed by

: V. S

CHUL

TZ, N

ASA L

angle

y Res

earch

Cente

r14

00 hr

sAIA

A-201

5-332

7An

Evalu

ation

of D

etect

and A

void

(DAA

) Disp

lays f

or U

nman

ned A

ircra

ft Sy

stems

: The

Effec

t of I

nform

ation

Le

vel a

nd D

isplay

Loca

tion o

n Pilo

t Pe

rform

ance

L. Fe

rn, R.

Rorie

, San

Jose

State

Unive

rsity,

Moffe

tt Field

, CA;

J. Pa

ck, In

foscite

x Co

rporat

ion, D

ayton

, OH;

J. Sh

ively,

NASA

Am

es Re

search

Cente

r, Moff

ett Fi

eld, C

A; M.

Dra

per, A

ir Forc

e Rese

arch L

abora

tory,

Wrigh

t-Pa

tterso

n AFB

, OH

1430

hrs

AIAA-2

015-3

328

Syste

m De

velop

ment

for t

he N

ASA

UAS A

irspa

ce O

pera

tions

Chall

enge

S. Fe

hrenb

ach,

Z. Ba

rbeau

, J. J

acob

, G.

Chow

dhary

, Okla

homa

Stat

e Univ

ersity

, St

illwate

r, OK

1500

hrs

AIAA-2

015-3

329

Platfo

rm-In

depe

nden

t Geo

fenc

ing

for L

ow A

ltitud

e UAS

Ope

ratio

nsM.

Stev

ens,

B. Co

loe, E

. Atki

ns, U

nivers

ity

of Mi

chiga

n, An

n Arbo

r, Ann

Arbo

r, MI

Thur

sday

, 25

June

201

527

5-AT

IO-2

5AT

M VI

- Ma

nage

ment

of N

AS R

esou

rces

Moro

ccoCh

aired

by: K

. MAR

AIS, P

urdue

Univ

ersity

1400

hrs

AIAA-2

015-3

330

Strat

egic

Air T

raffi

c Plan

ning w

ith

Frec

het D

istan

ce A

ggre

gatio

n an

d Re

rout

ingA.

Bomb

elli, L

. Sole

r, K. M

ease

, Univ

ersity

of

Califo

rnia,

Irvine

, Irvi

ne, C

A

1430

hrs

AIAA-2

015-3

331

Perfo

rman

ce Im

pact

of Im

prov

ed

Depa

rture

Time

Pre

dictio

n Re

lative

to

Secto

r Dem

and &

Arri

val T

ime

Pred

ictab

ility

R. Cu

rran,

E. Ko

nnem

ann,

Delft

Unive

rsity

of Te

chno

logy,

Delft,

The N

etherl

ands

; S.

Mahli

ch, E

UROC

ONTR

OL, B

retign

y, Fra

nce

1500

hrs

AIAA-2

015-3

332

Proa

ctive

and R

eacti

ve

Mana

geme

nt of

Non

-Wea

ther

Ca

pacit

y Disr

uptio

n Ev

ents

in th

e Na

tiona

l Airs

pace

Syste

m: A

Flow

Mo

delin

g and

Des

ign A

ppro

ach

S. Ro

y, Wa

shing

ton S

tate U

nivers

ity,

Pullm

an, W

A; Y.

Wan,

Unive

rsity

of No

rth

Texa

s, De

nton,

TX

1530

hrs

AIAA-2

015-3

333

Prob

abilis

tic Ti

me-S

eries

Mod

els fo

r Gr

ound

Dela

y Pro

gram

Dec

ision

Su

ppor

tE.

Vargo

, C. T

aylor

, C. W

anke

, MITR

E Co

rporat

ion, M

cLean

, VA

1600

hrs

AIAA-2

015-3

334

Analy

tical

Iden

tifica

tion

and

Rank

ing of

Chok

e Poin

ts in

the

Natio

nal A

irspa

ce Sy

stem

D. Lo

ng, S

. Has

an, V

. Stou

ffer, L

MI,

McLe

an, V

A; K.

Rama

moort

hy, S

aab

Sens

is Co

rporat

ion, E

ast S

yracu

se, N

Y; H.

Idr

is, En

gility

Corpo

ration

, Bille

rica,

MA; B

. Ba

llard,

GRA

, Inc

., Je

nkint

own,

PA; e

t al.

1630

hrs

AIAA-2

015-3

335

Stake

holde

r Fee

dbac

k-Bas

ed

Identi

ficati

on, R

ankin

g, an

d Cau

ses of

Ch

oke P

oints

in the

Nati

onal

Airsp

ace

Syste

mM.

Alcab

in, Th

e Boe

ing Co

mpan

y, Se

attle,

WA

; R. G

olasze

wski,

GRA,

Inc., J

enkin

town,

PA; W

. Cott

on, C

otton

Aviat

ion En

terpri

ses,

Lake

way,

TX; V

. Stou

ffer, L

MI, M

cLean

, VA;

J. Mu

siak,

The B

oeing

Comp

any,

Seatt

le, W

A

112

Thur

sday

, 25

June

201

527

6-AT

IO-2

6Tra

nsfo

rmat

ional

Fligh

t - U

ncon

vent

ional

VTOL

Confi

gura

tions

Mone

t Ball

room

Chair

ed by

: I. C

HOUT

APAL

LI, Th

e Univ

ersity

of Te

xas -

Pan A

meric

an14

00 hr

sOr

al Pre

senta

tion

Fligh

t Tes

t Res

ults f

or th

e DZY

NE

ROTO

Rwing

- A

High

Endu

ranc

e VT

OL Co

ncep

tM.

Page

, DZY

NE Te

chno

logies

, Irvi

ne, C

A

1430

hrs

AIAA-2

015-3

336

Desig

n and

Testi

ng of

the J

oby L

otus

Multif

uncti

onal

Rotor

VTOL

UAV

P. Sin

ha, T

ransit

ion Ro

botic

s, Inc

., Sa

nta

Cruz,

CA; A

. Stol

l, B. G

oldsm

ith, J

oby

Aviat

ion, S

anta

Cruz,

CA

1500

hrs

Oral

Prese

ntatio

nDe

sign

and T

estin

g of t

he Jo

by S2

Ele

ctric

VTOL

PAV P

rope

llers

A. St

oll, P

. Pei,

A. Cl

ark, J

. Bev

irt, Jo

by

Aviat

ion, S

anta

Cruz,

CA

1530

hrs

AIAA-2

015-3

337

Integ

ratio

n of

Elec

tric P

ropu

lsion

in

Effic

ient H

eavy

-Lift

VTOL

Conc

ept

E. De

mers

Bouc

hard,

D. R

anco

urt, D

. Ma

vris,

Georg

ia Ins

titute

of Te

chno

logy,

Atlan

ta, G

A

1600

hrs

Oral

Prese

ntatio

nTh

e Cen

trifu

gally

Stiff

ened

Rot

or

(CSR

) VTO

L Lon

g End

uran

ce

Conc

ept

M. M

oore,

NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

Thur

sday

, 25

June

201

527

7-F3

60-9

14

00 -

1630

hrs

Supe

rcomp

uting

: Roa

dmap

and i

ts Fu

ture

Role

in A

eros

pace

Engin

eerin

gGr

and B

allro

om E

Mode

rator:

Dou

g Clin

e, Te

chnic

al Le

ad, H

igh Pe

rform

ance

Comp

uting

, Loc

khee

d Mart

in Ae

ronau

tics

P

aneli

sts:

Willia

m Gr

opp

Thom

as M

. Sieb

el Ch

air, D

epart

ment

of Co

mpute

r Scie

nce a

nd

Direc

tor, P

aralle

l Com

putin

g Ins

titute

Unive

rsity

of Illi

nois

at Ur

bana

-Cham

paign

Brian

Mitc

hell

Senio

r Prin

cipal

Engin

eer

GE G

lobal

Rese

arch

Mark

Seag

erInt

el Fe

llow

CTO,

High

Perfo

rman

ce Co

mputi

ng Ec

osys

tem,

Intel

Corpo

ration

Jef D

awso

nAp

plica

tions

Man

ager

Cray,

Inc.

Thur

sday

, 25

June

201

527

8-FD

-30

Hype

rsonic

and C

hemi

cally

-Rea

cting

Flow

sSa

pphir

eCh

aired

by: B

. WHE

ATON

, The

John

s Hop

kins U

nivers

ity Ap

plied

Phys

ics La

borat

ory an

d J. S

MITH

, San

dia N

ation

al La

borat

ories

1400

hrs

AIAA-2

015-3

338

Starti

ng Ch

arac

terist

ics of

the U

S Ai

r For

ce A

cade

my M

ach

6 Lu

dwieg

Tu

beR.

Deck

er, M

. Sem

per, J

. Anth

ony,

R. Cu

mming

s, U.

S. Ai

r Forc

e Aca

demy

, Co

lorad

o Spri

ngs,

CO

1430

hrs

AIAA-2

015-3

339

Nume

rical

Mode

ling a

nd Si

mulat

ion

of Co

mbus

tion

Phen

omen

a Rela

ted

to Th

erma

l Ign

ition

and F

lame

Fron

tsW.

Tave

rnetti,

M. H

afez,

Unive

rsity

of Ca

liforni

a, Da

vis, D

avis,

CA

1500

hrs

AIAA-2

015-3

340

Larg

e-Edd

y Sim

ulatio

n of A

utoign

ition-

Domi

nated

Supe

rsonic

Comb

ustio

nG.

Cand

ler, P

. Sub

bared

dy, U

nivers

ity of

Mi

nnes

ota, M

innea

polis,

Minn

eapo

lis,

MN; N

. Cym

balist

, P. D

imota

kis, C

alifor

nia

Institu

te of

Tech

nolog

y, Pa

sade

na, C

A

1530

hrs

AIAA-2

015-3

341

A Nu

meric

al Sc

heme

for H

yper

sonic

Tu

rbule

nt Fl

owM.

Righ

i, Zuri

ch U

nivers

ity of

Appli

ed

Scien

ces,

Wint

erthu

r, Swi

tzerla

nd

Thur

sday

, 25

June

201

527

9-FD

-31

Flow

Cont

rol -

Vorti

cal F

lows

Sena

tors

Lectu

re H

allCh

aired

by: M

. YU,

Univ

ersity

of M

arylan

d, Ba

ltimore

Coun

ty an

d L. P

ACK M

ELTO

N, N

ASA-L

angle

y Res

earch

Cente

r14

00 hr

sAIA

A-201

5-334

2Ob

serv

ation

s on

the M

ean

and

Turb

ulent

Wak

e of a

Micr

o-Ra

mp

Arra

yE.

Bayd

ar, F.

Lu, U

nivers

ity of

Texa

s, Arl

ington

, Arlin

gton,

TX; J

. Slat

er, N

ASA

Glenn

Rese

arch C

enter

, Clev

eland

, OH

1430

hrs

AIAA-2

015-3

343

Mixin

g Lay

er: N

umer

ical a

nd

Expe

rimen

tal C

ontro

l Stra

tegies

J. Lit

tle, U

nivers

ity of

Arizo

na, T

ucso

n, Tu

cson,

AZ; U

. Kau

l, NAS

A Ame

s Res

earch

Ce

nter, M

offett

Field

, CA

1500

hrs

AIAA-2

015-3

344

Effe

cts of

Puls

e Ene

rgy o

n Sh

ear

Laye

r Con

trol u

sing S

urfa

ce P

lasma

Di

schar

ges

D. Ak

ins, A

. Sing

h, J.

Little

, Univ

ersity

of

Arizo

na, T

ucso

n, Tu

cson,

AZ

1530

hrs

AIAA-2

015-3

345

Towa

rds i

nteg

ral b

ound

ary l

ayer

mo

dellin

g of v

ane-

type

vorte

x ge

nera

tors

D. B

aldac

chino

, C. S

imao

Ferre

ira, G

. van

Bu

ssel, D

elft U

nivers

ity of

Tech

nolog

y, De

lft, Th

e Neth

erlan

ds

113

Thur

sday

, 25

June

201

528

0-FT

-2/G

T-14

Optim

izatio

n Te

chniq

ues i

n Fli

ght T

est/

Grou

nd Te

stOb

elisk

BCh

aired

by: W

. SCH

UMAN

, AF T

STA/

AEDC

and B

. MILL

S, AE

DC/

ATA

1400

hrs

AIAA-2

015-3

346

Optim

ized C

alcula

tion

of Fo

rces f

or

Fulls

cale

Aircr

aft S

tructu

re Fa

tigue

Te

sting

C. He

, Avia

tion I

ndus

try Co

rporat

ion of

Ch

ina (A

VIC),

Xi’an

, Chin

a

1430

hrs

AIAA-2

015-3

347

The d

esign

and t

est re

sult o

f pres

sure

dis

tortio

n com

pens

ation

devic

e in

Weigh

t and

Balan

ce Sy

stem

Y. Mi

nqian

g, C.

Yue,

Taiyu

an Ae

ro-Ins

trume

nts Co

mpan

y, Ltd

., Ta

iyuan

, Chin

a

1500

hrs

AIAA-2

015-3

348

Evalu

ation

of Lo

w-Co

st Au

topil

ots

for S

UAS O

pera

tions

C. Br

own,

J. Ja

cob,

Oklah

oma S

tate

Unive

rsity,

Still

water

, OK

1530

hrs

AIAA-2

015-3

349

Appli

catio

n of

a sm

all U

AV fl

eet f

or

demo

nstra

tion

of op

timize

d miss

ionM.

Kasp

rzyk,

P. Bib

ik, M

. Mali

nows

ki,

J. Po

lacze

k, K.

Wron

owsk

i, Wars

aw

Unive

rsity

of Te

chno

logy,

Warsa

w, Po

land

Thur

sday

, 25

June

201

528

1-GE

PC-1

Over

view

of N

ASA

Adva

nced

Air

Vehic

les P

rogr

amMe

tropo

litan

Ballr

oom

Chair

ed by

: B. E

SKER

and R

. DEL

ROSA

RIO, N

ASA G

lenn R

esea

rch Ce

nter

1400

hrs

Oral

Prese

ntatio

nAd

vanc

ed A

ir Ve

hicles

Pro

gram

Ov

ervie

wJ.

Drye

r, B. E

sker,

NAS

A Hea

dqua

rters,

Wa

shing

ton, D

C

1430

hrs

Oral

Prese

ntatio

nNA

SA’s

Adva

nced

Air

Trans

port

Tech

nolog

y Pro

ject

R. De

l Ros

ario,

NASA

Glen

n Res

earch

Ce

nter, C

levela

nd, O

H; S

. And

ers, N

ASA

Lang

ley Re

searc

h Cen

ter, H

ampto

n, VA

; N.

Mada

van,

NASA

Ames

Rese

arch C

enter

, Mo

ffett

Field,

CA

1500

hrs

Oral

Prese

ntatio

nCo

mmer

cial S

uper

sonic

Tech

nolog

y Pr

oject

Over

view

P. Co

en, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA;

K. Civ

inska

s, L.

Povin

elli,

NASA

Glen

n Res

earch

Cente

r, Clev

eland

, OH

1530

hrs

Oral

Prese

ntatio

nRe

volut

ionar

y Ver

tical

Lift

Tech

nolog

y Pro

ject

S. G

orton

, NAS

A Lan

gley R

esea

rch

Cente

r, Ham

pton,

VA; I

. Lóp

ez, N

ASA

Glenn

Rese

arch C

enter

, Clev

eland

, OH;

C.

Theo

dore,

NAS

A Ame

s Res

earch

Cente

r, Mo

ffett

Field,

CA

1600

hrs

Oral

Prese

ntatio

nAd

vanc

ed Co

mpos

ites P

rojec

t Ov

ervie

wR.

Youn

g, S.

Sme

ltzer,

NAS

A Lan

gley

Rese

arch C

enter

, Ham

pton,

VA

1630

hrs

Oral

Prese

ntatio

nNA

SA A

eron

autic

s Eva

luatio

n an

d Te

st Ca

pabil

ities P

rojec

tC.

Mouri

ng, N

ASA L

angle

y Res

earch

Ce

nter, H

ampto

n, VA

; R. C

olanto

nio, N

ASA

Glenn

Rese

arch C

enter

, Clev

eland

, OH

Thur

sday

, 25

June

201

528

2-LTA

-2Lig

hter

-than

-Air

Syste

ms &

Tech

nolog

ies II

Steub

enCh

aired

by: D

. HOR

KHEIM

ER, H

oney

well I

nterna

tiona

l, Inc

.14

00 hr

sAIA

A-201

5-335

0La

b-Sc

ale Ch

arac

teriza

tion

of a

Light

er-Th

an-A

ir Wi

nd En

ergy

Sy

stem

- Clos

ing th

e Loo

pJ.

Dees

e, T.

Muyim

bwa,

N. D

eodh

ar, C.

Ve

rmilli

on, P

. Tka

cik, U

nivers

ity of

Nort

h Ca

rolina

, Cha

rlotte

, Cha

rlotte

, NC

1430

hrs

AIAA-2

015-3

351

The 1

2M™

Teth

ered

Aer

osta

t Sy

stem:

Rap

id Ta

ctica

l Dep

loyme

nt

for S

urve

illanc

e Miss

ions

J. Kra

usma

n, D.

Mille

r, TCO

M, L.

P.,

Colum

bia, M

D

1500

hrs

AIAA-2

015-3

352

Desig

n an

d Flig

ht Te

sting

of an

Au

tono

mous

Airs

hipJ.

Santo

s, D.

Garc

ia, M

. Cun

ha, L

. Góe

s, Te

chno

logica

l Insti

tute o

f Aero

nauti

cs (IT

A), S

ão Jo

sé do

s Cam

pos,

Braz

il; R.

Pant,

India

n Ins

titute

of Te

chno

logy

Mumb

ai, M

umba

i, Ind

ia

1530

hrs

AIAA-2

015-3

353

Diap

hrag

m Te

sting

of Fa

bric

Comp

onen

ts &

Corre

lation

to

Analy

sisK.

Crome

r, S. P

eterse

n, TC

OM, L

.P.,

Colum

bia, M

D

Thur

sday

, 25

June

201

528

3-MA

O-10

Shap

e and

Topo

logy I

IMa

drid

Chair

ed by

: B. M

ESME

R, Un

iversi

ty of

Alaba

ma an

d V. K

ALIVA

RAPU

, Iow

a Stat

e Univ

ersity

1400

hrs

AIAA-2

015-3

354

Volum

etric

Shap

e Par

amete

risat

ion

for C

ombin

ed A

erod

ynam

ic Ge

ometr

y and

Topo

logy

Optim

isatio

nJ.

Hall,

D. Po

ole, T

. Ren

dall,

C. All

en,

Unive

rsity

of Br

istol,

Bris

tol, U

nited

Kin

gdom

1430

hrs

AIAA-2

015-3

355

A Di

screte

Adjo

int Fr

amew

ork

for U

nstea

dy A

erod

ynam

ic an

d Ae

roac

ousti

c Opt

imiza

tion

B. Zh

ou, T

. Albr

ing, N

. Gau

ger, T

echn

ical

Unive

rsity

of Ka

isersl

auter

n, Ka

isersl

auter

n, Ge

rman

y; T.

Econ

omon

, F. P

alacio

s, J.

Alons

o, St

anfor

d Univ

ersity

, Stan

ford,

CA

1500

hrs

AIAA-2

015-3

356

Towa

rds s

hape

optim

izatio

n of

stea

dy-st

ate fl

uid-st

ructu

re

inter

actio

n pr

oblem

s usin

g ver

tex

morp

hing

R. Na

jian A

sl, D

. Bau

mgärt

ner, K

. Ble

tzing

er, Te

chnic

al Un

iversi

ty of

Munic

h, Mu

nich,

Germ

any

1530

hrs

AIAA-2

015-3

357

Know

ledge

-bas

ed In

tegra

ted W

ing

Auto

matio

n an

d Opt

imiza

tion

for

Conc

eptu

al De

sign

R. Mu

njulur

y, P.

Berry

, T. M

elin,

K. Am

adori

, P. K

rus, L

inköp

ing U

nivers

ity,

Linkö

ping,

Swed

en

1600

hrs

AIAA-2

015-3

358

Conc

eptua

l opti

mal d

esign

of

envir

onme

ntally

frien

dly ai

rliners

: a

review

of av

ailab

le me

thodo

logies

an

d the

ir inte

grati

on in

to a c

onsis

tent

frame

work

for e

very

day u

seP. M

agalh

aes,

B. Ma

ttos,

Techn

ologic

al Ins

titute

of Ae

ronau

tics (I

TA), S

ão Jo

sé do

s Ca

mpos,

Braz

il

1630

hrs

AIAA-2

015-3

359

Robu

st an

d Reli

abilit

y-Ba

sed

Topo

logy O

ptim

izatio

n of

Wing

Bo

dies

D. Pa

padim

itriou

, C. P

apad

imitri

ou,

Unive

rsity

of Th

essa

ly, Vo

los, G

reece

114

Thur

sday

, 25

June

201

528

4-MA

O-11

Unce

rtaint

y IMa

nche

ster

Chair

ed by

: R. K

OLON

AY, A

ir Forc

e Res

earch

Labo

ratory

/RQV

C/W

PAFB

and P

. PIPE

RNI,

Bomb

ardier

Inc

1400

hrs

AIAA-2

015-3

360

High

-Fide

lity W

eight

Estim

ation

fo

r Airc

raft

Conc

eptu

al De

sign

Optim

izatio

nN.

Niga

m, S

. Ayy

alaso

maya

jula,

X.

Qi, P

. Che

n, Int

ellige

nt Au

tomati

on,

Inc.,

Rock

ville,

MD;

J. Al

onso

, Stan

ford

Unive

rsity,

Stan

ford,

CA

1430

hrs

AIAA-2

015-3

361

Surro

gate-

base

d Rob

ust S

hape

Op

timiza

tion

for V

ane C

luster

sI.

Arsen

yev,

F. Du

ddec

k, Te

chnic

al Un

iversi

ty of

Munic

h, Mu

nich,

Germ

any;

A. Fis

chers

worrin

g-Bun

k, MT

U Ae

ro En

gines

, Mu

nich,

Germ

any

Thur

sday

, 25

June

201

528

5-MS

T-12

Prop

ulsion

Syste

msTra

verti

neCh

aired

by: A

. ELM

ILIGU

I, NA

SA La

ngley

Rese

arch C

enter

1400

hrs

AIAA-2

015-3

362

One-

dimen

siona

l Mod

el of

a Clo

sed-

loop U

nder

water

Pro

pulsi

on

Syste

mJ.

Lu, C

hina S

hipbu

ilding

Indu

stry

Corpo

ration

Comp

any,

Ltd.,

Xi’an

, Chin

a

1430

hrs

AIAA-2

015-3

363

Indiv

idual

mode

l iden

tifica

tion

for

turb

ofan

engin

e bas

ed on

parti

cle

swar

m op

timiza

tion

J. Qi

an, F

. Liu,

Nan

jing U

nivers

ity of

Ae

ronau

tics a

nd As

trona

utics,

Nan

jing,

China

; X. Q

iu, Av

iation

Moto

r Con

trol

Syste

m Ins

titute,

Wux

i, Chin

a

1500

hrs

AIAA-2

015-3

364

Nume

rical

Study

of Si

milar

ity an

d Di

mens

ional

Meth

ods i

n Sc

aled

Turb

ine Va

ne co

oling

perfo

rman

ce

expe

rimen

tY.

Liu, M

. Jun

kui, G

. Dila

n, Na

njing

Un

iversi

ty of

Aeron

autic

s and

Astro

nauti

cs,

Nanji

ng, C

hina

Thur

sday

, 25

June

201

528

6-PD

L-13

Plasm

a Aer

odyn

amics

& Fl

ow Co

ntro

l VMi

roCh

aired

by: J

. POG

GIE,

USAF

AFRL

/RBA

C14

00 hr

sAIA

A-201

5-336

5Nu

meric

al Stu

dy of

Th

erma

l Pro

tectio

n Us

ing

Magn

etohy

drod

ynam

ic Flo

w Co

ntro

l in M

ars E

ntry

Fligh

tT.

Taka

hash

i, Y. S

himos

awa,

K. Ma

suda

, T.

Fujin

o, Un

iversi

ty of

Tsuku

ba, T

suku

ba,

Japa

n

1430

hrs

AIAA-2

015-3

366

Three

-dime

nsion

al Nu

meric

al Sim

ulatio

n of M

agne

tohyd

rody

nami

c Flo

w Co

ntrol

in Re

entry

Fligh

tK.

Masud

a, Y.

Shim

osawa

, Univ

ersity

of

Tsuku

ba, T

sukub

a, Jap

an; S

. Oga

wa, T

. Yo

shino

, Tosh

iba Co

rporat

ion, K

awasa

ki,

Japan

; T. F

ujino,

Unive

rsity o

f Tsuk

uba,

Tsuku

ba, J

apan

1500

hrs

AIAA-2

015-3

367

Mode

ling D

BD P

lasma

Actu

ator

s in

Integ

ral B

ound

ary L

ayer

Fo

rmula

tion

for A

pplic

ation

in

Pane

l Meth

ods

G. de

Oliv

eira,

R. Sa

ntos P

ereira

, D.

Ragn

i, M. K

otson

is, D

elft U

nivers

ity of

Te

chno

logy,

Delft,

The N

etherl

ands

1530

hrs

AIAA-2

015-3

368

Nume

rical

Inve

stiga

tion

of Se

vera

l Al

kali M

etal A

dditio

n Me

thod

s for

th

e For

ced E

levat

ion of

the S

tarti

ng

Altit

ude i

n th

e Elec

trody

nami

c Ae

robr

aking

Dec

leara

tion

H. Ka

tsuray

ama,

Yama

guch

i Univ

ersity

, Ub

e, Ja

pan

1600

hrs

AIAA-2

015-3

369

Parti

cle in

Cell (

PIC)

simu

lation

s of

plasm

a-ele

ctrod

e int

erac

tions

for

Reen

try B

lacko

ut A

llevia

tion

S. Kr

ishna

moort

hy, S

. Clos

e, St

anfor

d Un

iversi

ty, S

tanfor

d, CA

Thur

sday

, 25

June

201

528

7-RL

A-3

1400

- 15

30 h

rsRi

sing L

eade

rs in

Aero

spac

e Pan

el Di

scussi

on: T

rans

itionin

g to L

eade

rship

Emer

ald

This

pane

l will

addre

ss the

chan

ges t

hat a

ccomp

any m

oving

into

a man

agem

ent r

ole, t

he di

fferen

t skil

l sets

that

will n

eed t

o be a

cquir

ed, a

nd th

e cha

nges

you c

an ex

pect

in yo

ur da

ily w

ork ro

utine

.Mo

derat

or: B

en M

archio

nna,

Syste

ms En

ginee

r, Loc

khee

d Mart

in Sk

unk W

orks

P

aneli

sts:

Russ

Alth

ofCh

ief En

ginee

rRa

ytheo

n Miss

ile S

ystem

s

Doug

las St

anley

Presid

ent a

nd Ex

ecuti

ve D

irecto

rNa

tiona

l Insti

tute o

f Aero

spac

e

Fred

erick

Wiel

and

Direc

tor, A

ir Traf

fic M

anag

emen

tInt

ellige

nt Au

tomati

on S

ystem

s, Inc

.

115

Thur

sday

, 25

June

201

528

8-TP

-13

DSMC

Rose

ttaCh

aired

by: D

. HAS

H, N

ASA -

ARC

1400

hrs

AIAA-2

015-3

370

DSMC

Stud

y of C

arbo

n Fibe

r Oxid

ation

in

Ablat

ive Th

ermal

Prote

ction

Syste

msA.

Borne

r, NAS

A Ame

s Rese

arch C

enter

, Mo

ffett F

ield, C

A; F. P

anera

i, Univ

ersity

of

Kentu

cky, L

exing

ton, L

exing

ton, K

Y; N.

Ma

nsour,

NAS

A Ame

s Rese

arch C

enter

, Mo

ffett F

ield, C

A

1430

hrs

AIAA-2

015-3

371

Sens

itivity

Ana

lysis

of D

SMC

Para

meter

s for

Ioniz

ing, R

adiat

ing

Hype

rsonic

Flow

sK.

Higdo

n, D.

Gold

stein,

P. Va

rghes

e, Un

iversi

ty of

Texa

s, Au

stin,

Austi

n, TX

1500

hrs

AIAA-2

015-3

372

DSMC

Inve

stiga

tion

of

None

quilib

rium

Effe

cts in

a H2

-O2

Unstr

etche

d Diff

usion

Flam

eI.

Borge

s Seb

astia

o, A.

Alexe

enko

, Purd

ue

Unive

rsity,

Wes

t Lafa

yette

, IN

1530

hrs

AIAA-2

015-3

373

Calib

ratio

n of

DSM

C par

amete

rs fo

r tra

nspo

rt pr

oces

ses i

n ion

ized

air m

ixtur

esK.

Swam

inatha

n Gop

alan,

K. St

epha

ni,

Unive

rsity

of Illi

nois,

Urba

na-Ch

ampa

ign,

Urba

na, I

L

Thur

sday

, 25

June

201

528

9-NW

-9

1530

- 16

00 h

rsNe

twor

king C

offe

e Bre

akMe

eting

Roo

m Fo

yers

Thur

sday

, 25

June

201

529

0-LE

C-6

1730

- 18

30 h

rsWr

ight B

roth

ers L

ectu

resh

ip in

Aero

naut

icsCh

antill

y Ball

room

Wes

t

Deve

lopme

nt an

d Test

ing of

the X

-47B

Pablo

Gon

zalez

, II

UCAS

-D Pro

gram

Mana

ger

North

rop G

rumma

n Aero

spac

e Sys

tems

Frida

y

Frida

y, 26

June

201

529

1-SB

-5

0730

- 08

00 h

rsSp

eake

rs’ B

riefin

gSe

ssion

Roo

ms

Frida

y, 26

June

201

529

2-PL

NRY-5

08

00 -

0900

hrs

Plena

ry K

eyno

teCh

antill

y Ball

room

Wes

t

The G

650 D

esign

, Dev

elopm

ent,

and T

estKu

rt Er

bach

erVic

e Pres

ident,

G65

0 Air

craft

Progra

mGu

lfstre

am Ae

rospa

ce Co

rporat

ion

Frida

y, 26

June

201

529

3-AC

D-8

Aero

naut

ic Di

scipli

ne Co

nside

ratio

ns in

Airc

raft

Desig

nMi

roCh

aired

by: H

. JIM

ENEZ

, Geo

rgia I

nstitu

te of

Tech

nolog

y09

00 hr

sAIA

A-201

5-337

4Pr

edict

ion of

Wing

Stru

ctura

l Mas

s fo

r Tra

nspo

rt Ca

tegor

y Aicr

aft

Conc

eptu

al De

sign

T. Ta

kaha

shi, T

. Lem

onds

, Ariz

ona S

tate

Unive

rsity,

Temp

e, AZ

0930

hrs

AIAA-2

015-3

375

Effe

ctive

L/D:

A Th

eore

tical

Appr

oach

to th

e Mea

sure

ment

of

Aer

o-Str

uctu

ral E

fficie

ncy i

n Ai

rcraf

t Des

ignM.

Guy

nn, N

ASA L

angle

y Res

earch

Cente

r, Ha

mpton

, VA

1000

hrs

AIAA-2

015-3

376

Revis

iting B

usem

ann:

The D

esign

Im

plica

tions

of In

cons

isten

cies

Foun

d With

in Sim

ple Sw

eep T

heor

yT.

Taka

hash

i, S. K

amat,

Arizo

na S

tate

Unive

rsity,

Temp

e, AZ

1030

hrs

AIAA-2

015-3

377

A To

tal F

light

Enve

lope A

ppro

ach

to Co

ncep

tual

Desig

n Sta

bility

&

Cont

rol

M. S

wann

, T. T

akah

ashi,

Arizo

na S

tate

Unive

rsity,

Temp

e, AZ

1100

hrs

AIAA-2

015-3

378

Feas

ibility

Stud

ies on

a Hi

gh-A

ltitud

e Ca

ptive

Ligh

ter-Th

an-A

ir Plat

form

Syste

mK.

Chiba

, S. S

atori,

R. Hir

amoto

, S. K

ase, R

. Mi

tsuha

shi, H

okka

ido Un

iversit

y of S

cience

, Sa

pporo

, Jap

an; J

. Sasa

ki, Ho

kkaid

o Ae

rospa

ce Sc

ience

and T

echno

logy I

ncuba

tion

Cente

r, Sap

poro,

Japa

n; et

al.

116

Frida

y, 26

June

201

529

4-AM

T-14/

GT-1

5Ae

rody

nami

c Mea

sure

ment

Syste

ms: C

alibr

ation

and M

onito

ring

Topa

zCh

aired

by: R

. RHE

W, N

ASA-L

angle

y Res

earch

Cente

r and

G. J

ONES

, NAS

A-Lan

gley R

esea

rch Ce

nter

0900

hrs

Oral

Prese

ntatio

nMe

asur

emen

t Sys

tem Ca

libra

tion

Fund

amen

tals

R. Rh

ew, P

. Park

er, G

. Jon

es, N

ASA

Lang

ley Re

searc

h Cen

ter, H

ampto

n, VA

0930

hrs

AIAA-2

015-3

379

Impr

oved

Reg

ressi

on A

nalys

is of

Te

mper

atur

e-De

pend

ent S

train-

Gage

Bala

nce C

alibr

ation

Dat

aN.

Ulbr

ich, J

acob

s, Mo

ffett

Field,

CA

1000

hrs

AIAA-2

015-3

380

Statis

tical

Proc

ess Co

ntrol

Imple

mente

d for

Long

Term

Stud

y of

Wind

Tunn

el Ba

lance

Calib

ratio

nsR.

Callah

an, D

. Lan

dman

, Old

Domi

nion

Unive

rsity,

Norfo

lk, VA

; S. C

ommo

, K. L

ynn,

NASA

Lang

ley Re

search

Cente

r, Ham

pton,

VA

1030

hrs

AIAA-2

015-3

381

Analy

sis of

Five

-Hole

Pro

be

Calib

ratio

n Pa

rame

ters

S. Ka

rahan

, A. K

utay,

Midd

le Ea

st Te

chnic

al Un

iversi

ty, An

kara,

Turke

y

1100

hrs

AIAA-2

015-3

382

The U

se of

Abs

olute-

Value

Term

s in

Regr

essio

n Mo

delin

g of M

ulti-P

iece

Force

Bala

nces

(Inv

ited)

M. Ka

mmey

er, Th

e Boe

ing Co

mpan

y, St

. Lo

uis, M

O; N

. Ulbr

ich, J

acob

s, Mo

ffett

Field,

CA

Frida

y, 26

June

201

529

5-AP

A-34

Icing

or R

ough

ness

Effe

cts on

Vehic

le Ae

rody

nami

csSte

mmon

s CCh

aired

by: G

. WOO

, Gen

eral E

lectric

Glob

al Re

searc

h and

D. O

’BRIE

N, U

S Arm

y RDE

COM

0900

hrs

AIAA-2

015-3

383

Data

-Driv

en Lo

w-Di

mens

ional

Mode

ling a

nd U

ncer

taint

y Qu

antifi

catio

n fo

r Airf

oil Ic

ingA.

DeGe

nnaro

, C. R

owley

, L. M

artine

lli,

Princ

eton U

nivers

ity, P

rince

ton, N

J

0930

hrs

AIAA-2

015-3

384

Aero

dyna

mic E

ffects

of R

ough

ness

on W

ind Tu

rbine

Blad

e Sec

tions

L. Jo

seph

, J. F

enou

il, A.

Borgo

ltz, W

. De

venp

ort, V

irgini

a Poly

techn

ic Ins

titute

and S

tate U

nivers

ity, B

lacks

burg,

VA

1000

hrs

AIAA-2

015-3

385

The C

hara

cteris

tics o

f SLD

icing

ac

cretio

ns an

d aero

dyna

mic e

ffects

on

high-l

ift co

nfigu

ratio

nsC.

Zhan

g, F. W

ang,

W. Ko

ng, H

. Liu,

Shan

ghai

Jiao T

ong U

nivers

ity, Sh

angh

ai, Ch

ina

Frida

y, 26

June

201

529

6-AP

A-35

Aero

dyna

mic D

esign

Meth

odolo

gies I

IICa

rpen

ter B

allro

omCh

aired

by: C

. ROS

EMA,

US Ar

my AM

RDEC

0900

hrs

AIAA-2

015-3

386

Expe

rimen

tal V

alida

tion

of a

Morp

hed W

ing G

eome

try U

sing

Small

Wind

Tunn

el Te

sting

A. Ko

reans

chi, S

. Oliv

iu, R.

Bote

z, Un

iversi

ty of

Québ

ec, M

ontré

al, Ca

nada

0930

hrs

AIAA-2

015-3

387

Stabil

ity D

eriva

tive C

ompu

tation

of

Taille

ss Air

craft

using

Varia

ble-Fi

delity

Ae

rody

nami

c Ana

lysis a

nd W

ind-

Tunn

el Ex

perim

ents

J. Pa

rk, C.

Oche

ltree,

J. Ch

oi, S.

Choi,

P. Ra

j, A.

Fried

man,

Virgin

ia Po

lytech

nic In

stitute

and

State

Unive

rsity,

Blacks

burg,

VA

1000

hrs

AIAA-2

015-3

388

Aero

dyna

mic p

erfo

rman

ce st

udy

of h

igh pr

essu

re zo

ne ca

ptur

e wing

co

nfigu

ratio

nsK.

Cui, G

. Li, Y

. Xiao

, Chin

ese A

cade

my of

Sc

ience

s, Be

ijing,

China

Frida

y, 26

June

201

529

7-AP

A-37

Prop

eller

/Rot

orcra

ft/Wi

nd Tu

rbine

Aer

odyn

amics

III

Stemm

ons B

Chair

ed by

: K. M

ASSE

Y, DA

RPA/

TTO

and J

. MUR

RAY,

Sand

ia Na

tiona

l Lab

orator

ies09

00 hr

sAIA

A-201

5-338

9Se

nsitiv

ity of

Wind

Turb

ine A

irfoil

Se

ction

s to G

eome

try Va

riatio

ns

Inhe

rent

in M

odula

r Blad

esK.

Brow

n, N.

Moli

naro,

T. M

eyers

, A.

Borgo

ltz, W

. Dev

enpo

rt, V

irgini

a Po

lytec

hnic

Institu

te an

d Stat

e Univ

ersity

, Bla

cksb

urg, V

A; J.

Lued

ke, G

enera

l Elec

tric

Comp

any,

Gree

nville

, SC;

et al.

0930

hrs

AIAA-2

015-3

390

Confi

gura

tion a

nd N

umeri

cal

Invest

igatio

n of t

he Ad

aptiv

e Cam

ber

Airfoi

l as P

assiv

e Loa

d Alle

viatio

n Me

chan

ism fo

r Wind

Turb

ines

D. Ma

rten,

Techn

ical U

nivers

ity of

Berlin

, Be

rlin, G

erman

y; H.

Spieg

elberg

, Tech

nical

Unive

rsity o

f Darm

stadt,

Darm

stadt,

Germ

any;

G. Pe

chliva

noglo

u, C.

Naye

ri, C.

Pasch

ereit,

Techn

ical U

nivers

ity of

Berlin

, Berl

in, Ge

rman

y; C.

Trope

a, Tec

hnica

l Univ

ersity

of Da

rmsta

dt,

Darm

stadt,

Germ

any

1000

hrs

AIAA-2

015-3

391

Exten

sion

of a

Para

bolic

Meth

od

with

out P

ressu

re A

ppro

ximat

ions

for W

ind Tu

rbine

s in

ABL F

lows

A. Mi

ttal, L

. Tay

lor, K

. Sree

nivas

, W.

Brile

y, D.

Nich

ols, U

nivers

ity of

Tenn

esse

e, Ch

attan

ooga

, Cha

ttano

oga,

TN

1030

hrs

AIAA-2

015-3

392

Expe

rimen

tal a

nd N

umer

ical

Inve

stiga

tions

of a

Small

Res

earch

Wi

nd Tu

rbine

S. Ve

y, D.

Mart

en, G

. Pec

hliva

noglo

u, C.

Naye

ri, C.

Pasch

ereit,

Tech

nical

Unive

rsity

of Be

rlin, B

erlin,

Germ

any

1100

hrs

AIAA-2

015-3

393

Optim

izatio

n of

Wind

Turb

ine

Airfo

ils Su

bject

to P

artic

le Er

osion

G. Fi

ore, M

. Seli

g, Un

iversi

ty of

Illino

is,

Urba

na-Ch

ampa

ign, U

rbana

, IL

117

Frida

y, 26

June

201

529

8-AT

IO-2

7AT

M VI

I - W

eath

er Im

pact

Moro

ccoCh

aired

by: Y

. JUN

G, N

ASA A

mes R

esea

rch Ce

nter

0900

hrs

AIAA-2

015-3

394

Dyna

mic A

rriva

l Rou

tes: A

Tra

jecto

ry-B

ased

Wea

ther

Av

oidan

ce Sy

stem

for M

ergin

g Ar

rivals

and M

eterin

gC.

Gong

, D. M

cnall

y, NA

SA Am

es Re

searc

h Ce

nter, M

offett

Field

, CA

0930

hrs

AIAA-2

015-3

395

Initia

l Ana

lysis

of an

d Pre

dictiv

e Mo

del D

evelo

pmen

t for

Wea

ther

Re

rout

e Adv

isory

Use

H. Ar

neso

n, NA

SA Am

es Re

searc

h Cen

ter,

Moffe

tt Fie

ld, CA

1000

hrs

AIAA-2

015-3

396

Bene

fits A

nalys

is of

Gro

und-

Sour

ced C

onve

ctive

Wea

ther

Al

ertin

g in

the C

ockp

itS.

Camp

bell,

M. M

cPart

land,

M. Is

hutki

na,

Linco

ln La

borat

ory, M

assa

chus

etts I

nstitu

te of

Tech

nolog

y, Le

xingto

n, MA

1030

hrs

AIAA-2

015-3

397

Dyna

mic W

ake V

ortex

Sepa

ratio

n Co

mbini

ng w

ith A

MAN/

DMAN

Co

ncep

tN.

Mata

yosh

i, E. Y

oshik

awa,

Japa

n Ae

rospa

ce Ex

plorat

ion Ag

ency

(JAX

A),

Mitak

a, Ja

pan

1100

hrs

AIAA-2

015-3

398

Wind

Info

rmat

ion U

plink

to A

ircra

ft Pe

rform

ing In

terva

l Man

agem

ent

Oper

ation

sN.

Ahma

d, B.

Barm

ore, K

. Swi

ering

a, NA

SA

Lang

ley Re

search

Cente

r, Ham

pton,

VA

1130

hrs

AIAA-2

015-3

399

Wind

Mea

sure

ment

s with

grou

nd-

base

d fibe

r-bas

ed w

ind D

opple

r LID

AR sy

stems

for a

viatio

n we

athe

r ap

plica

tions

L. Th

obois

, Leo

sphe

re, O

rsay,

Franc

e

Frida

y, 26

June

201

529

9-AT

IO-2

8Fu

ture

Conc

epts

Wyeth

Chair

ed by

: K. M

ARAIS

, Purd

ue U

nivers

ity09

00 hr

sAIA

A-201

5-340

0Ac

hievin

g TAS

AR O

pera

tiona

l Re

adine

ssD.

Wing

, NAS

A Lan

gley R

esea

rch Ce

nter,

Hamp

ton, V

A

0930

hrs

AIAA-2

015-3

401

A Pr

elimi

nary

Evalu

ation

of

Supe

rsonic

Tran

spor

t Cat

egor

y Ve

hicle

Oper

ation

s in

the N

ation

al Ai

rspac

e Sys

temM.

Und

erwoo

d, M.

Gum

insky

, NAS

A La

ngley

Rese

arch C

enter

, Ham

pton,

VA

1000

hrs

AIAA-2

015-3

402

Impr

oving

Situ

ation

Awa

rene

ss wi

th

a Tra

ffic M

anag

emen

t Por

tal

A. St

aley,

C. Bo

lczak

, MITR

E Corp

oratio

n, Mc

Lean

, VA

1030

hrs

AIAA-2

015-3

403

Dyna

mic A

irspa

ce Co

nfigu

ratio

n in

SESA

R: bu

ilding

a sm

ooth

and

dyna

mic o

penin

g sch

eme t

hrou

gh

airsp

ace b

uildin

g bloc

ks as

sessm

ent

T. Du

bot,

S. Au

bry, J

. Bed

ouet,

ONE

RA,

Toulo

use,

Franc

e

1100

hrs

AIAA-2

015-3

404

The I

mpac

t of M

itigati

on M

easu

res fo

r Sy

stem

Capa

city C

onstr

aints

on th

e Fu

ture A

ir Tra

nspo

rtatio

n Sys

temN.

Dziku

s, Ge

rman

Aeros

pace

Cente

r (DL

R),

Hamb

urg, G

erman

y; S.

Barto

sch, R

WTH

Aache

n Univ

ersity,

Aache

n, Ge

rman

y; M.

Sc

haefe

r, Fed

eral M

inistry

of Tra

nsport

and

Digita

l Infra

struct

ure, B

onn,

Germ

any

Frida

y, 26

June

201

530

0-AT

IO-2

9UA

S Int

egra

tion

& Op

erat

ions I

IMi

ngCh

aired

by: D

. DEL

AURE

NTIS,

Purdu

e Univ

ersity

0900

hrs

AIAA-2

015-3

405

UAS D

eman

d Gen

erat

ion U

sing

Subje

ct Ma

tter E

xper

t Int

ervie

ws

and S

ocio-

econ

omic

Analy

sisS.

Ayya

lasom

ayaju

la, R.

Sha

rma,

F. W

ielan

d, Int

ellige

nt Au

tomati

on, I

nc.,

Rock

ville,

MD;

A. Tr

ani, N

. Hinz

e, T.

Spen

cer, V

irgini

a Poly

techn

ic Ins

titute

and

State

Univ

ersity

, Blac

ksbu

rg, VA

0930

hrs

AIAA-2

015-3

406

Inve

stiga

tion

of Si

mulat

ed U

AS

Safe

ty In

ciden

ts Us

ing U

AS Sa

fety

An

alysis

Mod

el (U

SAM)

A. Ty

agi, F

. Wiel

and,

Intell

igent

Autom

ation

, Inc

., Ro

ckvil

le, M

D; S

. To

ussa

int, C

ohere

nt Te

chnic

al Se

rvice

s, Inc

., Le

xingto

n Park

, MD;

J. Lu

xhoj,

LCR,

LLC, S

omers

et, N

J

1000

hrs

AIAA-2

015-3

407

RPAS

- AT

M In

tegra

tion

Demo

nstra

tion

- Rea

l-Tim

e Sim

ulatio

n Re

sults

E. Fil

ippon

e, Ita

lian A

erosp

ace R

esea

rch

Cente

r (CIR

A), C

apua

, Ital

y

118

Frida

y, 26

June

201

530

1-CF

D-31

Visua

lizat

ion fo

r CFD

203

0Gr

and B

allro

om A

Chair

ed by

: S. I

MLAY

, Tec

plot,

Inc09

00 hr

sAIA

A-201

5-340

8In

dustr

ial P

ersp

ectiv

es on

Geo

metry

Han

dling

for A

erod

ynam

icsN.

Taylo

r, MBD

A, Br

istol,

Unit

ed Ki

ngdo

m

1000

hrs

AIAA-2

015-3

409

The P

ath to

and S

tate o

f Geo

metry

an

d Mesh

ing in

2030

: Pan

el Su

mmar

yJ.

Chaw

ner, P

ointw

ise, In

c., Fo

rt Wort

h, TX

; J.

Dann

enho

ffer, S

yracus

e Univ

ersity,

Syrac

use,

NY; S

. Dey,

Nav

al Re

search

Labo

ratory

, Wa

shing

ton, D

C; W.

Jone

s, NA

SA La

ngley

Re

search

Cente

r, Ham

pton,

VA; J

. Slot

nick,

The B

oeing

Comp

any,

Hunti

ngton

Beach

, CA;

N. Ta

ylor, M

BDA,

Bristo

l, Unit

ed Ki

ngdo

m

1030

hrs

Pane

lPa

nel: T

he P

ath

to CF

D Vis

ualiz

ation

in 2

030

Mode

rato

r: Sc

ott I

mlay

, Tec

plot,

Inc

S. Im

lay, T

ecplo

t, Inc

., Sn

ohom

ish, W

A; E.

Duqu

e, Int

ellige

nt Lig

ht, Pr

esco

tt, AZ

; K.

Colbu

rn, Co

mputa

tion E

ngine

ering

Inter

natio

nal, I

nc.,

Hous

ton, T

X; G

. Che

n, Un

iversi

ty of

Hous

ton, H

ousto

n, TX

Frida

y, 26

June

201

530

2-CF

D-32

Post-

Proc

essin

g and

Mod

el Re

ducti

onGr

and B

allro

om B

Chair

ed by

: S. S

PEER

, Nort

hrop G

rumma

n Corp

oratio

n09

00 hr

sAIA

A-201

5-341

0EP

IC - A

n Ex

tract

Plug-

In

Comp

onen

ts To

olkit

for I

n-Sit

u Da

ta

Extra

cts A

rchite

cture

E. Du

que,

`. Hie

pler, I

ntellig

ent L

ight,

Ruthe

rford,

NJ;

R. Ha

imes

, Mas

sach

usett

s Ins

titute

of Te

chno

logy,

Camb

ridge

, MA;

C. St

one,

Comp

utatio

nal S

cienc

e and

En

ginee

ring,

LLC, C

hicag

o, IL;

S. G

orrell

, M.

Jone

s, Br

igham

Youn

g Univ

ersity

, Pro

vo, U

T; et

al.

0930

hrs

AIAA-2

015-3

411

Dyna

mic M

ode D

ecom

posit

ion

of B

ackw

ard F

acing

Step

Flow

Sim

ulatio

n Da

taT.

Horch

ler, K

. Man

i, K. H

anne

mann

, Ge

rman

Aeros

pace

Cente

r (DL

R),

Göttin

gen,

Germ

any

1000

hrs

AIAA-2

015-3

412

Statis

tical

Analy

sis an

d Mod

el Re

ducti

on of

Surfa

ce P

ressu

re

for I

nter

actio

n of

a Str

eamw

ise-

Orien

ted Vo

rtex

with

a Wi

ngA.

Moha

n, L.

Agos

tini, D

. Gait

onde

, Oh

io St

ate U

nivers

ity, C

olumb

us, O

H; D

. Ga

rman

n, Air

Force

Rese

arch L

abora

tory,

Wrig

ht-Pa

tterso

n AFB

, OH

Frida

y, 26

June

201

530

3-CF

D-33

Inter

discip

linar

y CFD

IIPlu

m Bl

osso

m A

Chair

ed by

: P. S

LABO

CH an

d D. G

ONZA

LEZ,

Nava

l Surf

ace W

arfare

Cente

r09

00 hr

sAIA

A-201

5-341

3Co

mput

ation

al Stu

dy of

Acti

ve Fl

ow

Cont

rol o

f a Fl

ow-Ex

cited

Helm

holtz

Re

sona

tor

J. Bu

ehn,

P. Sla

boch

, Sain

t Mart

in’s

Unive

rsity,

Lace

y, WA

0930

hrs

AIAA-2

015-3

414

Aero

elasti

c Res

pons

e of R

ocke

t No

zzles

Sube

cted t

o Com

bined

Th

rust

and S

ide Lo

ads

X. Zh

ao, A

labam

a A&M

Univ

ersity

, Hu

ntsvil

le, AL

; S. Z

hang

, ESI

Grou

p, Hu

ntsvil

le, AL

1000

hrs

AIAA-2

015-3

415

Finite

-Time

Lyap

unov

Expo

nent

An

alysis

of In

termi

ttent

Aco

ustic

Ev

ents

in a R

ound

Jet

D. G

onza

lez, N

aval

Surfa

ce W

arfare

Ce

nter, I

ndian

Hea

d, MD

; D. G

aiton

de,

Ohio

State

Univ

ersity

, Colu

mbus

, OH;

M.

Lewi

s, Sc

ience

and T

echn

ology

Policy

Ins

titute,

Was

hingto

n, DC

1030

hrs

AIAA-2

015-3

416

Nume

rical

Simula

tion

of th

e In

terac

tion

betw

een

Rim

Seal

and

Main

Annu

lus Fl

ow in

a Fo

ur St

age

Low-

Pres

sure

Axia

l Tur

bine

Z. We

i tao,

China

Gas

Turbi

ne

Estab

lishme

nt, Ch

engd

u, Ch

ina

1100

hrs

AIAA-2

015-3

417

Calcu

lation

of A

irfoil

Ant

i-icin

g Hea

t Lo

ad in

SLD

Cond

itions

Z. Wa

ng, N

anjin

g Univ

ersity

of Ae

ronau

tics

and A

stron

autic

s, Na

njing

, Chin

a

119

Frida

y, 26

June

201

530

4-CF

D-34

Multip

hase

and N

oneq

uilibr

ium Fl

ows

Cora

lCh

aired

by: C

. TSA

I, Lo

ckhe

ed M

artin

Spac

e Sys

tems a

nd R.

AGAR

WAL,

Wash

ington

Univ

ersity

in S

t Lou

is09

00 hr

sAIA

A-201

5-341

8Nu

meric

al sim

ulatio

n of

a scr

amjet

iso

lator

with

ther

mody

nami

c no

nequ

ilibriu

mR.

Fiéve

t, H.

Koo,

V. Ra

man,

Unive

rsity

of Mi

chiga

n, An

n Arbo

r, Ann

Arbo

r, MI

0930

hrs

AIAA-2

015-3

419

A Mu

ltipha

se an

d Mult

iphys

ics CF

D Te

chniq

ue fo

r Fue

l Spu

rt Pr

edict

ion

with

Cavit

ation

and F

luid-

Struc

ture

In

terac

tion

H. Ya

ng, C

FD Re

searc

h Corp

oratio

n, Hu

ntsvil

le, AL

1000

hrs

AIAA-2

015-3

420

Appli

catio

n of a

Max

imum

-Entro

py-

Based

14-M

omen

t Clos

ure f

or M

ulti-

Dime

nsion

al No

n-Equ

ilibriu

m Flo

wsB.

Tens

uda,

Unive

rsity

of To

ronto,

To

ronto,

Cana

da; J

. McD

onald

, Univ

ersity

of

Ottaw

a, Ot

tawa,

Cana

da; C

. Grot

h, Un

iversi

ty of

Toron

to, To

ronto,

Cana

da

1030

hrs

AIAA-2

015-3

421

An A

LE/F

E for

mulat

ion fo

r high

pr

ecisi

on in

terfa

ce tr

ackin

g in

sepa

rated

mult

iphas

e flow

sA.

Hay,

S. Et

ienne

, D. P

elleti

er, Éc

ole

Polyt

echn

ique d

e Mon

tréal,

Mon

tréal,

Ca

nada

1100

hrs

AIAA-2

015-3

422

Simula

tion

of th

e Sep

arat

ed

flow

over

a Wa

ll-Mo

unted

Hum

p us

ing Fi

nite-

Volum

e Bas

ed La

ttice

Bo

ltzma

nn M

ethod

B. Ya

giz, G

. Guz

el, I.

Koc,

ASEL

SAN,

Inc.,

An

kara,

Turke

y

Frida

y, 26

June

201

530

5-CF

D-35

Over

set a

nd Ca

rtesia

n Gr

id Me

thod

sPlu

m Bl

osso

m B

Chair

ed by

: N. F

OSTE

R, Ap

plied

Rese

arch L

abora

tory -

Penn

Stat

e and

M. G

HORE

YSHI

, Unit

ed S

tates

Air F

orce A

cade

my09

00 hr

sAIA

A-201

5-342

3Th

ree-

Dime

nsion

al Dy

nami

c Ov

erse

t Meth

od fo

r Sta

bilize

d Fin

ite El

emen

tsC.

Liu, J

. New

man,

W. An

derso

n, Un

iversi

ty of

Tenn

essse

, Cha

ttano

oga,

Chatt

anoo

ga, T

N

0930

hrs

AIAA-2

015-3

424

Accu

racy

of H

igh-O

rder

CFD

and

Over

set I

nter

polat

ion in

Finit

e Vo

lume/

Diffe

renc

e Cod

esN.

Foste

r, Pen

nsylv

ania

State

Univ

ersity

, St

ate Co

llege

, PA

1000

hrs

AIAA-2

015-3

425

Adva

nces

in D

istan

ce-B

ased

Hole

Cu

ts on

Ove

rset G

rids

W. Ch

an, S

. Pan

dya,

NASA

Ames

Rese

arch

Cente

r, Moff

ett Fi

eld, C

A

1030

hrs

AIAA-2

015-3

426

Simula

tion

Valid

ation

of St

atic

and

Force

d Mot

ion Fl

ow P

hysic

s of a

Ca

nard

Confi

gure

d Tra

nsCr

uiser

M. G

horey

shi, R

. Kork

is-Kan

aan,

A. Jir

asek

, A. L

oftho

use,

R. Cu

mming

s, U.

S.

Air Fo

rce Ac

adem

y, Co

lorad

o Spri

ngs,

CO

1100

hrs

AIAA-2

015-3

427

Shar

p res

olutio

n of

comp

lex

movin

g geo

metri

es u

sing a

mult

i-cu

t-cell

visco

us fl

ow so

lver

L. Sc

hneid

ers, C

. Gue

nther,

J. G

rimme

n, M.

Mein

ke, W

. Sch

roede

r, RW

TH Aa

chen

Un

iversi

ty, Aa

chen

, Germ

any

1130

hrs

AIAA-2

015-3

428

Integ

ratin

g the

Stan

ford

Univ

ersit

y Un

struc

ture

d Cod

e (SU

2) W

ith

Over

set G

rids

A. Ka

noria

, Ind

ian In

stitut

e of T

echn

ology

Ga

ndhin

agar,

Gan

dhina

gar, I

ndia;

D.

Chan

dar, I

nstitu

te of

High P

erform

ance

Co

mputi

ng, S

ingap

ore, S

ingap

ore

1200

hrs

AIAA-2

015-3

429

A Co

mpar

ative

Stud

y of F

low

arou

nd a

Circu

lar Cy

linde

r usin

g La

ttice

Bolt

zman

n Me

thod

D. H

aman

e, O.

Gue

rri, Re

newa

ble En

ergy

Deve

lopme

nt Ce

nter A

lgeria

, Bou

zarea

h, Alg

eria;

S. La

rbi, P

olytec

hnica

l Sch

ool o

f Alg

iers,

Elhara

che,

Algeri

a

Frida

y, 26

June

201

530

6-CF

D-36

LES,

DNS,

and H

ybrid

RAN

S-LE

S IV

Emer

aldCh

aired

by: J

. POG

GIE,

USAF

AFRL

/RBA

C and

B. T

HORN

BER,

The U

nivers

ity of

Syd

ney

0900

hrs

AIAA-2

015-3

430

Impa

ct of

Comp

utat

ional

Doma

in Siz

e in

Simula

tions

of

Homo

gene

ous D

ecay

ing Tu

rbule

nce

and M

ixing

Laye

rsB.

Thorn

ber, U

nivers

ity of

Syd

ney,

Sydn

ey,

Austr

alia

0930

hrs

AIAA-2

015-3

431

Dire

ct Nu

meric

al Sim

ulatio

n of

Tu

rbule

nt Fl

ow A

roun

d a Su

rface

Mo

unted

Cube

A. Cu

rley,

M. U

ddin,

B. P

eters,

Univ

ersity

of

North

Carol

ina, C

harlo

tte, C

harlo

tte, N

C

1000

hrs

AIAA-2

015-3

432

Supe

rsonic

Corn

er Fl

ow P

redic

tions

us

ing th

e Qua

drat

ic Co

nstit

utive

Re

lation

T. Le

ger, J

. Pog

gie, A

ir Forc

e Res

earch

La

borat

ory, W

right-

Patte

rson A

FB, O

H

1030

hrs

AIAA-2

015-3

433

Asses

smen

t of n

ovel

DES a

ppro

ach

with

enha

nced

SGS m

odell

ing fo

r pr

edict

ion of

sepa

rated

flow

over

a de

lta w

ingM.

Fuchs

, Tech

nical

Unive

rsity o

f Berl

in, Be

rlin,

Germ

any;

C. Mo

ckett,

CFD S

oftwa

re Gm

bH,

Berlin

, Germ

any;

J. Se

sterhe

nn, F.

Thiele

, Tec

hnica

l Univ

ersity

of Be

rlin, B

erlin,

Germ

any

Frida

y, 26

June

201

530

7-MA

O-12

Shap

e and

Topo

logy I

IIMa

drid

Chair

ed by

: B. R

OTH,

Wall

a Wall

a Univ

and S

. CHO

I, Vir

ginia

Polyt

echn

ic Ins

titute

and S

tate U

nivers

ity09

00 hr

sAIA

A-201

5-343

4Ad

joint

-Enha

nced

Mult

i-Lev

el Op

timiza

tion:

Inve

stiga

tion

of

Algo

rithm

Par

amete

r Sett

ings

Y. Te

sfahu

negn

, S. K

oziel

, Rey

kjavik

Un

iversi

ty, Re

ykjav

ik, Ic

eland

; L. L

eifsso

n, Iow

a Stat

e Univ

ersity

, Ame

s, IA

0930

hrs

AIAA-2

015-3

435

Discr

ete A

djoint

Des

ign

Optim

izatio

n Ap

proa

ch fo

r In

creas

ing Tr

anso

nic B

uffe

t Ons

et An

gle-o

f-Atta

ckJ.

Thom

as, E

. Dow

ell, D

uke U

nivers

ity,

Durha

m, N

C

1000

hrs

AIAA-2

015-3

436

Aero

dyna

mic S

hape

Opt

imiza

tion

of a

Truss-

Brac

ed-W

ing A

ircra

ftD.

Ivald

i, N. S

ecco

, S. C

hen,

J. Hw

ang,

J. Ma

rtins,

Unive

rsity

of Mi

chiga

n, An

n Arbo

r, An

n Arbo

r, MI

1030

hrs

AIAA-2

015-3

437

Cons

idera

tions

abou

t Wint

ip De

vices

Des

ign of

Tran

spor

t Ai

rplan

eB.

Matt

os, A

. Pau

la, P.

Koma

tsu,

Tech

nolog

ical In

stitut

e of A

erona

utics

(ITA)

, São

José

dos C

ampo

s, Br

azil

120

Frida

y, 26

June

201

530

8-MA

O-13

Unce

rtaint

y II

Manc

heste

rCh

aired

by: S

. CHO

WDH

URY,

Missi

ssipp

i Stat

e Univ

ersity

and S

. FER

GUSO

N, N

orth C

arolin

a Stat

e Univ

ersity

0900

hrs

AIAA-2

015-3

438

Multi-

Objec

tive O

ptim

izatio

n Un

der

Unce

rtaint

yC.

Liang

, S. M

ahad

evan

, Van

derbi

lt Un

iversi

ty, N

ashv

ille, T

N

0930

hrs

AIAA-2

015-3

439

A Mu

lti-Fid

elity

App

roac

h to

Qu

antifi

catio

n of

Unc

erta

inty i

n Sta

bility

and C

ontro

l Dat

abas

es

for u

se in

Stoc

hasti

c Airc

raft

Simula

tions

A. We

ndorf

f, J.

Alons

o, St

anfor

d Un

iversi

ty, S

tanfor

d, CA

; S. B

ieniaw

ski,

The B

oeing

Comp

any,

Seatt

le, W

A

1000

hrs

AIAA-2

015-3

440

Sculpt

ing: A

Fast,

Inter

activ

e Meth

od

for Pr

obab

ilistic

Desi

gn Sp

ace

Explo

ratio

n and

Mar

gin Al

locati

onR.

Cook

e, Re

source

s for

the Fu

ture,

Washi

ngton

, DC;

T. Za

ng, Z

ang M

&S

Consu

lting,

LLC, Z

ebulo

n, NC

; D. M

avris,

J. Ta

i, Ge

orgia

Institu

te of

Techn

ology,

Atlan

ta, GA

1030

hrs

AIAA-2

015-3

441

Multid

iscipl

inary

Unc

erta

inty

Quan

tifica

tion

in Ae

roela

stic

Analy

ses o

f Sem

i-Spa

n Su

perso

nic

Trans

port

Wing

M. N

ikbay

, P. A

car, I

stanb

ul Te

chnic

al Un

iversi

ty, Is

tanbu

l, Turk

ey

1100

hrs

AIAA-2

015-3

442

An In

tegra

ted Fr

amew

ork

for B

ayes

ian U

ncer

taint

y Qu

antifi

catio

n an

d Pro

babil

istic

Multi-

Crite

ria D

ecisi

on M

aking

in

Aero

-Engin

e Pre

limina

ry D

esign

J. Gr

amaty

ka, M

. Eres

, J. S

canla

n, Un

iversi

ty of

South

ampto

n, So

utham

pton,

Unite

d King

dom;

M. M

oss,

R. Ba

tes, R

olls-

Royc

e Grou

p plc,

Derb

y, Un

ited K

ingdo

m

1130

hrs

AIAA-2

015-3

443

A Str

ateg

y for

Pro

babil

istic

Marg

in Al

locat

ion in

Airc

raft

Conc

eptu

al De

sign

T. Za

ng, Z

ang M

&S Co

nsult

ing, L

LC,

Zebu

lon, N

C; S.

Mah

adev

an, V

ande

rbilt

Unive

rsity,

Nas

hville

, TN;

J. Ta

i, D.

Mavri

s, Ge

orgia

Institu

te of

Tech

nolog

y, Atl

anta,

GA

Frida

y, 26

June

201

530

9-NW

-10

0900

- 09

30 h

rsNe

twor

king C

offe

e Bre

akMe

eting

Roo

m Fo

yers

Auth

or/S

essio

n Ch

air In

dex

A. da

Silv

a, R.,

9-AF

M-2

Abde

lhady

, M.,

43-AF

M-3

Abde

llatif,

O.,

178-M

ST-8

Abdo

l-Ham

id, K.

, 160

-APA-1

7, 2

33-AP

A-25

Abdra

shito

v, R.,

226

-AA-31

Abdu

l-Lati

f, A.,

12-A

PA-1

Abe,

M., 2

3-CFD

-3Ab

e, T.,

144

-PDL-7

Abe,

Y., 1

30-CF

D-13

Acar,

E., 6

4-MAO

-2Ac

ar, P.

, 308

-MAO

-13Ad

ams,

N., 8

7-APA

-9Ad

ler, M

., 24

5-CFD

-30Ad

usum

illi, S

., 15

9-AMT

-10/G

T-10

Afsar,

M.,

79-AA

-13, 2

09-FD

-24Ag

arwal,

N.,

226-A

A-31

Agarw

al, R.

, 26-F

D-2, 4

7-APA

-5, 1

22-AP

A-13,

1

39-FD

-18, 1

82-TP

-9, 2

11-FD

-26, 3

04-CF

D-34

Agbo

losu-A

miso

n, S.

, 197

-ATIO

-18Ag

ostin

i, L.,

80-AA

-14, 3

02-CF

D-32

Ahma

d, N.

, 163

-ASE-1

, 237

-ASE-3

, 272

-ASE-4

, 2

98-AT

IO-27

Ahme

d, N.

, 115

-AA-19

Ahsa

n, N.

, 136

-FD-15

Ahuja

, K.,

189-A

A-30,

261

-AA-39

Ahuja

, V.,

127-A

TIO-13

, 161

-APA-1

8Aig

ner, M

., 18

5-AA-2

6

Airiau

, C.,

5-AA-3

Akay

din, H

., 49

-APA-7

Akba

rzade

h, S.

, 131

-CFD-1

4Ak

ella,

M., 9

-AFM-

2Ak

htar, I

., 13

3-CFD

-16, 1

36-FD

-15Ak

illi, H

., 25

-FD-1

Akins

, D.,

279-F

D-31

Alaou

i, M.,

226-A

A-31

Alaza

rd, D

., 83

-AFM-

5Alb

a, C.,

34-T

P-1Alb

ring,

T., 2

52-M

AO-9,

283

-MAO

-10Alb

uque

rque,

P., 1

04-M

AO-3

Alcab

in, M

., 27

5-ATIO

-25Alc

orn, J

., 25

0-LTA

-1Ale

ksen

tsev,

A., 1

89-AA

-30Ale

ssand

ro, T.

, 108

-TP-5

Alexa

nder,

W.,

37-AA

-6, 3

8-AA-7

, 114

-AA-18

, 1

52-AA

-22, 1

87-AA

-28, 2

60-AA

-38, 2

61-AA

-39Ale

xeen

ko, A

., 35

-TP-2,

288

-TP-13

Alexe

ev, T

., 9-A

FM-2,

105

-MST

-5Alf

onso

, X.,

234-A

PA-26

Algoz

ino, S

., 23

6-APA

-28Ali

aga,

C., 1

96-AS

E-2Ali

zard,

F., 9

8-CFD

-12All

en, B

., 16

5-ATIO

-16, 1

99-AT

IO-20

Allen

, C.,

64-M

AO-2,

125

-APA-1

6, 2

83-M

AO-10

Allen

, J.,

104-M

AO-3

Allen

, N.,

45-AM

T-3/G

T-3All

erdice

, J.,

197-A

TIO-18

Alliso

n, D.

, 104

-MAO

-3All

maras

, S.,

95-CF

D-9, 1

23-AP

A-14,

170

-CFD-1

8Alm

eida,

F., 2

49-FT

-1Alm

ond,

M., 8

8-APA

-10Alo

nso,

E., 1

26-AT

IO-12

Alons

o, J.,

202

-CFD-2

2, 2

04-CF

D-24,

212

-MAO

-6,

283

-MAO

-10, 2

84-M

AO-11

, 308

-MAO

-13Alo

nso-M

iralle

s, J.,

260

-AA-38

AlQad

i, I.,

236-A

PA-28

Alter,

S.,

233-A

PA-25

Altmi

kus,

A., 8

8-APA

-10Alu

nni, A

., 21

6-TP-1

0/PD

L-10

Alves

, L.,

243-C

FD-28

Aly, A

., 17

8-MST

-8Aly

anak

, E.,

104-M

AO-3,

176

-MAO

-5Alz

amora

Prev

itali,

F., 1

02-FD

-13Am

adori

, K.,

283-M

AO-10

Amara

l, F.,

230-A

A-35

Amili,

O.,

153-A

A-23

Amita

y, M.

, 63-F

D-9, 1

01-FD

-12, 2

48-FD

-29Am

os, D

., 35

-TP-2

Amun

dson

, I.,

128-A

TIO-14

Anan

da Kr

ishna

n, G.

, 15-A

PA-4

Anda

libi, M

., 48

-APA-6

Ande

rs, S

., 49

-APA-7

, 281

-GEPC

-1

Ande

rson,

J., 2

31-AA

-36An

derso

n, W.

, 95-C

FD-9,

170

-CFD-1

8, 3

05-CF

D-35

Andre

, F.,

65-M

ST-3

Andre

ws, S

., 14

1-MAO

-4, 2

67-AP

A-29

Andri

enko

, D.,

69-TP

-4, 2

56-TP

-12An

emaa

t, W.

, 117

-ACD-3

, 232

-ACD-6

Angla

nd, D

., 20

5-CFD

-25, 2

59-AA

-37, 2

63-AA

-41An

saldi

, T.,

5-AA-3

Antho

ny, J

., 27

8-FD-3

0An

tônio

dos S

antos

, D.,

30-M

ST-1

Anton

y, T.,

44-A

FM-4

Anup

indi, K

., 17

1-CFD

-19Ao

ki, T.

, 68-T

P-3Ao

ki, Y.

, 89-A

PA-11

Aono

, H.,

268-A

PA-30

Apon

so, B

., 91

-ATIO

-9Ap

pel, C

., 22

6-AA-3

1Ap

pelba

um, J

., 25

9-AA-3

7Ara

dag,

S., 2

04-CF

D-24

Arena

, A.,

157-A

FM-9

Arina

, R.,

155-A

A-25

Arnal,

D.,

99-FD

-10Arn

dt, C.

, 266

-AMT-1

3/GT

-13Arn

eson

, H.,

18-AT

IO-3,

298

-ATIO

-27Aro

ra, N

., 97

-CFD-1

1, 2

48-FD

-29, 2

68-AP

A-30

Arsen

yev,

I., 2

84-M

AO-11

Aru

najat

esan

, S.,

139-F

D-18,

175

-FD-22

, 229

-AA-34

Asad

a, K.,

60-F

D-6/P

DL-2

Asan

o, K.,

60-F

D-6/P

DL-2

Ashle

y, A.,

176

-MAO

-5As

hton,

N., 1

72-CF

D-20,

230

-AA-35

Astle

y, R.,

78-A

A-12

Atassi

, H.,

77-AA

-11, 1

51-AA

-21Ati

nault

, O.,

13-AP

A-2Atk

ins, E

., 27

4-ATIO

-24Atk

ins, S

., 14

0-ITA

R-2Att

anas

io, L.

, 13-A

PA-2,

104

-MAO

-3Au

bert,

A., 4

0-AA-9

Aubry

, S.,

42-AC

D-1, 2

99-AT

IO-28

Avery

, A.,

196-A

SE-2

Awas

thi, M

., 26

1-AA-3

9Ay

ton, L

., 26

0-AA-3

8Ay

yad,

E., 3

1-MST

-2Ay

yalas

omay

ajula,

S.,

284-M

AO-11

, 300

-ATIO

-29Az

arm, S

., 29

-MAO

-1Az

arpey

vand

, M.,

3-AA-1

, 38-A

A-7Az

eved

o, J.,

12-A

PA-1,

98-C

FD-12

, 241

-CFD-2

6,

270

-APA-3

2Ba

bbar,

Y., 9

-AFM-

2, 1

24-AP

A-15,

270

-APA-3

2Ba

ccala,

L., 7

-AA-5

Badri

nath,

S.,

136-F

D-15

Baed

er, J.

, 162

-APA-1

9, 1

71-CF

D-19

Bagin

ski, F

., 20

0-BAL

-2Ba

gwell

, T.,

140-I

TAR-2

121

Auth

or/S

essio

n Ch

air In

dex

Bahr,

C., 1

86-AA

-27, 1

88-AA

-29, 2

62-AA

-40Ba

i, B.,

112-A

A-16

Bai, J

., 49

-APA-7

, 145

-TP-7

Bailly

, C.,

4-AA-2

, 114

-AA-18

, 231

-AA-36

Bailly

, D.,

161-A

PA-18

Bake

, F.,

41-AA

-10, 1

51-AA

-21Ba

kker,

B.,

238-A

TIO-21

Balak

umar,

P., 6

1-FD-7

, 139

-FD-18

, 248

-FD-29

Balan

, A.,

95-CF

D-9Ba

lares

que,

N., 8

8-APA

-10Ba

las, G

., 15

7-AFM

-9Ba

lboni,

J., 1

08-TP

-5, 2

16-TP

-10/P

DL-10

Balda

cchino

, D.,

279-F

D-31

Balla

rd, B

., 27

5-ATIO

-25Ba

ne, S

., 25

5-PDL

-12Ba

ngert

, L.,

14-AP

A-3Ba

rbarin

o, M.

, 6-AA

-4, 1

15-AA

-19Ba

rbeau

, Z.,

274-A

TIO-24

Barm

ore, B

., 29

8-ATIO

-27Ba

rnes,

C., 2

70-AP

A-32

Barne

s, J.,

83-A

FM-5

Barte

ls, R.

, 124

-APA-1

5Ba

rtoli,

N., 8

2-ACD

-2Ba

rtosch

, S.,

299-A

TIO-28

Basti

de, M

., 45

-AMT-3

/GT-3

Basto

, K.,

234-A

PA-26

Bates

, R.,

308-M

AO-13

Bathe

l, B.,

86-AM

T-6/G

T-6,

121

-AMT-8

/FD-1

4/TP

-6/GT

-8Ba

tista,

M.,

30-M

ST-1

Batte

n, P.,

245

-CFD-3

0Ba

uer, M

., 12

5-APA

-16Ba

uman

, P.,

108-T

P-5Ba

umgä

rtner,

D.,

283-M

AO-10

Bayd

ar, E.

, 279

-FD-31

Bayo

da, K

., 33

-PDL-1

/FD-5

Beav

erstoc

k, C.,

29-M

AO-1

Beck

, J.,

35-TP

-2Be

doue

t, J.,

299

-ATIO

-28Be

kirop

oulos

, D.,

155-A

A-25

Belle

mans

, A.,

216-T

P-10/

PDL-1

0Be

lley,

C., 2

04-CF

D-24

Belm

ouss,

M.,

255-P

DL-12

Belya

ev, I

., 11

5-AA-1

9, 1

87-AA

-28, 1

89-AA

-30Be

nard,

N.,

33-PD

L-1/F

D-5, 1

80-PD

L-8/A

PA-20

Bend

er, J.

, 256

-TP-12

Benn

aceu

r, I.,

154-A

A-24

Bento

n, S.

, 50-A

PA-8

Berci

, M.,

236-A

PA-28

Berda

nier, R

., 17

3-FD-1

9Be

resh,

S., 62

-FD-8,

175-F

D-22,

192-A

MT-12

/GT-1

2,

266

-AMT-1

3/GT

-13

Berge

ron, K

., 23

6-APA

-28Be

ring,

E., 2

00-BA

L-2Bé

riot,

H., 2

63-AA

-41Be

rkefel

d, T.,

186

-AA-27

, 260

-AA-38

Berna

rdini,

G.,

162-A

PA-19

, 263

-AA-41

Berna

rdo, J

., 52

-ATIO

-6, 1

98-AT

IO-19

Berne

r, C.,

47-AP

A-5Be

rry, P

., 28

3-MAO

-10Be

rry, S

., 21

7-TP-1

1Be

rsene

v, Y.,

189

-AA-30

Berto

n, J.,

77-A

A-11

Beulz

e, B.

, 92-A

TIO-10

Beuz

e, B.

, 18-A

TIO-3

Beva

n, R.,

125

-APA-1

6Be

virt,

J., 2

76-AT

IO-26

Bhag

at, N

., 10

4-MAO

-3Bh

agwa

ndin,

V., 2

67-AP

A-29

Bham

idipa

ti, K.,

22-C

FD-2

Bhau

mik,

S., 2

05-CF

D-25

Bianc

hi, D

., 12

8-ATIO

-14Bib

ik, P.

, 280

-FT-2/

GT-14

Bidino

, D.,

45-AM

T-3/G

T-3Bie

nert,

N.,

51-AT

IO-5

Bienia

wski,

S.,

308-M

AO-13

Bienie

k, D.

, 237

-ASE-3

Bier, N

., 10

5-MST

-5Bij

l, H.,

97-CF

D-11

Bil, C

., 42

-ACD-1

, 117

-ACD-3

, 190

-ACD-5

Bilim

oria,

K., 1

77-M

ST-7

Bin Ab

dul M

alik,

M., 1

62-AP

A-19

Bisek

, N.,

98-CF

D-12,

143

-PDL-6

, 245

-CFD-3

0Bla

ckwe

ll, B.

, 68-T

P-3Bla

ir, L.,

143

-PDL-6

Blaisd

ell, G

., 11

3-AA-1

7, 1

39-FD

-18, 2

45-CF

D-30

Blake

, M.,

142-M

ST-6

Blake

, W.,

8-AFM

-1, 2

9-MAO

-1, 2

73-AS

E-5Bla

ndea

u, V.,

77-A

A-11

Bleisc

hwitz

, R.,

136-F

D-15

Bletzi

nger,

K., 2

83-M

AO-10

Bloeb

aum,

C., 2

12-M

AO-6

Blom,

H.,

238-A

TIO-21

Bo, Y

., 35

-TP-2,

145

-TP-7

Bobe

nrieth

Mise

rda, R

., 77

-AA-11

Boco

la, F.

, 84-A

FM-6

Bode

n, F.,

231

-AA-36

Bode

n, H.

, 7-AA

-5, 2

61-AA

-39Bo

gdan

off, D

., 18

2-TP-9

Boge

y, C.,

4-AA

-2, 5

-AA-3,

229

-AA-34

Boiss

onne

au, F

., 18

9-AA-3

0Bo

lczak

, C.,

299-A

TIO-28

Bolds

-Moo

rehea

d, P.,

249

-FT-1

Bolen

der, M

., 44

-AFM-

4

Bomb

elli, A

., 27

5-ATIO

-25Bo

nnet,

J., 1

80-PD

L-8/A

PA-20

Bons

, J.,

50-AP

A-8Bo

o, K.,

12-A

PA-1

Boom

, P.,

132-C

FD-15

Borde

neuv

e, J.,

83-A

FM-5

Borer

, N.,

127-A

TIO-13

Borg,

M.,

137-F

D-16

Borge

s Seb

astia

o, I.,

288

-TP-13

Borgo

ltz, A

., 29

5-APA

-34, 2

97-AP

A-37

Borne

r, A.,

288-T

P-13

Bosso

n, C.,

16-A

TIO-1

Botez

, R., 1

3-APA

-2, 18

-ATIO-

3, 66

-MST

-4, 84

-AFM-

6,

92-A

TIO-10

, 238

-ATIO

-21, 2

96-AP

A-35

Bouh

aj, M

., 22

6-AA-3

1Bo

uley,

S., 1

52-AA

-22Bo

usfie

ld, S

., 12

7-ATIO

-13Bo

ussu

ge, J

., 18

8-AA-2

9Bo

uty, E

., 18

5-AA-2

6Bo

uvy,

Q., 2

59-AA

-37Bo

va, S

., 20

2-CFD

-22Bo

wers,

L., 1

66-AT

IO-17

, 239

-ATIO

-22Bo

wn, A

., 16

7-BAL

-1Bo

xx, I

., 26

6-AMT

-13/G

T-13

Boyd

, I.,

35-TP

-2, 6

9-TP-4

, 256

-TP-12

Brak

ke, K

., 20

0-BAL

-2Br

amble

y, E.,

7-AA

-5, 8

1-AA-1

5Br

andis

, A.,

69-TP

-4, 2

17-TP

-11Br

ando

n, J.,

118

-AFM-

7, 2

49-FT

-1Br

andt,

S.,

64-M

AO-2

Brau

ckma

nn, G

., 23

3-APA

-25Br

aud,

P., 1

89-AA

-30Br

azier

, J.,

228-A

A-33

Brea

rd, C.

, 4-AA

-2, 6

-AA-4

Breh

m, C.

, 4-AA

-2Br

eitsa

mter,

C., 8

7-APA

-9Br

ès, G

., 5-A

A-3, 8

0-AA-1

4Br

evigl

ieri, C

., 24

1-CFD

-26Br

ichet,

G.,

4-AA-2

Bridg

es, J

., 18

9-AA-3

0, 2

27-AA

-32Br

iley,

W., 1

5-APA

-4, 2

97-AP

A-37

Britc

hford,

K., 2

27-AA

-32Br

oeren

, A.,

196-A

SE-2

Bron

z, M.

, 161

-APA-1

8Br

osza

t, D.

, 151

-AA-21

Brow

n, C.,

189

-AA-30

, 228

-AA-33

, 280

-FT-2/

GT-14

Brow

n, K.,

297

-APA-3

7Br

own,

L., 1

58-AM

T-9/G

T-9Br

own,

M., 1

43-PD

L-6, 2

14-M

ST-9

Brow

n, R.,

9-AF

M-2

Brun

et, M

., 42

-ACD-1

Brya

n, B.

, 261

-AA-39

Bueh

n, J.,

303

-CFD-3

3Bu

geda

, G.,

180-P

DL-8/

APA-2

0Bu

lte, J

., 3-A

A-1, 2

61-AA

-39, 2

62-AA

-40Bu

nge,

R., 8

-AFM-

1, 2

49-FT

-1Bu

ning,

P., 2

30-AA

-35Bu

ono,

A., 3

7-AA-6

Burns

, R.,

86-AM

T-6/G

T-6Bu

rnside

, N.,

186-A

A-27

Burt,

J., 6

9-TP-4

, 181

-PDL-9

/TP-8

Burtc

h, T.,

8-AF

M-1

Busch

, G.,

37-AA

-6Bu

sque

ts, J.

, 126

-ATIO

-12Bu

ttini, T

., 9-A

FM-2

Byerl

ey, A

., 15

-APA-4

Bynu

m, M

., 99

-FD-10

Cai, J

., 67

-PDL-3

, 178

-MST

-8Ca

i, W.,

145-T

P-7Ca

in, A.

, 88-A

PA-10

, 143

-PDL-6

, 255

-PDL-1

2Ca

ldas,

L., 7

-AA-5

Calla

han,

R., 2

94-AM

T-14/

GT-15

Calle

nder,

M.,

62-FD

-8Ca

llicoa

t, J.,

231

-AA-36

Calve

rt, M

., 15

-APA-4

, 194

-APA-2

2Ca

lvert,

N.,

86-AM

T-6/G

T-6Ca

mpbe

ll, S.

, 16-A

TIO-1,

298

-ATIO

-27Ca

ndler

, G.,

139-F

D-18,

202

-CFD-2

2, 2

44-CF

D-29,

2

46-FD

-27, 2

56-TP

-12, 2

78-FD

-30Ca

nfield

, R.,

252-M

AO-9

Canp

olat,

C., 2

5-FD-1

Cantu

, L.,

86-AM

T-6/G

T-6Ca

pittin

i, G.,

236-A

PA-28

Capiz

zano

, F.,

6-AA-4

, 115

-AA-19

Capre

cci, M

., 5-A

A-3Ca

raball

o, E.,

175

-FD-22

Carae

ni, M

., 39

-AA-8

Cardi

to, F.

, 162

-APA-1

9Ca

riou,

J., 2

72-AS

E-4Ca

rlson

, J.,

58-CF

D-8, 1

33-CF

D-16

Carm

ine, M

., 26

-FD-2

Caro,

S.,

6-AA-4

, 113

-AA-17

Carol

us, T

., 15

2-AA-2

2Ca

rranz

a Moy

ao, O

., 84

-AFM-

6Ca

rroll,

D., 1

07-PD

L-4, 1

66-AT

IO-17

Carso

n, H.

, 170

-CFD-1

8Ca

rter, C

., 26

6-AMT

-13/G

T-13

Cartm

ell, D

., 31

-MST

-2Ca

ruelle

, B.,

155-A

A-25

Casa

lino,

D., 1

88-AA

-29, 2

59-AA

-37Ca

salis,

G.,

228-A

A-33

Casa

rtelli,

E., 2

03-CF

D-23

Casp

er, K.

, 28-F

D-4, 1

03-IT

AR-1,

140

-ITAR

-2,

175

-FD-22

Castn

er, R.

, 14-A

PA-3

Cathe

y, H.

, 167

-BAL-1

Catle

tt, M

., 23

1-AA-3

6Ca

ttafes

ta, L.

, 248

-FD-29

Caud

le, D

., 83

-AFM-

5Ca

valie

ri, A.,

5-AA

-3, 41

-AA-10

, 80-A

A-14,

189-A

A-30,

2

60-AA

-38Ce

dric,

C., 1

32-CF

D-15

Cerm

inara,

A., 2

09-FD

-24Ce

snik,

C., 9

-AFM-

2, 1

19-AF

M-8

Cetin

, M.,

80-AA

-14Ch

abot,

J., 1

75-FD

-22Ch

aderj

ian, N

., 13

6-FD-1

5Ch

akrab

orty,

I., 4

2-ACD

-1, 1

56-AC

D-4, 2

65-AC

D-7Ch

akrab

orty,

P., 2

46-FD

-27Ch

akrav

arthy

, S.,

245-C

FD-30

Chalo

t, F.,

99-F

D-10

Chan

, W.,

305-C

FD-35

Chan

dar, D

., 30

5-CFD

-35Ch

aney

, V.,

249-F

T-1Ch

ang,

C., 1

93-AP

A-21,

211

-FD-26

, 228

-AA-33

Chan

g, S.

, 35-T

P-2, 1

45-TP

-7Ch

ao, H

., 43

-AFM-

3Ch

ao, T

., 11

9-AFM

-8Ch

aput,

A., 8

2-ACD

-2, 1

28-AT

IO-14

Chard

, J.,

271-A

PA-33

Charn

igo, R

., 18

1-PDL

-9/TP

-8Ch

atterj

i, G.,

142-M

ST-6,

253

-MST

-11Ch

auvin

, A.,

227-A

A-32

Chaw

ner, J

., 30

1-CFD

-31Ch

azot,

O.,

108-T

P-5Ch

edev

ergne

, F.,

60-FD

-6/PD

L-2Ch

eli, R

., 26

-FD-2

Cheli

us, A

., 18

7-AA-2

8Ch

elliah

, K.,

262-A

A-40

Chen

, G.,

301-C

FD-31

Chen

, L.,

191-A

MT-11

/GT-1

1, 2

50-LT

A-1Ch

en, N

., 92

-ATIO

-10, 1

91-AM

T-11/

GT-11

Chen

, P.,

284-M

AO-11

Chen

, S.,

269-A

PA-31

, 307

-MAO

-12Ch

en, W

., 10

7-PDL

-4, 1

51-AA

-21, 2

60-AA

-38Ch

en, X

., 11

2-AA-1

6, 1

45-TP

-7Ch

en, Y

., 34

-TP-1

Chen

g, G.

, 193

-APA-2

1, 2

11-FD

-26Ch

eng,

H., 2

29-AA

-34Ch

eng,

J., 1

22-AP

A-13

Chen

g, Y.,

215

-MST

-10Ch

ernys

hev,

S., 2

28-AA

-33Ch

evall

ey, E

., 51

-ATIO

-5Ch

habra

, R.,

29-M

AO-1

Chiba

, K.,

293-A

CD-8

Chier

eghin

, N.,

270-A

PA-32

122

Auth

or/S

essio

n Ch

air In

dex

Chint

agun

ta, A.

, 80-A

A-14

Chng

, S.,

162-A

PA-19

Chng

, T.,

143-P

DL-6

Cho,

K., 2

35-AP

A-27

Choi,

J., 2

7-FD-3

, 55-C

FD-5,

62-F

D-8, 1

32-CF

D-15,

1

33-CF

D-16,

251

-MAO

-8, 2

96-AP

A-35

Choi,

S., 1

2-APA

-1, 64

-MAO

-2, 89

-APA-1

1, 13

2-CFD

-15,

251

-MAO

-8, 2

96-AP

A-35,

307

-MAO

-12Ch

ong,

T., 3

-AA-1

Chou

, A.,

209-F

D-24

Chou

dhari

, M.,

56-CF

D-6, 9

9-FD-1

0, 1

37-FD

-16,

155

-AA-25

, 230

-AA-35

Chou

dhary

, A.,

97-CF

D-11

Chou

tapall

i, I.,

276-A

TIO-26

Chow

dhary

, G.,

274-A

TIO-24

Chow

dhury

, S., 1

76-M

AO-5,

213-M

AO-7,

251-M

AO-8,

3

08-M

AO-13

Chris

tophe

, J.,

79-AA

-13, 1

12-AA

-16Ch

ua, Z

., 65

-MST

-3Ch

udob

a, B.

, 53-A

TIO-7

Chue

, R.,

269-A

PA-31

Chwa

lowsk

i, P.,

124-A

PA-15

Chyn

oweth

, B.,

28-FD

-4Cia

rella,

A., 2

9-MAO

-1Cil

iberti,

D.,

13-AP

A-2Cin

nella

, P.,

62-FD

-8, 1

13-AA

-17, 1

32-CF

D-15

Cioba

ca, V

., 12

5-APA

-16Cis

neros

, E.,

216-T

P-10/

PDL-1

0Cis

otto,

A., 4

6-AMT

-4/GT

-4Civ

inska

s, K.,

281

-GEPC

-1Cla

ir, V.,

6-AA

-4, 1

13-AA

-17Cla

rk, A.

, 276

-ATIO

-26Cla

rk, I.

, 38-A

A-7Cla

rke, S

., 24

0-ATIO

-23Cle

mens

, N.,

33-PD

L-1/F

D-5, 1

74-FD

-20Clé

ro, F.

, 185

-AA-26

Cliff,

S.,

89-AP

A-11

Cling

man,

D., 6

3-FD-9

Close

, S.,

286-P

DL-13

Clouti

er, R.

, 239

-ATIO

-22Clu

ts, J.

, 153

-AA-23

Coak

ley, T

., 17

2-CFD

-20Co

bb, P

., 14

2-MST

-6Co

bb, R

., 14

1-MAO

-4, 1

58-AM

T-9/G

T-9Co

der, J

., 58

-CFD-8

, 61-F

D-7Co

en, P

., 28

1-GEP

C-1Co

etzee

, E.,

105-M

ST-5

Cofer

, A.,

35-TP

-2Co

ggon

, S.,

213-M

AO-7

Cohe

n, E.,

226

-AA-31

Colan

tonio,

R., 2

81-GE

PC-1

Colbu

rn, K.

, 301

-CFD-3

1

Cole,

S.,

45-AM

T-3/G

T-3Co

llery,

O.,

226-A

A-31

Collin

s, E.,

41-A

A-10,

81-A

A-15

Colm

enare

s, J.,

96-C

FD-10

, 205

-CFD-2

5Co

loe, B

., 27

4-ATIO

-24Co

lonius

, T.,

5-AA-3

, 80-A

A-14,

228

-AA-33

Colon

no, M

., 21

2-MAO

-6Co

mmo,

S., 1

20-AM

T-7/G

T-7, 2

94-AM

T-14/

GT-15

Comm

unier

, D.,

84-AF

M-6

Cons

tantin

escu

, E.,

163-A

SE-1

Cook

e, R.,

308

-MAO

-13Co

ppen

barge

r, R.,

91-AT

IO-9

Corde

s, U.

, 50-A

PA-8,

271

-APA-3

3Co

reixa

s, C.,

188

-AA-29

Corre

ale, G

., 33

-PDL-1

/FD-5

, 60-F

D-6/P

DL-2

Corre

ia Gr

ácio,

B.,

31-M

ST-2

Corrig

an, A

., 15

3-AA-2

3Co

stes,

M., 1

61-AP

A-18

Cotto

n, W.

, 275

-ATIO

-25Co

ulouv

rat, F

., 11

4-AA-1

8Co

upe,

J., 9

1-ATIO

-9, 1

98-AT

IO-19

Coup

land,

J., 7

8-AA-1

2, 2

64-AA

-42Co

urty,

J., 9

9-FD-1

0Co

usy,

M., 6

5-MST

-3Co

yle, C

., 90

-APA-1

2, 1

95-AP

A-23

Cozz

i, F.,

26-FD

-2Cra

ig, S

., 13

7-FD-1

6Cra

nford,

J., 3

0-MST

-1Cra

wford

, B.,

137-F

D-16

Crawl

ey, M

., 15

3-AA-2

3Cro

mer, K

., 28

2-LTA

-2Cro

ss, C.

, 165

-ATIO

-16, 1

99-AT

IO-20

Crossl

ey, W

., 52

-ATIO

-6, 8

2-ACD

-2Cro

uch,

J., 6

1-FD-7

Crow,

B.,

197-A

TIO-18

Crowt

her, W

., 30

-MST

-1, 2

71-AP

A-33

Crude

n, B.

, 69-T

P-4, 1

82-TP

-9, 2

17-TP

-11Cru

z, E.,

63-F

D-9Cu

enca

, R.,

7-AA-5

Cui, D

., 17

8-MST

-8Cu

i, H.,

44-AF

M-4

Cui, K

., 29

6-APA

-35Cu

lbreth

, W.,

31-M

ST-2

Cumm

ings,

R., 6

3-FD-9

, 160

-APA-1

7, 2

36-AP

A-28,

2

78-FD

-30, 3

05-CF

D-35

Cunh

a, G.

, 155

-AA-25

Cunh

a, M.

, 282

-LTA-2

Cuoc

i, A.,

244-C

FD-29

Curle

y, A.,

306

-CFD-3

6Cu

rran,

R., 5

1-ATIO

-5, 9

1-ATIO

-9, 1

98-AT

IO-19

, 2

75-AT

IO-25

Cusa

ti, V.,

13-A

PA-2

Cutle

r, A.,

86-AM

T-6/G

T-6,

121

-AMT-8

/FD-1

4/TP

-6/GT

-8Cy

mbali

st, N

., 27

-FD-3,

278

-FD-30

D’So

uza,

S., 4

3-AFM

-3Da

Ronc

h, A.,

9-AF

M-2,

84-A

FM-6

da S

ilva,

A., 4

-AA-2

da S

ilva,

F., 4

-AA-2

Dahl,

D.,

39-AA

-8Da

hl, M

., 78

-AA-12

Dale,

G.,

26-FD

-2, 2

10-FD

-25Da

lle, D

., 23

3-APA

-25Da

ly, C.

, 38-A

A-7Da

moda

ran, M

., 20

5-CFD

-25, 2

35-AP

A-27,

250

-LTA-1

Danc

ila, B

., 92

-ATIO

-10Da

ncila

, R.,

18-AT

IO-3

Dane

hy, P

., 86

-AMT-6

/GT-6

, 1

21-AM

T-8/F

D-14/

TP-6/

GT-8

Danie

ls, C.

, 273

-ASE-5

Dann

enho

ffer, J

., 30

1-CFD

-31Da

ntske

r, O.,

87-AP

A-9Da

oud,

F., 2

12-M

AO-6

Darm

ofal, D

., 95

-CFD-9

, 170

-CFD-1

8Da

skira

n, O.

, 128

-ATIO

-14Da

vidso

n, L.,

6-AA

-4, 1

15-AA

-19, 1

54-AA

-24Da

viller

, G.,

229-A

A-34

Davis

, D.,

85-AM

T-5/G

T-5Da

vis, R

., 20

3-CFD

-23Da

vy, R

., 3-A

A-1, 2

62-AA

-40Da

wson

, R.,

174-F

D-20

Daws

on, S

., 13

6-FD-1

5De

Breu

ker, R

., 29

-MAO

-1de

Jong

, A.,

38-AA

-7De

Kat,

R., 1

36-FD

-15De

La Pu

ente,

F., 2

59-AA

-37De

Marc

o, A.,

8-AF

M-1,

104

-MAO

-3de

Mon

te, F.

, 35-T

P-2de

Oliv

eira,

G., 2

86-PD

L-13

De Ro

eck,

W., 1

13-AA

-17de

San

tana,

L., 3

-AA-1

de S

ouza

, F.,

192-A

MT-12

/GT-1

2De

Armon

, J.,

197-A

TIO-18

DeBo

nis, J

., 55

-CFD-5

, 130

-CFD-1

3, 1

75-FD

-22De

Chan

t, L.,

139

-FD-18

DeCic

co, A

., 65

-MST

-3, 1

42-M

ST-6

Deck

er, R.

, 278

-FD-30

Dedic

, C.,

181-P

DL-9/

TP-8

Dees

, J.,

173-F

D-19

Dees

e, J.,

282

-LTA-2

DeGe

nnaro

, A.,

295-A

PA-34

Degre

z, G.

, 216

-TP-10

/PDL

-10De

inert,

S.,

212-M

AO-6

Del R

ey Fe

rnánd

ez, D

., 16

9-CFD

-17, 2

42-CF

D-27

Del R

osari

o, R.,

281

-GEPC

-1De

Laure

ntis,

D., 5

2-ATIO

-6, 23

9-ATIO

-22, 3

00-AT

IO-29

Deleg

lise, B

., 46

-AMT-4

/GT-4

Delfs

, J.,

79-AA

-13, 1

12-AA

-16, 2

30-AA

-35,

231

-AA-36

, 263

-AA-41

Delisi

, D.,

237-A

SE-3,

272

-ASE-4

Dell’O

rso, H

., 10

1-FD-1

2, 2

48-FD

-29De

lla Ve

cchia,

P., 8

-AFM-

1, 1

3-APA

-2De

llery,

B.,

167-B

AL-1

Delne

ro, J.

, 236

-APA-2

8De

mauro

, E.,

101-F

D-12

Deme

autis

, C.,

45-AM

T-3/G

T-3De

mers,

F., 6

0-FD-6

/PDL

-2De

mers

Bouc

hard,

E., 2

76-AT

IO-26

Deng

, S.,

97-CF

D-11

Denia

u, H.

, 229

-AA-34

Denie

ul, Y.

, 83-A

FM-5

Denis

on, M

., 24

8-FD-2

9De

nisov

, S.,

115-A

A-19

Denis

sen,

K., 1

95-AP

A-23

Denn

is, B

., 48

-APA-6

Deod

har, N

., 28

2-LTA

-2De

rlaga

, J.,

97-CF

D-11

Desch

amps

, C.,

4-AA-2

, 80-A

A-14

Desm

et, W

., 3-A

A-1, 1

13-AA

-17De

ters,

R., 1

5-APA

-4De

venp

ort, W

., 37

-AA-6,

38-A

A-7, 1

14-AA

-18,

152

-AA-22

, 187

-AA-28

, 260

-AA-38

, 261

-AA-39

, 2

95-AP

A-34,

297

-APA-3

7De

wey,

R., 1

67-BA

L-1De

y, S.

, 301

-CFD-3

1Dh

aene

, T.,

66-M

ST-4

Dham

anka

r, N.,

245-C

FD-30

Dias,

B., 3

4-TP-1

Dias,

J., 1

18-AF

M-7

Dicke

y, D.

, 189

-AA-30

Dicke

y, E.,

49-A

PA-7,

87-A

PA-9

Dief,

T., 4

3-AFM

-3Die

rke, J

., 39

-AA-8,

185

-AA-26

, 263

-AA-41

DiGiro

lamo,

E., 2

65-AC

D-7Dil

an, G

., 28

5-MST

-12Dil

l, E.,

166-A

TIO-17

Dimota

kis, P

., 27

-FD-3,

139

-FD-18

, 244

-CFD-2

9,

278

-FD-30

Diosa

dy, L

., 21

-CFD-1

, 201

-CFD-2

1Dir

k, B.

, 230

-AA-35

Djedd

i, R.,

243-C

FD-28

Doga

n, A.,

8-AF

M-1,

83-AF

M-5,

128-A

TIO-14

, 273

-ASE-5

Doga

riu, A

., 86

-AMT-6

/GT-6

Dolfi-

Boute

yre, A

., 27

2-ASE

-4Do

nado

n, M.

, 260

-AA-38

Dong

, H.,

136-F

D-15,

248

-FD-29

Dong

, M.,

99-FD

-10Do

ng, X

., 84

-AFM-

6Do

ngre,

R., 2

50-LT

A-1Do

olan,

C., 1

15-AA

-19, 1

52-AA

-22, 2

31-AA

-36Do

ty, M

., 15

8-AMT

-9/GT

-9Do

ughe

rty, N

., 68

-TP-3,

228

-AA-33

Douv

ille, T

., 18

0-PDL

-8/AP

A-20,

269

-APA-3

1Do

well,

E., 3

07-M

AO-12

Dowl

ing, D

., 21

1-FD-2

6Do

wning

, J.,

40-AA

-9Do

yle, J

., 90

-APA-1

2Dr

aper,

M.,

274-A

TIO-24

Drew

, M.,

126-A

TIO-12

Drive

r, D.,

108-T

P-5Dr

ozda

, T.,

244-C

FD-29

Drye

r, J.,

281-G

EPC-1

Duan

, D.,

250-L

TA-1

Duan

, F.,

47-AP

A-5Du

an, L

., 13

7-FD-1

6, 2

05-CF

D-25

Duan

, Z.,

23-CF

D-3, 5

6-CFD

-6Du

bot,

T., 2

99-AT

IO-28

Dubo

urg, V

., 16

7-BAL

-1Du

bov,

Y., 3

1-MST

-2Du

cruix,

S.,

185-A

A-26

Duda

, B.,

188-A

A-29

Dudd

eck,

F., 2

84-M

AO-11

Duffy

, M.,

194-A

PA-22

Dumi

trach

e, C.,

107

-PDL-4

, 143

-PDL-6

Dunc

an, G

., 13

7-FD-1

6Du

ncan

, M.,

85-AM

T-5/G

T-5Du

nlap,

P., 2

73-AS

E-5Du

nn, S

., 45

-AMT-3

/GT-3

, 191

-AMT-1

1/GT

-11Du

nne,

R., 1

62-AP

A-19

Duqu

e, E.,

301

-CFD-3

1, 3

02-CF

D-32

Durai

samy

, K.,

58-CF

D-8Du

rak, U

., 17

7-MST

-7Du

rand,

C., 1

54-AA

-24Du

tta, S

., 44

-AFM-

4Dz

ikus,

N., 2

39-AT

IO-22

, 299

-ATIO

-28Ec

hekk

i, T.,

185-A

A-26

Econ

omon

, T., 1

33-CF

D-16,

204-C

FD-24

, 212

-MAO

-6,

271

-APA-3

3, 2

83-M

AO-10

Edgin

gton-M

itche

ll, D.

, 153

-AA-23

Edoh

, A.,

132-C

FD-15

Edwa

rds, D

., 48

-APA-6

Edwa

rds, J

., 20

3-CFD

-23Ed

wards

, M.,

86-AM

T-6/G

T-6Efr

aimsso

n, G.

, 78-A

A-12,

235

-APA-2

7Eg

orov,

I., 9

9-FD-1

0Eh

renfrie

d, K.,

260

-AA-38

Eisfel

d, B.

, 172

-CFD-2

0Eit

elberg

, G.,

37-AA

-6, 2

69-AP

A-31

123

Auth

or/S

essio

n Ch

air In

dex

Ekate

rin, J

., 56

-CFD-6

Ekici,

K., 2

43-CF

D-28

Ekme

kci, A

., 25

9-AA-3

7Ek

oule,

C., 3

7-AA-6

El ba

ialy,

I., 1

78-M

ST-8

Elham

, A.,

64-M

AO-2

Elias

son,

P., 1

60-AP

A-17

Eljac

k, E.,

236

-APA-2

8Ell

ejmi, M

., 91

-ATIO

-9Elm

iligui,

A., 1

60-AP

A-17,

285

-MST

-12Em

pl, D

., 53

-ATIO

-7En

ghard

t, L.,

151

-AA-21

, 152

-AA-22

, 173

-FD-19

Enjia

o, Z.,

119

-AFM-

8En

tz, R.

, 104

-MAO

-3En

via, E

., 26

4-AA-4

2Ep

pink,

J., 1

37-FD

-16Ere

s, M.

, 128

-ATIO

-14, 3

08-M

AO-13

Eriks

son,

L., 6

-AA-4,

154

-AA-24

Ernst,

D.,

186-A

A-27

Errico

, A.,

164-A

TIO-15

Erturk

, S.,

83-AF

M-5

Esco

bar, J

., 23

4-APA

-26Es

ker, B

., 28

1-GEP

C-1Etc

hessa

har, M

., 22

6-AA-3

1Eti

enne

, S.,

304-C

FD-34

Evan

s, A.,

126

-ATIO

-12Ev

ans,

M., 2

44-CF

D-29

Evers

man,

W., 7

-AA-5

Ewert

, R.,

38-AA

-7, 3

9-AA-8

, 41-A

A-10,

79-A

A-13,

1

12-AA

-16, 1

55-AA

-25, 1

85-AA

-26, 2

30-AA

-35Ey

i, S.,

57-CF

D-7, 1

31-CF

D-14,

244

-CFD-2

9Ey

mann

, T.,

174-F

D-20

Faga

n, A.,

189

-AA-30

Fagle

y, C.,

12-A

PA-1,

125

-APA-1

6Fa

irbrot

her, D

., 16

7-BAL

-1, 2

00-BA

L-2Fa

la, N

., 15

6-ACD

-4Fa

lcão,

C., 2

43-CF

D-28

Faliss

ard, F

., 15

4-AA-2

4Fa

n, D.

, 56-C

FD-6

Fan,

H., 1

65-AT

IO-16

, 199

-ATIO

-20Fa

n, Y.,

180

-PDL-8

/APA

-20Fa

ranos

ov, G

., 11

5-AA-1

9, 1

89-AA

-30, 2

28-AA

-33Fa

res, E

., 18

8-AA-2

9Fa

rnswo

rth, J

., 16

2-APA

-19Fa

rr, R.,

228

-AA-33

Farrin

gton,

A., 2

02-CF

D-22

Fase

l, H., 2

8-FD-4

, 100

-FD-11

, 102

-FD-13

, 208

-FD-23

Fassm

ann,

B., 7

9-AA-1

3Fa

ttah,

R., 1

13-AA

-17, 2

63-AA

-41Fe

dorov

, A.,

99-FD

-10Fe

hlman

, W.,

165-A

TIO-16

, 199

-ATIO

-20Fe

hrenb

ach,

S., 2

74-AT

IO-24

Felde

r, W.,

239-A

TIO-22

Feldh

usen

, A.,

41-AA

-10Fe

lipe,

V., 1

6-ATIO

-1Fé

lix Pa

trón,

R., 1

8-ATIO

-3Fe

ltrop,

E., 2

70-AP

A-32

Feng

, F.,

80-AA

-14Fe

nouil

, J.,

295-A

PA-34

Fergu

son,

S., 6

4-MAO

-2, 1

04-M

AO-3,

308

-MAO

-13Fe

rmen

-Coke

r, M.,

119-A

FM-8

Fern,

L., 2

74-AT

IO-24

Ferna

ndes

de O

liveir

a, R.,

104

-MAO

-3Fe

rnand

o, A.,

229

-AA-34

Ferna

ndo,

R., 1

87-AA

-28Fe

rrari,

D., 1

17-AC

D-3, 2

13-M

AO-7

Ferre

ira de

Castr

o, D.

, 30-M

ST-1

Fidko

wski,

K., 9

5-CFD

-9, 1

70-CF

D-18

Field,

J., 3

1-MST

-2Fie

lds, T

., 15

7-AFM

-9Fié

vet,

R., 3

04-CF

D-34

Filipp

one,

E., 1

64-AT

IO-15

, 300

-ATIO

-29Fil

izola,

A., 6

5-MST

-3Fin

danis

, N.,

125-A

PA-16

Finley

, D.,

47-AP

A-5, 1

61-AP

A-18

Fiore,

G.,

297-A

PA-37

Firso

v, A.,

107

-PDL-4

Fisch

els, M

., 24

3-CFD

-28Fis

cher,

P., 2

02-CF

D-22

Fisch

erswo

rring-B

unk,

A., 2

84-M

AO-11

Fishe

r, T.,

145-T

P-7, 2

02-CF

D-22

Flatau

, A.,

50-AP

A-8Fle

tcher,

D.,

181-P

DL-9/

TP-8

Fleury

, V.,

3-AA-1

, 262

-AA-40

Florez

Mera

, J.,

35-TP

-2Fo

ster, J

., 15

7-AFM

-9Fo

ster, N

., 30

5-CFD

-35Fo

ster, T

., 24

0-ATIO

-23Fo

uladi,

H.,

196-A

SE-2

Franç

ois, B

., 15

2-AA-2

2Fra

nke,

D., 1

3-APA

-2Fra

nkho

user,

M.,

33-PD

L-1/F

D-5Fra

nko,

K., 2

02-CF

D-22

Frasso

ldati,

A., 2

44-CF

D-29

Frazz

a, L.,

58-C

FD-8

Frede

ricks

, W.,

19-AT

IO-4,

127

-ATIO

-13Fre

ret, L

., 97

-CFD-1

1Fre

sconi,

F., 9

0-APA

-12, 1

19-AF

M-8

Freun

d, J.,

78-A

A-12

Frew,

E., 1

57-AF

M-9,

273

-ASE-5

Fried

man,

A., 1

76-M

AO-5,

296

-APA-3

5Fri

edma

n, C.,

236

-APA-2

8Fri

schem

eier, S

., 11

7-ACD

-3Fu

chs,

M., 3

06-CF

D-36

Fuck

e, L.,

31-M

ST-2

Fujii,

K., 6

0-FD-6

/PDL

-2, 1

14-AA

-18, 1

30-CF

D-13,

1

69-CF

D-17

Fujin

o, T.,

286

-PDL-1

3Fu

jita, K

., 68

-TP-3,

69-T

P-4Fu

jiwara

, G.,

49-AP

A-7Fu

ller, C

., 22

6-AA-3

1Fu

nk, C

., 12

4-APA

-15Fu

rukaw

a, D.

, 89-A

PA-11

Gaba

rd, G

., 6-A

A-4, 7

8-AA-1

2, 1

13-AA

-17, 2

63-AA

-41Ga

bbert

, D.,

48-AP

A-6Ga

ddai,

A., 2

03-CF

D-23

Gaeta

, R.,

37-AA

-6, 2

31-AA

-36Ga

itond

e, D.

, 80-A

A-14,

174

-FD-20

, 205

-CFD-2

5,

245

-CFD-3

0, 2

66-AM

T-13/

GT-13

, 302

-CFD-3

2,

303

-CFD-3

3Ga

lbrait

h, M.

, 170

-CFD-1

8Ga

llman

, J.,

79-AA

-13Ga

llo, E

., 86

-AMT-6

/GT-6

Galye

n, N.

, 11-A

MT-2/

GT-2

Gamb

a, M.

, 102

-FD-13

Gamb

ardell

a, D.

, 104

-MAO

-3Ga

mblin

, R.,

200-B

AL-2

Gamb

oa, P

., 43

-AFM-

3, 1

04-M

AO-3

Gan,

J., 9

0-APA

-12Ga

napa

thisu

brama

ni, B

., 3-A

A-1, 3

8-AA-7

, 136

-FD-15

Gao,

D., 1

07-PD

L-4Ga

o, Z.,

161

-APA-1

8, 2

13-M

AO-7

Garci

a, D.

, 282

-LTA-2

Garci

a, E.,

239

-ATIO

-22Ga

rgiulo

, F.,

164-A

TIO-15

Garla

nd, M

., 14

2-MST

-6Ga

rman

, K.,

249-F

T-1Ga

rman

n, D.

, 208

-FD-23

, 302

-CFD-3

2Ga

rrard,

G.,

120-A

MT-7/

GT-7

Garre

tt, S

., 98

-CFD-1

2, 2

09-FD

-24Ga

rrick,

D., 2

43-CF

D-28

Gartn

er, J.

, 63-F

D-9Ga

ry, J.

, 167

-BAL-1

Gasb

arri, P

., 11

9-AFM

-8Ga

tian,

K., 5

2-ATIO

-6Ga

tlin, G

., 88

-APA-1

0Ga

uger,

N.,

79-AA

-13, 2

52-M

AO-9,

283

-MAO

-10Ga

uthier

, T.,

47-AP

A-5Ga

utier,

M.,

238-A

TIO-21

Gea-A

guile

ra, F.

, 112

-AA-16

Gebre

egzia

bher,

A., 4

2-ACD

-1Ge

der, J

., 48

-APA-6

, 233

-APA-2

5Ge

e, K.,

40-A

A-9Ge

isbau

er, S

., 10

5-MST

-5, 1

95-AP

A-23

Geisle

r, R.,

159-A

MT-10

/GT-1

0Ge

mma,

S., 2

9-MAO

-1

Genn

aretti,

M.,

162-A

PA-19

, 263

-AA-41

Georg

e, J.,

11-A

MT-2/

GT-2,

50-A

PA-8

Georg

iadis,

N.,

175-F

D-22

Gerbe

r, T.,

167-B

AL-1

Gerla

ch, T

., 17

7-MST

-7Ge

rman

, B.,

93-AT

IO-11

, 127

-ATIO

-13Ge

rn, F.

, 82-A

CD-2

Gerz,

T., 1

96-AS

E-2Ge

tsing

er, D

., 17

3-FD-1

9Ge

uther,

S.,

164-A

TIO-15

Geye

r, T.,

231-A

A-36

Geze

r, R.,

83-AF

M-5

Gherm

an, G

., 96

-CFD-1

0Gh

orawa

t, P.,

84-A

FM-6

Ghorb

anias

l, G.,

152-A

A-22

Ghore

yshi,

M.,

236-A

PA-28

, 305

-CFD-3

5Gh

osh,

A., 1

18-AF

M-7

Ghos

h, D.

, 163

-ASE-1

Ghos

h, S.

, 125

-APA-1

6, 2

13-M

AO-7

Giauq

ue, A

., 18

5-AA-2

6Gie

pman

, R.,

138-F

D-17

Gil Pr

ieto,

D., 2

70-AP

A-32

Gilde

rslee

ve, S

., 10

1-FD-1

2Gil

es, M

., 20

0-BAL

-2Gil

ge, P

., 23

5-APA

-27Gil

l, J., 1

12-AA

-16, 1

13-AA

-17, 1

52-AA

-22, 2

60-AA

-38Gil

lespie

, E.,

8-AFM

-1Gil

liam,

F., 6

4-MAO

-2Gil

more,

B.,

104-M

AO-3

Ginn,

S., 2

40-AT

IO-23

Giret,

J., 1

88-AA

-29Gir

imaji

, S.,

58-CF

D-8Gla

ab, P

., 14

2-MST

-6Gla

ss, C.

, 233

-APA-2

5Gle

gg, S

., 37

-AA-6,

38-A

A-7, 7

7-AA-1

1, 1

14-AA

-18,

187

-AA-28

, 261

-AA-39

Gloerf

elt, X

., 56

-CFD-6

, 62-F

D-8, 1

13-AA

-17 ,

154

-AA-24

, 226

-AA-31

Gloud

eman

s, J.,

82-A

CD-2

Gnoff

o, P.,

132

-CFD-1

5Go

blet,

V., 1

56-AC

D-4Gó

es, L

., 30

-MST

-1, 2

82-LT

A-2Go

ginen

i, S.,

266-A

MT-13

/GT-1

3Go

jon, R

., 4-A

A-2Go

kcen

, T.,

34-TP

-1, 1

08-TP

-5, 2

16-TP

-10/P

DL-10

Golas

zews

ki, R.

, 275

-ATIO

-25Go

ldberg

, U.,

245-C

FD-30

Golds

mith,

B.,

276-A

TIO-26

Golds

tein,

D., 2

88-TP

-13Go

li, N.

, 265

-ACD-7

Golub

ev, A

., 22

6-AA-3

1Go

lubev

, V.,

79-AA

-13

Gond

a, J.,

239

-ATIO

-22Go

ng, C

., 25

2-MAO

-9, 2

98-AT

IO-27

Gonz

alez,

D., 3

03-CF

D-33

Gonz

alez,

L., 1

01-FD

-12Go

nzale

z-Line

ro, L.

, 190

-ACD-5

Good

rich,

K., 9

3-ATIO

-11, 1

99-AT

IO-20

Gopa

larath

nam,

A., 2

35-AP

A-27,

267

-APA-2

9Go

paraj

u, K.,

205

-CFD-2

5Go

rdeye

v, S.

, 88-A

PA-10

, 143

-PDL-6

, 255

-PDL-1

2Go

rdnier

, R.,

62-FD

-8, 2

08-FD

-23Go

rham,

P., 2

00-BA

L-2Go

ri, G.

, 133

-CFD-1

6, 1

96-AS

E-2Go

ri, R.,

162

-APA-1

9Go

rrell,

S., 3

02-CF

D-32

Gorto

n, S.

, 281

-GEPC

-1Go

urina

t, Y.,

82-A

CD-2

Govin

daraj

an, R

., 28

-FD-4

Govin

daraj

u, P.,

82-A

CD-2

Goya

l, T.,

234-A

PA-26

Goyn

e, C.,

159

-AMT-1

0/GT

-10Gr

abe,

C., 6

1-FD-7

Grac

e, S.

, 264

-AA-42

Grah

am, R

., 51

-ATIO

-5Gr

amaty

ka, J

., 30

8-MAO

-13Gr

anlun

d, K.,

63-F

D-9, 1

75-FD

-22Gr

ant,

J., 3

7-AA-6

Gran

t, M.

, 44-A

FM-4,

83-A

FM-5

Gras

so, F

., 98

-CFD-1

2Gr

asso

, G.,

112-A

A-16

Grau

be, P

., 10

8-TP-5

Grau

er, J.

, 118

-AFM-

7Gr

een,

C., 2

40-AT

IO-23

Gree

n, M.

, 26-F

D-2Gr

eenb

latt,

D., 1

01-FD

-12, 1

58-AM

T-9/G

T-9, 2

08-FD

-23Gr

eend

yke,

R., 3

4-TP-1

Gree

ne, B

., 33

-PDL-1

/FD-5

Gree

ne, G

., 23

7-ASE

-3Gr

eene

, K.,

43-AF

M-3

Greg

ory, J

., 33

-PDL-1

/FD-5

, 268

-APA-3

0Gr

enon

, R.,

13-AP

A-2Gr

iffiths

, P.,

209-F

D-24

Grim

m, F.

, 185

-AA-26

Grim

men,

J., 3

05-CF

D-35

Grim

sley,

J., 1

40-IT

AR-2

Grins

tead,

J., 6

9-TP-4

Grive

l, A.,

46-AM

T-4/G

T-4Gr

oss,

A., 2

08-FD

-23Gr

oss,

R., 9

9-FD-1

0Gr

oth, C

., 97

-CFD-1

1, 1

71-CF

D-19,

304

-CFD-3

4Gr

ound

, C.,

86-AM

T-6/G

T-6Gr

und,

T., 1

25-AP

A-16

Gu, L

., 25

2-MAO

-9

124

Auth

or/S

essio

n Ch

air In

dex

Gu, Q

., 26

5-ACD

-7Gu

, Y.,

43-AF

M-3

Guan

, Y.,

38-AA

-7Gu

ardon

e, A.,

26-F

D-2, 1

33-CF

D-16,

196

-ASE-2

Guen

ther, C

., 30

5-CFD

-35Gu

erin,

S., 4

1-AA-1

0, 7

7-AA-1

1Gu

erreir

o, N.

, 17-A

TIO-2

Guerr

i, O.,

305-C

FD-35

Gugli

elmo,

J., 2

35-AP

A-27

Gumi

nsky

, M.,

142-M

ST-6,

299

-ATIO

-28Gu

o, C.,

84-A

FM-6

Guo,

J., 1

64-AT

IO-15

Guo,

Y., 1

12-AA

-16, 1

16-AA

-20Gu

pta, A

., 97

-CFD-1

1, 2

68-AP

A-30

Gupta

, M.,

38-AA

-7Gu

pte, A

., 57

-CFD-7

Gursu

l, I.,

25-FD

-1, 1

38-FD

-17Gu

tmark

, E.,

153-A

A-23

Guyn

n, M.

, 293

-ACD-8

Guyto

n, R.,

85-A

MT-5/

GT-5

Guze

l, G.,

304-C

FD-34

Haba

shi, W

., 19

6-ASE

-2Ha

bbit,

R., 9

6-CFD

-10Ha

eri, S

., 26

1-AA-3

9Ha

fez, M

., 10

5-MST

-5, 2

78-FD

-30Ha

ga, T

., 13

0-CFD

-13Ha

gen,

G., 1

7-ATIO

-2Ha

hn, M

., 29

-MAO

-1Ha

imes

, R.,

302-C

FD-32

Haina

ut, T.

, 6-AA

-4Ha

ji-She

ikh, A

., 35

-TP-2

Hajia

n, R.,

25-F

D-1Ha

jj, M.

, 236

-APA-2

8Ha

le, L.

, 30-M

ST-1

Hall,

D., 6

4-MAO

-2Ha

ll, J.,

283

-MAO

-10Ha

llock

, J.,

237-A

SE-3

Halls,

B.,

86-AM

T-6/G

T-6Ha

m, F.

, 202

-CFD-2

2Ha

mane

, D.,

305-C

FD-35

Hami

che,

K., 2

63-AA

-41Ha

mmac

k, S.

, 107

-PDL-4

Hamm

ock,

G., 1

58-AM

T-9/G

T-9, 1

91-AM

T-11/

GT-11

Han,

K., 1

98-AT

IO-19

Han,

X., 1

44-PD

L-7Ha

nnem

ann,

K., 3

02-CF

D-32

Hanq

uist,

K., 3

5-TP-2

Hans

es, C

., 51

-ATIO

-5Ha

nsma

n, R.,

156

-ACD-4

Harad

a, N.

, 181

-PDL-9

/TP-8

Harih

aran,

N., 1

22-AP

A-13

Harik

, R.,

64-M

AO-2

Harke

r, B.,

40-AA

-9Ha

rringto

n, A.,

136

-FD-15

Harris

, R., 4

1-AA-1

0, 81

-AA-15

, 195

-APA-2

3, 24

1-CFD

-26Ha

rrison

, E.,

156-A

CD-4

Harsh

e, S.

, 235

-APA-2

7Ha

rtfield

, R.,

127-A

TIO-13

, 161

-APA-1

8Ha

rtwich

, P.,

87-AP

A-9, 1

33-CF

D-16

Hasa

n, S.

, 65-M

ST-3,

142

-MST

-6, 1

97-AT

IO-18

, 2

75-AT

IO-25

Hash

, D.,

288-T

P-13

Hash

emi, A

., 68

-TP-3

Hash

emi, K

., 9-A

FM-2

Hask

in, H

., 15

8-AMT

-9/GT

-9Ha

snain

, Z.,

12-AP

A-1, 5

0-APA

-8Ha

ssan,

M., 3

7-AA-6

, 42-A

CD-1,

53-AT

IO-7,

239-A

TIO-22

Hassa

n, W.

, 15-A

PA-4

Hatha

way,

J., 1

96-AS

E-2Ha

ttenb

erger,

G.,

161-A

PA-18

Haxte

r, S.,

260-A

A-38

Hay,

A., 5

8-CFD

-8, 2

04-CF

D-24,

304

-CFD-3

4Ha

yash

ibara,

S.,

27-FD

-3Ha

yden

, T.,

88-AP

A-10,

143

-PDL-6

, 255

-PDL-1

2Ha

ys, T

., 15

7-AFM

-9Ha

ywoo

d, J.,

24-C

FD-4

Hazir

, A.,

188-A

A-29

He, A

., 27

2-ASE

-4He

, C.,

280-F

T-2/G

T-14

Hebe

rt, P.

, 85-A

MT-5/

GT-5

Hedri

ck, T

., 10

0-FD-1

1He

eg, J

., 12

4-APA

-15He

fferno

n, T.,

259

-AA-37

Hegd

e, A.,

174

-FD-20

Hege

n, S.

, 13-A

PA-2

Heine

ck, J

., 19

2-AMT

-12/G

T-12

Heinr

ich, R

., 57

-CFD-7

Heise

r, W.,

15-AP

A-4He

itmeir

, F.,

151-A

A-21

Helbe

r, B.,

108-T

P-5He

lm, S

., 91

-ATIO

-9He

mpley

, L.,

165-A

TIO-16

, 199

-ATIO

-20He

nders

on, B

., 22

7-AA-3

2He

nders

on, R

., 13

7-FD-1

6He

nfling

, J.,

62-FD

-8, 1

75-FD

-22He

nry de

Frah

an, M

., 20

1-CFD

-21He

rbst,

S., 8

8-APA

-10, 2

53-M

ST-11

Heret

h, L.,

15-A

PA-4

Herol

d, G.

, 186

-AA-27

, 231

-AA-36

Herr,

M., 1

15-AA

-19, 1

55-AA

-25, 2

26-AA

-31, 2

30-AA

-35He

rrema

, F.,

51-AT

IO-5

Herrin

g, A.,

158

-AMT-9

/GT-9

Herrm

ann,

J., 2

9-MAO

-1He

rron,

A., 2

62-AA

-40

Herzo

g, S.

, 252

-MAO

-9He

ss, C.

, 11-A

MT-2/

GT-2

Hicke

l, S.,

87-AP

A-9Hic

ken,

J., 1

76-M

AO-5,

212

-MAO

-6, 2

42-CF

D-27,

2

51-M

AO-8

Hieple

r, `.,

302-C

FD-32

Higdo

n, K.,

288

-TP-13

High,

J., 1

65-AT

IO-16

Higue

ra Ca

ubilla

, D.,

58-CF

D-8Hil

debra

nd, N

., 4-A

A-2Hin

er, W

., 79

-AA-13

Hinze

, N.,

300-A

TIO-29

Hipp,

K., 5

0-APA

-8Hir

amoto

, R.,

293-A

CD-8

Hiray

ama,

T., 6

6-MST

-4Hit

zel, S

., 16

0-APA

-17Hix

on, D

., 6-A

A-4, 7

8-AA-1

2, 8

1-AA-1

5, 1

54-AA

-24,

229

-AA-34

Hoell

ing, M

., 50

-APA-8

Hoffle

r, K.,

43-AF

M-3

Hoffm

an, R

., 14

2-MST

-6Ho

ffman

n, K.,

175

-FD-22

Höge

r, M.,

151-A

A-21

Holla

day,

W., 8

5-AMT

-5/GT

-5Ho

lland

, K.,

186-A

A-27

Holla

nd, M

., 11

7-ACD

-3Hö

lling,

M., 2

71-AP

A-33

Hollin

gswo

rth, P

., 30

-MST

-1, 5

3-ATIO

-7Ho

lst, T

., 13

6-FD-1

5Ho

lzäpfe

l, F.,

196-A

SE-2,

237

-ASE-3

Hong

, S.,

51-AT

IO-5,

166

-ATIO

-17Ho

ng, Z

., 10

7-PDL

-4Ho

nnery

, D.,

153-A

A-23

Hoog

reef,

M., 4

2-ACD

-1, 1

76-M

AO-5

Hopf,

J., 1

91-AM

T-11/

GT-11

Horch

ler, T

., 30

2-CFD

-32Ho

rio, B

., 65

-MST

-3, 1

42-M

ST-6

Horkh

eimer,

D.,

282-L

TA-2

Horn,

J., 4

3-AFM

-3, 8

3-AFM

-5Ho

rne, W

., 18

6-AA-2

7, 2

62-AA

-40Ho

rnung

, M.,

88-AP

A-10,

91-A

TIO-9,

253

-MST

-11Ho

sang

adi, P

., 23

5-APA

-27Ho

sder,

S.,

58-CF

D-8Ho

sseinv

erdi, S

., 10

0-FD-1

1Ho

usma

n, J.,

4-AA

-2, 1

4-APA

-3, 4

9-APA

-7Ho

ward,

M.,

68-TP

-3Ho

werto

n, B.

, 7-AA

-5, 1

16-AA

-20Hu

, F.,

229-A

A-34

Hu, H

., 18

0-PDL

-8/AP

A-20

Hu, J

., 17

1-CFD

-19Hu

, Y.,

208-F

D-23

Hu, Z

., 22

-CFD-2

, 205

-CFD-2

5

Hua,

J., 3

5-TP-2

Huan

g, G.

, 159

-AMT-1

0/GT

-10, 1

62-AP

A-19,

2

67-AP

A-29,

270

-APA-3

2Hu

ang,

X., 7

-AA-5,

26-F

D-2, 7

8-AA-1

2, 1

13-AA

-17Hu

ang,

Z., 9

9-FD-1

0Hu

bbard

, E.,

191-A

MT-11

/GT-1

1Hu

bbard

, J.,

12-AP

A-1, 5

0-APA

-8Hu

ber, J

., 18

9-AA-3

0Hu

e, D.

, 13-A

PA-2

Hueh

ne, C

., 12

5-APA

-16Hu

et, M

., 18

5-AA-2

6Hu

ff, B

., 12

8-ATIO

-14Hu

fnage

l, K.,

271-A

PA-33

Hug,

S., 2

4-CFD

-4Hu

ghes

, M.,

196-A

SE-2

Hui, F

., 10

8-TP-5

Hulsh

off, S

., 33

-PDL-1

/FD-5

Hultg

ren, L

., 15

1-AA-2

1Hu

mpert

, B.,

37-AA

-6Hu

mphre

ys, C

., 14

1-MAO

-4Hu

mphre

ys, W

., 18

8-AA-2

9Hu

r, J.,

124-A

PA-15

Husse

in, A.

, 236

-APA-2

8Hu

ssein,

S.,

246-F

D-27

Hutch

eson

, F.,

4-AA-2

, 158

-AMT-9

/GT-9

Huyn

h, H.

, 55-C

FD-5,

130

-CFD-1

3, 1

70-CF

D-18,

2

42-CF

D-27

Hwan

g, I.,

31-M

ST-2,

126

-ATIO

-12Hw

ang,

J., 2

9-MAO

-1, 3

07-M

AO-12

Idier,

A., 3

-AA-1

Idris,

H.,

16-AT

IO-1,

275

-ATIO

-25Ihm

e, M.

, 151

-AA-21

, 242

-CFD-2

7Ike

da, T

., 15

5-AA-2

5Im

, D.,

12-AP

A-1, 1

32-CF

D-15

Imam

ura, T

., 15

5-AA-2

5, 2

41-CF

D-26

Imlay

, S.,

301-C

FD-31

Ims,

J., 2

3-CFD

-3Im

tiaz,

H., 1

33-CF

D-16

Ingrah

am, D

., 6-A

A-4Iop

polo,

T., 4

6-AMT

-4/GT

-4Ior

io, M

., 10

1-FD-1

2Ish

ida, Y

., 68

-TP-3

Ishiok

a, H.

, 270

-APA-3

2Ish

utkina

, M.,

298-A

TIO-27

Isikv

eren,

A., 5

3-ATIO

-7Ita

sse, M

., 22

8-AA-3

3Ito

, H.,

23-CF

D-3Ito

, K.,

66-M

ST-4

Ito, Y

., 23

0-AA-3

5Iva

ldi, D

., 30

7-MAO

-12Iva

nov,

V., 2

43-CF

D-28

Iwak

awa,

A., 8

9-APA

-11, 1

38-FD

-17

Jack

, D.,

43-AF

M-3

Jack

son,

G., 1

45-TP

-7Ja

ckso

n, R.,

138

-FD-17

Jack

son,

T., 2

03-CF

D-23

Jaco

b, D.

, 237

-ASE-3

, 272

-ASE-4

Jaco

b, J.,

37-A

A-6, 4

8-APA

-6, 1

40-IT

AR-2,

196

-ASE-2

, 2

31-AA

-36, 2

74-AT

IO-24

, 280

-FT-2/

GT-14

Jaco

bi, R.

, 100

-FD-11

Jaco

bs, S

., 10

7-PDL

-4Ja

cque

s, D.

, 141

-MAO

-4Ja

ffrez

ic, B

., 17

8-MST

-8Ja

in, N

., 17

1-CFD

-19Ja

lali, A

., 21

-CFD-1

Jamb

unath

an, R

., 20

3-CFD

-23Ja

mes,

M., 4

0-AA-9

Jame

son,

A., 5

5-CFD

-5, 1

23-AP

A-14,

132

-CFD-1

5,

271

-APA-3

3Ja

njic,

Z., 1

63-AS

E-1Ja

nn, T

., 10

5-MST

-5Ja

ouan

i, N.,

187-A

A-28

Jaron

, R.,

77-AA

-11Ja

rzemb

ski, A

., 25

0-LTA

-1Ja

strze

bski,

M.,

17-AT

IO-2

Jaun

et, V.

, 80-A

A-14,

189

-AA-30

Jawo

rski, J

., 25

-FD-1,

38-A

A-7Je

nkins

, L.,

188-A

A-29,

192

-AMT-1

2/GT

-12Je

nkins

, T.,

11-AM

T-2/G

T-2, 1

59-AM

T-10/

GT-10

Jens

en, L

., 15

6-ACD

-4Je

ssberg

er, C.

, 52-A

TIO-6

Jesu

s, A.,

98-C

FD-12

Jewe

ll, J.,

28-F

D-4Ji,

C., 1

16-AA

-20Ji,

L., 1

51-AA

-21Jia

nchu

n, X.

, 215

-MST

-10Jia

ng, C

., 18

0-PDL

-8/AP

A-20

Jiang

, H.,

78-AA

-12Jia

ng, N

., 86

-AMT-6

/GT-6

Jiang

, Z.,

22-CF

D-2Jia

o, J.,

263

-AA-41

Jie, B

., 25

3-MST

-11Jim

enez

, H.,

52-AT

IO-6,

156

-ACD-4

, 293

-ACD-8

Jin, J

., 85

-AMT-5

/GT-5

Jin, W

., 85

-AMT-5

/GT-5

Jing,

C., 2

52-M

AO-9

Jinwu

, X.,

214-M

ST-9

Jiras

ek, A

., 16

0-APA

-17, 3

05-CF

D-35

Jo, Y

., 25

1-MAO

-8Jo

hans

en, C

., 12

1-AMT

-8/FD

-14/T

P-6/G

T-8,

159

-AMT-1

0/GT

-10Jo

hnse

n, E.,

201

-CFD-2

1, 2

11-FD

-26Jo

hnso

n, H.

, 103

-ITAR

-1Jo

hnso

n, S.

, 43-A

FM-3,

214

-MST

-9

125

Auth

or/S

essio

n Ch

air In

dex

John

ston,

C., 6

9-TP-4

, 217

-TP-11

Jolly,

B.,

23-CF

D-3, 1

36-FD

-15, 2

41-CF

D-26

Jond

eau,

E., 2

31-AA

-36Jo

nes,

A., 2

68-AP

A-30

Jone

s, G.

, 294

-AMT-1

4/GT

-15Jo

nes,

J., 2

28-AA

-33Jo

nes,

M., 7

-AA-5,

26-F

D-2, 1

16-AA

-20, 2

62-AA

-40,

302

-CFD-3

2Jo

nes,

S., 8

6-AMT

-6/GT

-6Jo

nes,

W., 3

01-CF

D-31

Joo,

J., 1

91-AM

T-11/

GT-11

Jorda

n, P.,

5-AA

-3, 8

0-AA-1

4, 1

89-AA

-30Jo

rris, T

., 24

9-FT-1

Jose

ph, L

., 29

5-APA

-34Jo

seph

, P.,

3-AA-1

, 7-AA

-5, 3

8-AA-7

, 79-A

A-13,

1

52-AA

-22, 2

61-AA

-39Jo

st, A.

, 203

-CFD-2

3Jo

syula

, E.,

69-TP

-4Jo

yce,

R., 3

1-MST

-2Ju

liano

, T.,

10-AM

T-1/G

T-1, 1

37-FD

-16Ju

mper,

E., 8

8-APA

-10, 1

43-PD

L-6, 2

55-PD

L-12

June

, J.,

262-A

A-40

Jung

, K.,

235-A

PA-27

Jung

, S.,

166-A

TIO-17

Jung

, T.,

64-M

AO-2

Jung

, Y.,

16-AT

IO-1,

91-A

TIO-9,

198

-ATIO

-19,

298

-ATIO

-27Ju

nkui,

M.,

45-AM

T-3/G

T-3, 2

85-M

ST-12

Junq

ueira

-Junio

r, C.,

270-A

PA-32

Jurko

vich,

M., 1

93-AP

A-21,

269

-APA-3

1Ju

stin,

C., 1

90-AC

D-5Ju

ve, D

., 18

9-AA-3

0, 2

31-AA

-36Ka

ddou

h, B.

, 30-M

ST-1

Kaila

sana

th, K.

, 153

-AA-23

Kaliv

arapu

, V.,

29-M

AO-1,

104

-MAO

-3, 2

83-M

AO-10

Kalkh

oran,

I., 2

33-AP

A-25

Kalya

n, A.,

228

-AA-33

Kama

li, S.

, 122

-APA-1

3Ka

mat,

S., 2

93-AC

D-8Ka

mle,

S., 2

34-AP

A-26

Kamm

eyer,

M.,

294-A

MT-14

/GT-1

5Ka

mpers

, G.,

50-AP

A-8, 2

71-AP

A-33

Kamr

uzza

man,

M., 1

55-AA

-25Ka

ng, H

., 16

2-APA

-19Ka

nistra

s, K.,

88-A

PA-10

Kann

an, H

., 21

2-MAO

-6Ka

noria

, A.,

250-L

TA-1,

305

-CFD-3

5Ka

pania

, R.,

29-M

AO-1

Kara,

K., 1

3-APA

-2, 5

0-APA

-8, 2

36-AP

A-28

Karab

asov

, S.,

5-AA-3

, 6-AA

-4, 8

0-AA-1

4, 2

28-AA

-33Ka

rahan

, S.,

294-A

MT-14

/GT-1

5Ka

rakoc

, T.,

273-A

SE-5

Karak

oç, N

., 27

3-ASE

-5Ka

rlgaa

rd, C.

, 44-A

FM-4

Karon

, A.,

189-A

A-30

Karth

a, A.,

244

-CFD-2

9Ka

se, S

., 29

3-ACD

-8Ka

sprzy

k, M.

, 280

-FT-2/

GT-14

Kato,

H.,

60-FD

-6/PD

L-2, 1

92-AM

T-12/

GT-12

Katsu

rayam

a, H.

, 286

-PDL-1

3Ka

tz, A.

, 21-C

FD-1,

243

-CFD-2

8Ka

tz, J.

, 88-A

PA-10

Kaul,

U.,

25-FD

-1, 4

9-APA

-7, 2

79-FD

-31Ka

usch

e, P.,

152

-AA-22

Kaya

, D.,

118-A

FM-7

Ke, G

., 26

1-AA-3

9Ke

geris

e, M.

, 99-F

D-10

Kelle

r, D.,

87-AP

A-9Ke

ller, E

., 83

-AFM-

5Ke

lly, M

., 26

9-APA

-31Ke

nned

y, G.

, 212

-MAO

-6Ke

nway

, G.,

141-M

AO-4

Kerho

, M.,

235-A

PA-27

Kessl

er, R.

, 22-C

FD-2,

96-C

FD-10

Key,

N., 1

58-AM

T-9/G

T-9, 1

73-FD

-19Ke

ye, S

., 87

-APA-9

Khali

d, M.

, 136

-FD-15

Khali

l, E.,

145-T

P-7, 1

78-M

ST-8

Kham

is, D

., 7-A

A-5Kh

an, S

., 66

-MST

-4Kh

ire, R

., 14

1-MAO

-4Kh

odad

oust,

A., 2

02-CF

D-22

Khoo

, B.,

235-A

PA-27

Khorr

ami, M

., 15

5-AA-2

5, 1

88-AA

-29, 2

59-AA

-37Kid

d, F.,

143

-PDL-6

Kim, C

., 24

2-CFD

-27Kim

, E.,

51-AT

IO-5

Kim, H

., 88

-APA-1

0Kim

, J., 3

-AA-1,

46-AM

T-4/G

T-4, 1

51-AA

-21, 2

61-AA

-39Kim

, K.,

126-A

TIO-12

Kim, T

., 46

-AMT-4

/GT-4

Kim, V

., 14

1-MAO

-4Kim

, Y.,

142-M

ST-6

Kimme

l, R.,

28-FD

-4, 1

02-FD

-13, 1

03-IT

AR-1

King,

L., 1

61-AP

A-18

King,

R., 9

9-FD-1

0, 1

37-FD

-16Kin

g, W.

, 250

-LTA-1

Kinga

n, M.

, 5-AA

-3, 3

7-AA-6

Kings

, N.,

41-AA

-10, 1

51-AA

-21Kio

, M.,

35-TP

-2Kir

by, A

., 20

1-CFD

-21Kir

by, M

., 19

8-ATIO

-19Kir

is, C.

, 4-AA

-2, 1

4-APA

-3Kir

k, C.,

159

-AMT-1

0/GT

-10

Kirk,

L., 6

9-TP-4

Kiyici,

F., 2

04-CF

D-24

Klabe

s, A.,

226

-AA-31

Kleb,

W., 5

8-CFD

-8, 2

33-AP

A-25

Kleinc

laus,

C., 2

59-AA

-37Kle

ine, H

., 10

2-FD-1

3Kle

ntzma

n, J.,

99-F

D-10

Kline

, H.,

204-C

FD-24

Kling

, U.,

53-AT

IO-7

Klock

, R.,

119-A

FM-8

Kloke

r, M.,

209-F

D-24

Knab

e, F.,

51-A

TIO-5

Knob

loch,

K., 1

51-AA

-21Kn

owles

, J.,

105-M

ST-5

Koc,

I., 3

04-CF

D-34

Koch

, J.,

236-A

PA-28

Koch

, M.,

238-A

TIO-21

Kocia

n, T.,

137

-FD-16

Koda

ma, H

., 15

2-AA-2

2Ko

enig,

M.,

4-AA-2

Koern

er, S

., 23

7-ASE

-3Ko

h, S.

, 38-A

A-7, 4

1-AA-1

0, 7

9-AA-1

3, 8

0-AA-1

4Ko

ike, S

., 19

2-AMT

-12/G

T-12

Koizu

mi, H

., 23

-CFD-3

Kok,

F., 2

7-FD-3

, 175

-FD-22

Koka

ly, M

., 17

8-MST

-8Ko

klu, M

., 63

-FD-9

Kolon

ay, R

., 29

-MAO

-1, 2

52-M

AO-9,

284

-MAO

-11Ko

matsu

, P.,

307-M

AO-12

Kong

, W.,

295-A

PA-34

Konn

eman

n, E.,

275

-ATIO

-25Ko

ntis,

K., 1

93-AP

A-21

Koo,

H., 3

04-CF

D-34

Kopie

v, V.,

187

-AA-28

, 189

-AA-30

, 228

-AA-33

Kopy

t, A.,

30-M

ST-1

Korea

nsch

i, A.,

13-AP

A-2, 2

96-AP

A-35

Korki

s-Kan

aan,

R., 3

05-CF

D-35

Korn,

B.,

51-AT

IO-5

Korol

ev, Y

., 5-A

A-3, 2

51-M

AO-8

Kosti

uk, P

., 14

2-MST

-6Kö

the, T

., 25

2-MAO

-9Ko

tikalp

udi, A

., 15

7-AFM

-9Ko

tov, D

., 24

-CFD-4

Kotov

, M.,

193-A

PA-21

Kotso

nis, M

., 88

-APA-1

0, 2

86-PD

L-13

Kozie

l, S.,

307-M

AO-12

Kozlo

v, A.,

77-A

A-11

Krako

s, J.,

23-C

FD-3

Kraus

man,

J., 2

82-LT

A-2Kra

ut, J.

, 51-A

TIO-5

Kreitz

man,

J., 1

53-AA

-23Kre

uz, M

., 16

4-ATIO

-15

Krimm

elbein

, N.,

61-FD

-7Kri

shna

, Y.,

11-AM

T-2/G

T-2Kri

shna

moort

hy, S

., 28

6-PDL

-13Kri

shna

murth

y, R.,

272

-ASE-4

Kroeb

er, S

., 26

0-AA-3

8Kro

nhau

s, I.,

144

-PDL-7

Kronin

ger, C

., 13

6-FD-1

5Kro

o, I.,

8-AF

M-1,

249

-FT-1

Kroze

l, J.,

142-M

ST-6

Krueg

er, P.

, 62-F

D-8Kru

eger,

W.,

198-A

TIO-19

Krüge

r, W.,

57-CF

D-7, 1

05-M

ST-5

Krumb

ein, A

., 61

-FD-7

Krumm

e, A.,

13-A

PA-2

Krus,

P., 2

83-M

AO-10

Kryu

kov,

I., 1

93-AP

A-21

Kucu

kcos

kun,

K., 7

9-AA-1

3Kü

gler, M

., 12

8-ATIO

-14Ku

hn, T

., 88

-APA-1

0Ku

lkarni

, M.,

252-M

AO-9

Kuma

r, D.,

234-A

PA-26

Kuma

r, R.,

118-A

FM-7,

174

-FD-20

Kuma

r, S.,

234-A

PA-26

Kuma

r, V.,

65-M

ST-3,

142

-MST

-6Ku

ntz, D

., 34

-TP-1

Kunz

, D.,

43-AF

M-3

Kuo,

C., 1

53-AA

-23Ku

relek

, J.,

100-F

D-11

Kurtz

, J.,

46-AM

T-4/G

T-4Ku

rz, H

., 20

9-FD-2

4Ku

tay, A

., 66

-MST

-4, 8

3-AFM

-5, 1

18-AF

M-7,

2

94-AM

T-14/

GT-15

Kutz,

D.,

158-A

MT-9/

GT-9

Kwon

, O.,

133-C

FD-16

La Ro

cca, G

., 17

6-MAO

-5La

caze

, G.,

244-C

FD-29

Lach

enme

ier, T

., 16

7-BAL

-1La

chow

ski, F

., 37

-AA-6

Laco

r, C.,

152-A

A-22

Lacy,

D.,

87-AP

A-9La

fage,

R., 4

2-ACD

-1La

ffay,

P., 3

-AA-1

Laffe

rty, J

., 10

3-ITA

R-1La

i, D.,

237-A

SE-3,

272

-ASE-4

Lajús

, F.,

5-AA-3

, 80-A

A-14

Lam,

T., 2

17-TP

-11La

mbert

, A.,

100-F

D-11

Lamm

el, O

., 26

6-AMT

-13/G

T-13

Lamp

inen,

M., 1

39-FD

-18La

ncas

ter, J

., 15

8-AMT

-9/GT

-9La

ndma

n, D.

, 294

-AMT-1

4/GT

-15La

ndrum

, B.,

30-M

ST-1,

265

-ACD-7

Land

rum, D

., 25

0-LTA

-1La

ndry,

R., 2

15-M

ST-10

Land

ry, S

., 16

4-ATIO

-15, 1

66-AT

IO-17

, 197

-ATIO

-18La

ng, S

., 20

0-BAL

-2La

ngtry

, R.,

61-FD

-7La

rbi, S

., 30

5-CFD

-35La

rchev

eque

, L.,

154-A

A-24

Latz,

J., 1

61-AP

A-18,

267

-APA-2

9La

urend

eau,

F., 6

0-FD-6

/PDL

-2La

val, J

., 98

-CFD-1

2La

vin, T

., 11

9-AFM

-8La

wren

ce, J

., 5-A

A-3, 2

27-AA

-32La

zarus

, S.,

117-A

CD-3

Le B

ras, S

., 22

9-AA-3

4Le

Garr

ec, T

., 18

7-AA-2

8Le

Rallic

, M.,

80-AA

-14Le

bofsk

y, S.

, 124

-APA-1

5Le

brun,

F., 4

6-AMT

-4/GT

-4Le

e, D.

, 12-A

PA-1

Lee,

H., 1

6-ATIO

-1Le

e, K.,

51-AT

IO-5,

84-AF

M-6,

162-A

PA-19

, 166

-ATIO-

17Le

e, S.

, 154

-AA-24

Lee,

T., 1

07-PD

L-4Le

fantzi

, S.,

139-F

D-18

Lege

r, T.,

306-C

FD-36

Leib,

S.,

79-AA

-13, 2

27-AA

-32Le

ifsso

n, L.,

307

-MAO

-12Le

le, S

., 80

-AA-14

Lemo

nds,

T., 2

93-AC

D-8Le

ng, M

., 35

-TP-2,

145

-TP-7

Léon

, O.,

60-FD

-6/PD

L-2, 2

28-AA

-33Le

ong,

C., 6

3-FD-9

, 101

-FD-12

Leon

ov, S

., 10

7-PDL

-4, 1

44-PD

L-7Le

opold

, F.,

45-AM

T-3/G

T-3Le

sieutr

e, D.

, 269

-APA-3

1Le

trenn

e, G.

, 167

-BAL-1

Leun

g, R.,

38-A

A-7Le

vin, D

., 69

-TP-4,

203

-CFD-2

3Le

Vine,

M., 4

2-ACD

-1, 5

2-ATIO

-6, 1

98-AT

IO-19

Lewi

s, D.

, 103

-ITAR

-1Le

wis,

M., 1

0-AMT

-1/GT

-1, 3

03-CF

D-33

Lewi

s, R.,

108

-TP-5

Lewi

s, S.

, 34-T

P-1Le

wis,

T., 1

7-ATIO

-2Le

yva,

I., 2

7-FD-3

Li, F.

, 9-AF

M-2,

99-F

D-10,

137

-FD-16

Li, G

., 29

6-APA

-35Li,

H.,

144-P

DL-7,

180

-PDL-8

/APA

-20, 2

71-AP

A-33

Li, J.

, 24-C

FD-4,

92-A

TIO-10

Li, M

., 21

4-MST

-9Li,

S.,

26-FD

-2, 1

16-AA

-20Li,

V., 2

9-MAO

-1, 1

76-M

AO-5

126

Auth

or/S

essio

n Ch

air In

dex

Li, W

., 89

-APA-1

1, 2

41-CF

D-26,

261

-AA-39

Li, X

., 81

-AA-15

, 112

-AA-16

, 116

-AA-20

Li, Z.

, 69-T

P-4, 1

78-M

ST-8

Liang

, C.,

308-M

AO-13

Libsig

, M.,

47-AP

A-5Lib

urdy,

J., 2

34-AP

A-26

Liebe

ck, R

., 12

3-APA

-14Lil

lard,

R., 6

9-TP-4

, 172

-CFD-2

0Lil

ler, T

., 15

-APA-4

Lim, C

., 26

5-ACD

-7Lim

, D.,

42-AC

D-1, 1

90-AC

D-5Lim

bach

, C.,

60-FD

-6/PD

L-2Lin

, H.,

265-A

CD-7

Lin, J

., 13

8-FD-1

7, 2

12-M

AO-6

Lin, P

., 20

2-CFD

-22Lin

, Q.,

241-C

FD-26

Lin, Y

., 46

-AMT-4

/GT-4

, 65-M

ST-3,

240

-ATIO

-23Lin

coln,

D.,

159-A

MT-10

/GT-1

0Lin

dsay

, K.,

238-A

TIO-21

Linke

, F.,

92-AT

IO-10

Liou,

M., 5

6-CFD

-6Lip

pert,

M.,

88-AP

A-10

Liston

, G.,

10-AM

T-1/G

T-1Lit

tle, J

., 60

-FD-6/

PDL-2

, 174

-FD-20

, 175

-FD-22

, 2

79-FD

-31Liu

, A.,

128-A

TIO-14

Liu, C

., 30

5-CFD

-35Liu

, D.,

85-AM

T-5/G

T-5Liu

, F., 3

3-PDL

-1/FD

-5, 45

-AMT-3

/GT-3

, 67-P

DL-3,

1

44-PD

L-7, 1

80-PD

L-8/A

PA-20

, 271

-APA-3

3,

285

-MST

-12Liu

, G.,

248-F

D-29

Liu, H

., 29

5-APA

-34Liu

, J.,

30-M

ST-1,

84-A

FM-6,

153

-AA-23

, 251

-MAO

-8Liu

, L.,

25-FD

-1, 3

1-MST

-2, 2

13-M

AO-7,

251

-MAO

-8Liu

, P.,

26-FD

-2, 4

7-APA

-5Liu

, Q.,

178-M

ST-8

Liu, R

., 12

8-ATIO

-14Liu

, S.,

173-F

D-19

Liu, T

., 25

-FD-1

Liu, X

., 3-A

A-1, 5

5-CFD

-5, 7

8-AA-1

2, 1

13-AA

-17Liu

, Y.,

49-AP

A-7, 1

85-AA

-26, 2

85-M

ST-12

Liu, Z

., 57

-CFD-7

, 141

-MAO

-4Liv

, A.,

18-AT

IO-3

Liveb

ardon

, T.,

185-A

A-26

Livne

, E.,

49-AP

A-7Llo

pis-Pa

scual,

A., 2

71-AP

A-33

Lo, K

., 19

3-APA

-21Lo

aec,

S., 2

72-AS

E-4Lo

bel, G

., 22

7-AA-3

2Lo

ckard

, D.,

3-AA-1

, 155

-AA-25

, 188

-AA-29

, 2

30-AA

-35, 2

59-AA

-37

Lofth

ouse

, A.,

160-A

PA-17

, 236

-APA-2

8, 3

05-CF

D-35

Loga

n, M.

, 190

-ACD-5

Lohr,

G.,

91-AT

IO-9

Lomb

ardi, A

., 21

3-MAO

-7Lo

ng, D

., 27

5-ATIO

-25Lo

ng, T

., 21

3-MAO

-7, 2

51-M

AO-8

Lope

s, L.,

112

-AA-16

, 155

-AA-25

Lópe

z, I.,

281

-GEPC

-1Ló

pez-M

orales

, M.,

55-CF

D-5Lo

seille

, A.,

23-CF

D-3, 1

14-AA

-18Lo

th, S

., 91

-ATIO

-9Lo

u, F.,

158

-AMT-9

/GT-9

Loum

an, R

., 13

8-FD-1

7Lo

we, K

., 46

-AMT-4

/GT-4

, 159

-AMT-1

0/GT

-10,

192

-AMT-1

2/GT

-12, 2

66-AM

T-13/

GT-13

Lowe

nberg

, M.,

122-A

PA-13

Loza

no, B

., 15

6-ACD

-4Lu

, F.,

246-F

D-27,

279

-FD-31

Lu, J

., 28

5-MST

-12Lu

ckne

r, R.,

237-A

SE-3

Luck

ring,

J., 1

60-AP

A-17

Ludw

ig, B

., 15

9-AMT

-10/G

T-10

Lued

ke, J

., 29

7-APA

-37Lu

kacz

yk, T

., 21

2-MAO

-6Lu

ke, E

., 41

-AA-10

, 81-A

A-15,

195

-APA-2

3Lu

mmer,

M.,

112-A

A-16

Lung

, T.,

169-C

FD-17

Luo,

H., 5

5-CFD

-5, 1

00-FD

-11, 1

73-FD

-19,

201

-CFD-2

1, 2

03-CF

D-23,

208

-FD-23

Luo,

L., 2

03-CF

D-23

Luo,

S., 3

3-PDL

-1/FD

-5, 6

7-PDL

-3, 1

44-PD

L-7,

180

-PDL-8

/APA

-20, 2

71-AP

A-33

Luo,

X., 1

78-M

ST-8

Lupo

glazo

ff, N

., 39

-AA-8

Lupp

, C.,

9-AFM

-2Lu

quet,

D.,

114-A

A-18

Lutz,

A., 1

81-PD

L-9/T

P-8Lu

tz, T.

, 249

-FT-1

Luxh

oj, J.

, 300

-ATIO

-29Lv,

Y., 2

42-CF

D-27

Lync

h, K.,

37-A

A-6, 2

66-AM

T-13/

GT-13

Lynn

, K.,

294-A

MT-14

/GT-1

5Ly

rintzi

s, A.,

37-A

A-6, 1

13-AA

-17, 2

45-CF

D-30

Lyu,

B., 3

8-AA-7

Ma, H

., 14

5-TP-7

Ma, P

., 26

-FD-2

Ma, Z

., 12

8-ATIO

-14Ma

chere

t, S.

, 216

-TP-10

/PDL

-10Ma

cMan

us, D

., 27

0-APA

-32Ma

dava

n, N.

, 281

-GEPC

-1Ma

ddale

na, L

., 86

-AMT-6

/GT-6

Madd

alon,

J., 1

7-ATIO

-2

Madd

en, T

., 67

-PDL-3

Maen

g, J.,

169

-CFD-1

7Ma

galha

es, P

., 28

3-MAO

-10Ma

gari,

P., 3

3-PDL

-1/FD

-5Ma

gin, T

., 34

-TP-1,

216

-TP-10

/PDL

-10, 2

17-TP

-11Ma

hade

van,

S., 3

08-M

AO-13

Maha

shab

de, A

., 92

-ATIO

-10, 1

97-AT

IO-18

Mahe

shwa

ri, A.,

52-A

TIO-6

Mahli

ch, S

., 27

5-ATIO

-25Ma

ierl, R

., 21

2-MAO

-6Ma

jić, F

., 78

-AA-12

, 235

-APA-2

7Ma

jumda

r, A.,

198-A

TIO-19

Maka

rov, B

., 24

3-CFD

-28Ma

lael, I

., 96

-CFD-1

0Ma

ldona

do, A

., 78

-AA-12

Malec

ki, T.

, 30-M

ST-1

Malick

, M.,

122-A

PA-13

Malik

, M.,

61-FD

-7, 2

02-CF

D-22

Malik

, W.,

16-AT

IO-1,

91-A

TIO-9,

198

-ATIO

-19Ma

linow

ski, M

., 28

0-FT-2

/GT-1

4Ma

llet,

M., 9

9-FD-1

0Ma

ngala

m, A.

, 9-AF

M-2,

124

-APA-1

5, 2

70-AP

A-32

Mang

ani, L

., 20

3-CFD

-23Ma

ni, K.

, 302

-CFD-3

2Ma

nkba

di, M

., 17

5-FD-2

2Ma

nkba

di, R.

, 79-A

A-13

Mano

ha, E

., 3-A

A-1, 1

55-AA

-25, 2

29-AA

-34,

230

-AA-35

, 259

-AA-37

Mano

salva

s, D.

, 271

-APA-3

3Ma

nsor,

S.,

12-AP

A-1Ma

nsou

r, N.,

58-CF

D-8, 2

88-TP

-13Ma

nsou

ri, N.

, 81-A

A-15

Mante

lli, M

., 35

-TP-2

Marai

s, K.,

156

-ACD-4

, 164

-ATIO

-15, 2

75-AT

IO-25

, 2

99-AT

IO-28

Marañ

on D

i Leo

, J.,

236-A

PA-28

March

iano,

R., 1

14-AA

-18Ma

rie, S

., 56

-CFD-6

Marin

eau,

E., 9

9-FD-1

0, 1

03-IT

AR-1

Marke

steijn

, A.,

6-AA-4

, 80-A

A-14

Marks

, C.,

191-A

MT-11

/GT-1

1Ma

rn, A.

, 151

-AA-21

Marqu

es, F

., 23

6-APA

-28Ma

rr, B.

, 238

-ATIO

-21Ma

rsan,

A., 2

27-AA

-32Ma

rsden

, O.,

4-AA-2

, 231

-AA-36

Marsh

, J.,

200-B

AL-2

Marsh

all, J

., 15

7-AFM

-9Ma

rshall

, P.,

85-AM

T-5/G

T-5Ma

rten,

D., 2

97-AP

A-37

Martin

, A.,

68-TP

-3, 1

08-TP

-5, 1

82-TP

-9Ma

rtin, P

., 12

0-AMT

-7/GT

-7

Martin

elli, L

., 57

-CFD-7

, 295

-APA-3

4Ma

rtinez

, A.,

101-F

D-12

Martin

ez, B

., 45

-AMT-3

/GT-3

, 47-A

PA-5

Martin

ez, S

., 14

5-TP-7

Martin

s, J.,

29-M

AO-1,

141

-MAO

-4, 2

52-M

AO-9,

3

07-M

AO-12

Mary,

I., 1

54-AA

-24Ma

sarat

i, P.,

84-AF

M-6

Maso

n, M.

, 217

-TP-11

Massa

, L.,

216-T

P-10/

PDL-1

0Ma

ssey,

K., 2

97-AP

A-37

Mastr

oddi,

F., 2

9-MAO

-1Ma

suda

, K.,

286-P

DL-13

Matay

oshi,

N.,

298-A

TIO-27

Mathe

r, J.,

273-A

SE-5

Mathe

w, J.

, 24-C

FD-4

Mathe

ws, E

., 25

5-PDL

-12Ma

thews

, J.,

3-AA-1

Matic

, P.,

102-F

D-13

Matsu

no, T

., 14

4-PDL

-7Ma

tsuno

, Y.,

51-AT

IO-5

Matto

s, B.

, 283

-MAO

-10, 3

07-M

AO-12

Matts

on, C

., 10

4-MAO

-3Ma

ughm

er, M

., 61

-FD-7

Mavri

plis,

D., 2

01-CF

D-21

Mavri

s, D.

, 37-A

A-6, 4

2-ACD

-1, 5

2-ATIO

-6, 5

3-ATIO

-7,

141

-MAO

-4, 1

42-M

ST-6,

156

-ACD-4

, 190

-ACD-5

, 1

98-AT

IO-19

, 213

-MAO

-7, 2

39-AT

IO-22

, 2

65-AC

D-7, 2

76-AT

IO-26

, 308

-MAO

-13Ma

y, G.

, 95-C

FD-9

Maye

r, R.,

92-AT

IO-10

, 197

-ATIO

-18Ma

zahe

ri, A.,

55-C

FD-5

McAlp

ine, A

., 37

-AA-6

Mcca

rthy,

P., 1

45-TP

-7Mc

Carth

y, P.,

259

-AA-37

McCla

in, S

., 19

6-ASE

-2Mc

Clure,

J., 1

32-CF

D-15

McCo

ll, C.,

83-A

FM-5

McCo

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A., 2

35-AP

A-27

McCri

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., 26

8-APA

-30Mc

Danie

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160-A

PA-17

McDa

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., 24

4-CFD

-29Mc

Dona

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, 304

-CFD-3

4Mc

Dona

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, 82-A

CD-2,

240

-ATIO

-23Mc

Grath

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123-A

PA-14

McGu

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., 24

-CFD-4

McIne

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., 40

-AA-9

Mcint

yre, T

., 34

-TP-1

McKe

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., 16

2-APA

-19Mc

Kierna

n, G.

, 28-F

D-4Mc

Kinley

, R.,

40-AA

-9Mc

Laug

hlin,

D., 3

9-AA-8

, 40-A

A-9

McLa

ughli

n, T.,

12-A

PA-1,

125

-APA-1

6Mc

Maste

rs, R.

, 35-T

P-2Mc

Mulla

n, W.

, 24-C

FD-4,

98-C

FD-12

Mcna

lly, D

., 29

8-ATIO

-27Mc

Partla

nd, M

., 51

-ATIO

-5, 2

98-AT

IO-27

McWa

ters,

M., 4

5-AMT

-3/GT

-3Me

ad, C

., 22

7-AA-3

2Me

ase,

K., 2

75-AT

IO-25

Meck

stroth

, C.,

29-M

AO-1

Mede

iros,

F., 2

43-CF

D-28

Mede

iros,

M., 2

30-AA

-35Me

dina,

A., 2

68-AP

A-30

Medw

ell, P

., 24

4-CFD

-29Me

hman

i, A.,

251-M

AO-8

Mehta

, P.,

214-M

ST-9

Mei, D

., 18

0-PDL

-8/AP

A-20

Mei, Q

., 25

3-MST

-11Me

ier, W

., 26

6-AMT

-13/G

T-13

Meink

e, M.

, 26-F

D-2, 3

8-AA-7

, 41-A

A-10,

79-A

A-13,

8

0-AA-1

4, 2

29-AA

-34, 3

05-CF

D-35

Melin

, T.,

283-M

AO-10

Mend

enha

ll, M.

, 269

-APA-3

1Me

ndon

ca, F

., 23

0-AA-3

5Me

ndoz

a, J.,

185

-AA-26

Mene

veau

, C.,

98-CF

D-12,

171

-CFD-1

9Me

ng, X

., 33

-PDL-1

/FD-5

, 144

-PDL-7

, 1

80-PD

L-8/A

PA-20

, 271

-APA-3

3Me

rle, X

., 11

3-AA-1

7Me

rrick,

J., 1

95-AP

A-23

Mery,

F., 2

62-AA

-40Me

smer,

B.,

212-M

AO-6,

283

-MAO

-10Me

ssac,

A., 1

76-M

AO-5,

251

-MAO

-8Me

yer, T

., 18

1-PDL

-9/TP

-8Me

yers,

J., 1

81-PD

L-9/T

P-8Me

yers,

T., 1

52-AA

-22, 2

97-AP

A-37

Mich

ael, J

., 18

1-PDL

-9/TP

-8Mi

chal,

T., 2

3-CFD

-3Mi

chel,

U.,

189-A

A-30

Mich

ou, Y

., 46

-AMT-4

/GT-4

, 192

-AMT-1

2/GT

-12Mi

cka,

D., 3

3-PDL

-1/FD

-5Mi

haes

cu, M

., 96

-CFD-1

0, 1

12-AA

-16Mi

lagre

da Fo

nsec

a, I.,

119

-AFM-

8Mi

lan, P

., 60

-FD-6/

PDL-2

Milan

ese,

F., 3

5-TP-2

Miles

, R.,

60-FD

-6/PD

L-2, 8

6-AMT

-6/GT

-6,

143

-PDL-6

, 255

-PDL-1

2Mi

ller, B

., 52

-ATIO

-6, 6

5-MST

-3Mi

ller, D

., 14

2-MST

-6, 2

82-LT

A-2Mi

ller, J

., 28

-FD-4

Mille

r, S.,

40-AA

-9, 1

53-AA

-23Mi

lls, B

., 85

-AMT-5

/GT-5

, 280

-FT-2/

GT-14

Mills,

M.,

120-A

MT-7/

GT-7

127

Auth

or/S

essio

n Ch

air In

dex

Milut

inovic

, D.,

91-AT

IO-9,

198

-ATIO

-19Mi

mani,

A., 2

31-AA

-36Mi

n, S.

, 42-A

CD-1,

156

-ACD-4

Minc

u, D.

, 154

-AA-24

, 187

-AA-28

Mine

ck, R

., 18

8-AA-2

9Mi

ngion

e, G.

, 115

-AA-19

Minis

ci, E.

, 214

-MST

-9Mi

nqian

g, Y.,

280

-FT-2/

GT-14

Miroc

hnitc

henk

o, V.,

190

-ACD-5

Misa

ka, T

., 19

6-ASE

-2Mi

tchell

, K.,

116-A

A-20

Mitsi

ngas

, C.,

107-P

DL-4

Mitsu

hash

i, R.,

293-A

CD-8

Mitta

l, A.,

15-AP

A-4, 2

34-AP

A-26,

297

-APA-3

7Mi

ttal, R

., 98

-CFD-1

2, 1

71-CF

D-19

Mock

ett, C

., 30

6-CFD

-36Mo

ckus

, L.,

239-A

TIO-22

Moell

er, T.

, 67-P

DL-3,

144-P

DL-7,

216-T

P-10/

PDL-1

0,

244

-CFD-2

9Mo

han,

A., 3

02-CF

D-32

Mohit

e, P.,

234

-APA-2

6Mo

in, P.

, 202

-CFD-2

2Mo

ini-Ye

kta, S

., 49

-APA-7

Molin

aro, N

., 29

7-APA

-37Mo

ntalvo

, C.,

157-A

FM-9

Monte

l, M.,

8-AFM

-1Mo

olcha

ndan

i, K.,

52-AT

IO-6

Moore

, M.,

54-AT

IO-8,

93-A

TIO-11

, 127

-ATIO

-13,

276

-ATIO

-26Mo

ored,

K., 1

00-FD

-11Mo

r-Yos

sef,

Y., 1

33-CF

D-16

Morar

u, G.

, 103

-ITAR

-1Mo

reau,

A., 7

7-AA-1

1, 1

52-AA

-22Mo

reau,

D., 1

52-AA

-22, 2

31-AA

-36Mo

reau,

E., 3

3-PDL

-1/FD

-5, 1

80-PD

L-8/A

PA-20

Morea

u, S.

, 3-AA

-1, 7

9-AA-1

3, 8

1-AA-1

5, 1

15-AA

-19,

152

-AA-22

, 185

-AA-26

, 187

-AA-28

, 227

-AA-32

Morei

ra, F.

, 9-AF

M-2,

241

-CFD-2

6Mo

relli,

E., 1

18-AF

M-7

Morga

n, P.,

102

-FD-13

Morga

n, R.,

34-T

P-1Mo

rikaw

a, Y.,

270

-APA-3

2Mo

rris, P

., 4-A

A-2, 4

0-AA-9

, 263

-AA-41

Morris

, S.,

38-AA

-7Mo

rrisse

y, P.,

108

-TP-5

Morsb

ach,

C., 1

33-CF

D-16

Morte

nsen

, C.,

209-F

D-24

Morto

n, S.

, 160

-APA-1

7, 1

74-FD

-20Mo

ses J

ohn C

hristy

Appo

lo, P.

, 67-P

DL-3

Moss,

M.,

308-M

AO-13

Mott,

D.,

102-F

D-13

Motte

r, M.,

165-A

TIO-16

, 199

-ATIO

-20

Mouri

ng, C

., 28

1-GEP

C-1Mo

vahe

d, P.,

211

-FD-26

Moye

s, A.,

137

-FD-16

Mueh

leise

n, R.,

262

-AA-40

Mueh

ler-Va

hl, H

., 10

1-FD-1

2Mu

eller,

F., 2

03-CF

D-23

Muell

er, J.

, 131

-CFD-1

4Mu

eller-

Vahl,

H.,

208-F

D-23

Mujum

dar, P

., 57

-CFD-7

Mukh

opad

hyay

, V.,

214-M

ST-9

Mulan

i, S.,

29-M

AO-1

Mulla

ne, M

., 19

3-APA

-21Mu

llene

rs, K.

, 50-A

PA-8,

235

-APA-2

7Mu

nday

, P.,

101-F

D-12

Mund

is, N

., 13

2-CFD

-15Mu

nera

Savin

o, F.,

8-AF

M-1,

249

-FT-1

Munju

lury,

R., 2

83-M

AO-10

Muns

on, M

., 13

6-FD-1

5Mu

rari, K

., 15

9-AMT

-10/G

T-10

Muray

ama,

M., 2

29-AA

-34, 2

30-AA

-35Mu

riel G

racia,

M.,

113-A

A-17

Murm

an, S

., 21

-CFD-1

, 96-C

FD-10

, 201

-CFD-2

1,

205

-CFD-2

5Mu

rphy,

C., 5

2-ATIO

-6, 6

5-MST

-3Mu

rray,

H., 1

14-AA

-18, 1

87-AA

-28Mu

rray,

J., 1

3-APA

-2, 2

97-AP

A-37

Murra

y, N.

, 80-A

A-14

Murra

y, W.

, 158

-AMT-9

/GT-9

Murrie

ta Me

ndoz

a, A.,

18-A

TIO-3

Musca

rello,

V., 8

4-AFM

-6Mu

siak,

J., 2

75-AT

IO-25

Muslu

bas,

Y., 5

7-CFD

-7Mu

yimbw

a, T.,

282

-LTA-2

Myos

e, R.,

27-F

D-3, 1

75-FD

-22Na

garaj

an, B

., 16

-ATIO

-1Na

huis,

R., 1

3-APA

-2Na

itoh,

K., 1

82-TP

-9Na

jafi, A

., 10

4-MAO

-3Na

jian A

sl, R.

, 283

-MAO

-10Na

kasa

to, K.

, 270

-APA-3

2Na

kash

ima,

T., 2

70-AP

A-32

Nalci,

M.,

66-M

ST-4

Nalla

pane

ni, S

., 35

-TP-2

Namb

a, M.

, 152

-AA-22

Namu

ra, N

., 12

5-APA

-16Na

nce,

D., 2

62-AA

-40Na

polita

no, M

., 43

-AFM-

3Na

rayan

aswa

my, V

., 27

-FD-3,

143

-PDL-6

, 174

-FD-20

Nark,

D.,

116-A

A-20

Narki

ewicz

, J.,

30-M

ST-1

Natar

ajan,

K., 1

53-AA

-23, 2

27-AA

-32Na

wroth

, H.,

27-FD

-3

Naye

ri, C.,

26-F

D-2, 2

97-AP

A-37

Neife

ld, A.

, 39-A

A-8Ne

ilan,

J., 1

65-AT

IO-16

, 199

-ATIO

-20Ne

ilsen,

T., 4

0-AA-9

Neitz

el, K.

, 69-T

P-4Ne

lson,

C., 4

9-APA

-7Ne

lson,

M., 1

14-AA

-18, 1

59-AM

T-10/

GT-10

, 187

-AA-28

Neuh

art, D

., 18

8-AA-2

9Ne

ville,

A., 2

46-FD

-27Ne

wcam

p, J.,

249

-FT-1

Newm

an, J

., 95

-CFD-9

, 170

-CFD-1

8, 3

05-CF

D-35

Ng, H

., 18

-ATIO

-3, 9

2-ATIO

-10Ng

uyen

, D.,

66-M

ST-4

Nguy

en, L

., 79

-AA-13

Nguy

en, M

., 88

-APA-1

0, 1

43-PD

L-6Ng

uyen

, N.,

49-AP

A-7, 1

24-AP

A-15

Nicho

ls, D

., 29

7-APA

-37Nic

hols,

J., 4

-AA-2,

39-A

A-8, 1

53-AA

-23Nic

olosi,

F., 8

-AFM-

1, 1

3-APA

-2, 1

04-M

AO-3

Niede

rmeie

r, D.,

31-M

ST-2

Nieto,

B.,

234-A

PA-26

Nigam

, N.,

284-M

AO-11

Nikba

y, M.

, 308

-MAO

-13Nis

hida,

H., 1

44-PD

L-7Nis

hikaw

a, H.

, 55-C

FD-5,

56-C

FD-6

Niu, J

., 24

4-CFD

-29Niu

, W.,

215-M

ST-10

Nodé

-Lang

lois,

T., 1

12-AA

-16, 1

87-AA

-28No

elting

, S.,

188-A

A-29

Nojim

a, Y.,

182

-TP-9

Noll,

B., 1

85-AA

-26No

mpeli

s, I.,

246

-FD-27

, 256

-TP-12

Nomu

ra, S

., 69

-TP-4

Nono

mura,

T., 6

0-FD-6

/PDL

-2, 1

14-AA

-18,

130

-CFD-1

3, 1

69-CF

D-17

Nords

trom,

J., 1

32-CF

D-15,

242

-CFD-2

7No

tt, J.

, 167

-BAL-1

, 200

-BAL-2

Nouz

awa,

T., 2

70-AP

A-32

Nova

ra, M

., 15

9-AMT

-10/G

T-10

Novik

ov, A

., 99

-FD-10

Nowa

k, M.

, 128

-ATIO

-14Nt

emos

, G.,

202-C

FD-22

O’Br

ien, D

., 15

-APA-4

, 295

-APA-3

4O’

Brien

, J.,

151-A

A-21

O’Br

ien, W

., 15

9-AMT

-10/G

T-10

O’By

rne, S

., 11

-AMT-2

/GT-2

, 46-A

MT-4/

GT-4,

1

21-AM

T-8/F

D-14/

TP-6/

GT-8

O’Co

nnor,

C., 9

1-ATIO

-9O’

Neill,

W.,

35-TP

-2O’

Reilly

, C.,

78-AA

-12, 2

35-AP

A-27

O’Su

llivan

, S.,

53-AT

IO-7

Obay

ashi,

S.,

125-A

PA-16

, 196

-ASE-2

Oberl

eithn

er, K.

, 266

-AMT-1

3/GT

-13Oc

heltre

e, C.,

89-A

PA-11

, 251

-MAO

-8, 2

96-AP

A-35

Ochie

ng, W

., 19

8-ATIO

-19Oe

felein

, J.,

244-C

FD-29

Ogas

awara

, T.,

68-TP

-3Og

awa,

S., 2

86-PD

L-13

Ojed

a, S.

, 95-C

FD-9

Okad

a, Y.,

270

-APA-3

2Ok

amoto

, T.,

182-T

P-9Ok

olo, W

., 8-A

FM-1,

273

-ASE-5

Ol, M

., 12

5-APA

-16, 2

34-AP

A-26

Olejn

iczak

, J.,

69-TP

-4Ol

iveira

, E.,

119-A

FM-8

Olive

r, J.,

104-M

AO-3

Olivi

ero, N

., 13

7-FD-1

6Ol

iviu,

S., 1

3-APA

-2, 2

96-AP

A-35

Olliv

ier G

ooch

, C.,

21-CF

D-1, 2

3-CFD

-3, 1

31-CF

D-14

Olse

n, M.

, 172

-CFD-2

0Ol

son,

E., 2

52-M

AO-9

Olso

n, M.

, 240

-ATIO

-23Ol

son,

R., 4

3-AFM

-3Om

ar, F.

, 51-A

TIO-5

Omidy

, A.,

68-TP

-3On

ishi, K

., 27

0-APA

-32Or

avec

, H.,

273-A

SE-5

Orda

z, I.,

14-A

PA-3

Orr, M

., 15

6-ACD

-4Or

ra, T.

, 128

-ATIO

-14, 2

12-M

AO-6

Osma

n, A.,

178

-MST

-8Os

trikov

, N.,

115-A

A-19

Otsu

, H.,

144-P

DL-7

Overm

eyer,

A., 1

20-AM

T-7/G

T-7Ow

ens,

J., 1

96-AS

E-2Oy

ama,

A., 1

14-AA

-18Oz

a, U.

, 22-C

FD-2

Ozca

n, M.

, 265

-ACD-7

Özge

n, S.

, 97-C

FD-11

Oztek

in, A.

, 164

-ATIO

-15Pa

ck, J

., 27

4-ATIO

-24Pa

ck M

elton

, L.,

279-F

D-31

Pado

is, T.

, 3-AA

-1Pa

gani,

C., 2

30-AA

-35Pa

ge, G

., 24

-CFD-4

Page

, M.,

276-A

TIO-26

Pagli

one,

P., 1

28-AT

IO-14

Pak,

C., 9

-AFM-

2, 1

41-M

AO-4

Palac

ios, F

., 13

3-CFD

-16, 2

04-CF

D-24,

271

-APA-3

3,

283

-MAO

-10Pa

lla, A

., 10

7-PDL

-4Pa

lmer,

E., 5

1-ATIO

-5Pa

lmer,

G.,

108-T

P-5Pa

lmier

i, F.,

46-AM

T-4/G

T-4

Palop

o, K.,

142

-MST

-6Pa

luch,

B., 1

3-APA

-2Pa

lumbo

, R.,

164-A

TIO-15

Pan,

J., 2

1-CFD

-1Pa

n, Q.

, 145

-TP-7

Panc

hal, J

., 52

-ATIO

-6Pa

ncha

l, K.,

250-L

TA-1

Pand

a, J.,

99-F

D-10

Pand

are, A

., 20

1-CFD

-21Pa

ndya

, S.,

305-C

FD-35

Pane

rai, F

., 28

8-TP-1

3Pa

nesi,

M.,

69-TP

-4Pa

nkrat

ov, I

., 18

7-AA-2

8Pa

nt, R.

, 282

-LTA-2

Papa

dimitri

ou, C

., 28

3-MAO

-10Pa

padim

itriou

, D.,

283-M

AO-10

Papa

georg

io, E.

, 128

-ATIO

-14Pa

pamo

schou

, D.,

227-A

A-32,

264

-AA-42

Papa

thakis

, K.,

240-A

TIO-23

Paran

in, G

., 11

5-AA-1

9Pa

rdowi

tz, B

., 17

3-FD-1

9Pa

rent,

B., 2

16-TP

-10/P

DL-10

Paren

te, A.

, 216

-TP-10

/PDL

-10Pa

rish,

E., 5

8-CFD

-8Pa

rk, G

., 13

9-FD-1

8Pa

rk, J.

, 202

-CFD-2

2, 2

42-CF

D-27,

251

-MAO

-8,

296

-APA-3

5Pa

rk, M

., 14-A

PA-3,

23-CF

D-3, 9

7-CFD

-11, 1

60-AP

A-17

Park,

S.,

235-A

PA-27

Parke

, B.,

51-AT

IO-5

Parke

r, P.,

294-A

MT-14

/GT-1

5Pa

rry, A

., 37

-AA-6

Parso

ns, N

., 69

-TP-4

Paruc

huri,

C., 3

-AA-1,

38-A

A-7, 7

9-AA-1

3, 1

52-AA

-22Pa

scarel

la, D

., 16

4-ATIO

-15Pa

schere

it, C.,

27-F

D-3, 2

97-AP

A-37

Pasco

, Y.,

227-A

A-32

Pasili

ao, C

., 12

-APA-1

, 22-C

FD-2,

90-A

PA-12

Passe

, B.,

162-A

PA-19

Pasto

relli,

V., 7

7-AA-1

1Pa

tel, S

., 24

-CFD-4

Pater

son,

E., 2

6-FD-2

Patil,

M.,

9-AFM

-2, 3

0-MST

-1, 2

52-M

AO-9

Patte

rson,

A., 1

57-AF

M-9

Patte

rson,

J., 2

14-M

ST-9

Patte

rson,

M., 1

27-AT

IO-13

Paul,

R., 2

35-AP

A-27

Paula

, A.,

307-M

AO-12

Pauz

, V.,

229-A

A-34

Pawl

etta,

T., 1

77-M

ST-7

Paya

n, A.,

53-A

TIO-7,

239

-ATIO

-22Pe

ake,

N., 3

-AA-1,

260

-AA-38

128

Auth

or/S

essio

n Ch

air In

dex

Pearc

e, R.,

52-A

TIO-6

Pech

livan

oglou

, G.,

26-FD

-2, 2

97-AP

A-37

Pede

rson,

C., 1

74-FD

-20Pe

drama

sl, N

., 64

-MAO

-2Pe

i, J.,

119-A

FM-8

Pei, P

., 27

6-ATIO

-26Pe

inke,

J., 5

0-APA

-8, 2

71-AP

A-33

Pelle

tier, D

., 58

-CFD-8

, 204

-CFD-2

4, 3

04-CF

D-34

Peltie

r, S.,

266-A

MT-13

/GT-1

3Pe

ng, D

., 19

7-ATIO

-18Pe

ng, J

., 19

0-ACD

-5Pe

ng, S

., 6-A

A-4, 1

15-AA

-19, 1

54-AA

-24Pe

ng, W

., 19

8-ATIO

-19Pe

ng, X

., 53

-ATIO

-7Pe

rcin,

M., 9

7-CFD

-11, 2

08-FD

-23Pe

reira,

D.,

236-A

PA-28

Perez

, R.,

141-M

AO-4,

267

-APA-2

9Pe

riaux

, J.,

180-P

DL-8/

APA-2

0Pe

roomi

an, O

., 24

5-CFD

-30Pe

rsson

, P.,

170-C

FD-18

Peter

, J.,

173-F

D-19

Peter

s, B.

, 306

-CFD-3

6Pe

ters,

C., 8

6-AMT

-6/GT

-6Pe

terse

n, S.

, 282

-LTA-2

Peter

sson,

Ö, 2

12-M

AO-6

Pfaen

der, H

., 53

-ATIO

-7, 2

39-AT

IO-22

Pfifer

, H.,

157-A

FM-9

Pianta

nida,

S., 5

-AA-3,

189

-AA-30

Piao,

Y., 2

44-CF

D-29

Pierre

, D.,

154-A

A-24

Pilon

, A.,

153-A

A-23

Pimen

ta, B

., 77

-AA-11

Pini, M

., 13

3-CFD

-16Pin

ier, J

., 88

-APA-1

0, 1

23-AP

A-14

Pinon

-Fisch

er, O

., 14

2-MST

-6Pio

t, E.,

262

-AA-40

Pipern

i, P.,

104-M

AO-3,

213

-MAO

-7, 2

84-M

AO-11

Planc

k, C.,

234

-APA-2

6Ple

mmon

s, D.

, 11-A

MT-2/

GT-2

Ploetn

er, K.

, 52-A

TIO-6,

53-A

TIO-7

Pogg

ie, J.

, 102

-FD-13

, 211

-FD-26

, 286

-PDL-1

3,

306

-CFD-3

6Po

insot,

T., 1

85-AA

-26Po

lacze

k, J.,

280

-FT-2/

GT-14

Pome

roy, B

., 87

-APA-9

Pons

-Prat,

J., 1

80-PD

L-8/A

PA-20

Poole

, D.,

64-M

AO-2,

125

-APA-1

6, 2

83-M

AO-10

Popie

, V.,

262-A

A-40

Popo

v, I.,

33-P

DL-1/

FD-5

Porne

t, C.,

53-A

TIO-7

Poros

eva,

S., 9

6-CFD

-10, 2

05-CF

D-25

Porte

ous,

A., 9

6-CFD

-10

Porum

bel, I

., 96

-CFD-1

0Po

st, M

., 64

-MAO

-2, 1

62-AP

A-19

Pott-P

ollen

ske,

M., 3

-AA-1,

230

-AA-35

Potte

r, C.,

141-M

AO-4

Povin

elli, L

., 28

1-GEP

C-1Po

wers,

R., 4

0-AA-9

Prabh

u, D.

, 102

-FD-13

, 108

-TP-5

Prach

ar, A.

, 233

-APA-2

5Pra

deep

, A.,

57-CF

D-7Pra

sad,

R., 1

2-APA

-1, 2

05-CF

D-25

Precu

p, N.

, 49-A

PA-7

Priolo

, F.,

9-AFM

-2Prö

bstin

g, S.

, 38-A

A-7Pru

ett, B

., 62

-FD-8,

175

-FD-22

Pruis,

M.,

237-A

SE-3,

272

-ASE-4

Przulj

, V.,

243-C

FD-28

Pullia

m, T.

, 136

-FD-15

Pytel

, D.,

34-TP

-1Qi

, B.,

145-T

P-7Qi

, X.,

284-M

AO-11

Qian

, J.,

285-M

ST-12

Qiao

, W.,

151-A

A-21,

260

-AA-38

, 267

-APA-2

9Qi

u, S.

, 204

-CFD-2

4Qi

u, X.

, 285

-MST

-12Qu

, Q.,

26-FD

-2, 4

7-APA

-5Qu

aglia

, M.,

187-A

A-28

Quall

s, G.

, 165

-ATIO

-16, 1

99-AT

IO-20

Quara

nta, G

., 84

-AFM-

6Qu

eiroz

, R.,

7-AA-5

Quinl

an, J

., 24

4-CFD

-29Qu

inn, M

., 45

-AMT-3

/GT-3

Quint

o, P.,

158

-AMT-9

/GT-9

Quix,

H.,

85-AM

T-5/G

T-5Qu

on, L

., 91

-ATIO

-9Ra

dyisy

ewsk

i, P.,

30-M

ST-1

Raffe

l, M.,

192-A

MT-12

/GT-1

2Ra

gab,

S., 2

36-AP

A-28

Ragn

i, D.,

37-AA

-6, 2

86-PD

L-13

Rahm

an, M

., 13

9-FD-1

8Ra

j, P., 1

76-M

AO-5,

251-M

AO-8,

265-A

CD-7,

296-A

PA-35

Rajag

opala

n, R.,

243

-CFD-2

8Ra

jput,

P., 2

33-AP

A-25

Ralla

bhan

di, S

., 14

-APA-3

, 89-A

PA-11

Rama

chan

dran,

A., 2

7-FD-3

, 28-F

D-4Ra

mamo

orthy

, K.,

275-A

TIO-25

Rama

murti,

R., 4

8-APA

-6, 2

33-AP

A-25

Rama

n, G.

, 262

-AA-40

Rama

n, V.,

304

-CFD-3

4Ra

mesh

, N.,

67-PD

L-3Ra

mirez

, W.,

38-AA

-7Ra

ncou

rt, D

., 21

3-MAO

-7, 2

76-AT

IO-26

Rand

, J.,

200-B

AL-2

Rand

t, N.

, 52-A

TIO-6,

128

-ATIO

-14Ra

o, A.,

126

-ATIO

-12, 1

56-AC

D-4Ra

shad

, R.,

204-C

FD-24

Ratha

krish

nan,

B., 2

44-CF

D-29

Ratha

krish

nan,

E., 5

0-APA

-8Ra

ulede

r, J.,

236-A

PA-28

Rautm

ann,

C., 7

9-AA-1

3, 1

55-AA

-25Ra

vetta

, P.,

188-A

A-29

Ray,

J., 1

39-FD

-18Ra

zi, P.

, 58-C

FD-8

Reard

on, J

., 46

-AMT-4

/GT-4

Reard

on, S

., 17

7-MST

-7Re

asor,

D.,

22-CF

D-2Re

donn

et, S

., 15

5-AA-2

5, 2

61-AA

-39Re

ed, D

., 26

2-AA-4

0Re

ed, H

., 61

-FD-7,

137

-FD-16

, 247

-FD-28

Reed

er, M

., 15

8-AMT

-9/GT

-9, 1

95-AP

A-23

Reeg

er, J.

, 141

-MAO

-4Re

ge, A

., 48

-APA-6

Rehm

anjan

, U.,

128-A

TIO-14

Reich

e, N.

, 39-A

A-8, 1

12-AA

-16Re

ichma

n, B.

, 40-A

A-9Re

imer,

L., 5

7-CFD

-7Re

issne

r, F.,

101-F

D-12

Reist

, T.,

267-A

PA-29

Reme

s, B.

, 97-C

FD-11

Ren,

Y., 2

1-CFD

-1, 8

4-AFM

-6, 2

14-M

ST-9,

2

41-CF

D-26,

248

-FD-29

Rend

all, T

., 64

-MAO

-2, 1

25-AP

A-16,

283

-MAO

-10Re

nder,

P., 8

8-APA

-10Re

nner,

A., 1

04-M

AO-3

Renn

ie, M

., 88

-APA-1

0, 1

43-PD

L-6, 2

55-PD

L-12

Rey,

C., 4

7-APA

-5Re

y, M.

, 262

-AA-40

Reya

z Ahm

ed, A

., 50

-APA-8

Reyn

olds,

D., 3

1-MST

-2Re

ynold

s, T.,

51-A

TIO-5,

163

-ASE-1

Reza

Ahrab

i, B.,

95-CF

D-9, 1

22-AP

A-13

Rhew

, R.,

158-A

MT-9/

GT-9,

1

91-AM

T-11/

GT-11

, 294

-AMT-1

4/GT

-15Rh

oads

, J.,

259-A

A-37

Rhod

es, D

., 52

-ATIO

-6Ric

hards

on, J

., 15

7-AFM

-9Ric

hards

on, T

., 84

-AFM-

6, 2

12-M

AO-6

Rickli

ck, M

., 14

5-TP-7

Righi,

M.,

236-A

PA-28

, 278

-FD-30

Ringu

ette,

M., 1

00-FD

-11Rit

ter, M

., 57

-CFD-7

Ritz,

R., 2

2-CFD

-2, 9

6-CFD

-10Riv

iere,

P., 2

17-TP

-11Riz

zetta

, D.,

101-F

D-12

Rizzi,

A., 1

60-AP

A-17

Rizzi,

S.,

152-A

A-22

Röbe

n, T.,

265

-ACD-7

Robe

rtson

, G.,

174-F

D-20

Robin

son,

S., 3

1-MST

-2, 2

69-AP

A-31

Robin

son I

II, J.,

239

-ATIO

-22Ro

chlitz

, H.,

159-A

MT-10

/GT-1

0Ro

deba

ugh,

G., 1

73-FD

-19Ro

drigu

ez, Y

., 51

-ATIO

-5Ro

e, P.,

56-C

FD-6,

169

-CFD-1

7Ro

ger, M

., 79

-AA-13

, 81-A

A-15,

152

-AA-22

, 1

54-AA

-24, 1

87-AA

-28Ro

gers,

M.,

61-FD

-7Ro

gers,

S.,

233-A

PA-25

Rohlm

ann,

D., 8

7-APA

-9Ro

idl, B

., 41

-AA-10

Rolin

g, P.,

91-A

TIO-9

Roma

nelli,

G.,

203-C

FD-23

Rorie

, R.,

274-A

TIO-24

Rose

, C.,

107-P

DL-4

Rose

ma, C

., 90

-APA-1

2, 2

96-AP

A-35

Rose

mann

, H.,

178-M

ST-8

Rossi

an, L

., 23

1-AA-3

6Ro

ssign

ol, K.

, 231

-AA-36

Roth,

B.,

251-M

AO-8,

307

-MAO

-12Ro

thhaa

r, P.,

119-A

FM-8,

165

-ATIO

-16, 1

99-AT

IO-20

Roug

ier, T

., 25

9-AA-3

7Ro

usse

l, C.,

98-CF

D-12

Rouz

bar, R

., 24

4-CFD

-29Ro

we, P

., 15

8-AMT

-9/GT

-9Ro

wley

, C.,

136-F

D-15,

295

-APA-3

4Ro

y, A.,

246

-FD-27

Roy,

C., 3

0-MST

-1, 9

7-CFD

-11, 1

31-CF

D-14

Roy,

R., 1

72-CF

D-20

Roy,

S., 9

2-ATIO

-10, 2

75-AT

IO-25

Roy S

alam,

I., 1

90-AC

D-5Ro

yalty

, C.,

116-A

A-20

Ru, P

., 15

7-AFM

-9Ru

dnick

-Cohe

n, E.,

29-M

AO-1

Rudn

ik, R.

, 87-A

PA-9

Ruett

en, M

., 22

-CFD-2

, 96-C

FD-10

, 178

-MST

-8Ru

leva,

L., 1

93-AP

A-21

Ruma

nn, H

., 27

3-ASE

-5Ru

msey

, C.,

58-CF

D-8, 1

39-FD

-18, 1

72-CF

D-20,

2

08-FD

-23Ru

sak,

Z., 6

2-FD-8

, 173

-FD-19

Russe

ll, S.

, 141

-MAO

-4Ru

therfo

rd, M

., 88

-APA-1

0Sa

, J.,

235-A

PA-27

Sabe

tta, V

., 8-A

FM-1

Sadiq

ue, J

., 98

-CFD-1

2, 1

71-CF

D-19

Sado

vsky

, A.,

17-AT

IO-2

Sadra

ey, M

., 19

1-AMT

-11/G

T-11

Sadri

, V.,

62-FD

-8Sa

geba

um, M

., 25

2-MAO

-9Sa

heby

, E.,

267-A

PA-29

Sahin

, B.,

25-FD

-1Sa

hin, M

., 64

-MAO

-2Sa

hni, O

., 63

-FD-9

Sahu

, J.,

90-AP

A-12

Said,

M.,

167-B

AL-1,

200

-BAL-2

Saif U

llah K

halid

, M.,

133-C

FD-16

Saiki

a, B.

, 28-F

D-4Sa

ini, A

., 46

-AMT-4

/GT-4

, 267

-APA-2

9Sa

ka, P

., 88

-APA-1

0Sa

kurai

, T.,

66-M

ST-4

Salah

El D

in, I.

, 114

-AA-18

Salas

, P.,

115-A

A-19

Salee

m, M

., 17

4-FD-2

0Sa

lehian

, S.,

79-AA

-13Sa

lemi, L

., 28

-FD-4

Salin

as, M

., 84

-AFM-

6Sa

lton,

A., 4

0-AA-9

Salze

, E.,

231-A

A-36

Sama

nta, A

., 78

-AA-12

Sama

reh, J

., 68

-TP-3

Sama

ritano

, A.,

194-A

PA-22

Sami

my, M

., 33

-PDL-1

/FD-5

, 153

-AA-23

Samu

el, A.

, 240

-ATIO

-23Sa

ndbe

rg, M

., 51

-ATIO

-5Sa

ndbe

rg, R.

, 171

-CFD-1

9Sa

nders

, L.,

259-A

A-37

Sand

ham,

N.,

209-F

D-24

Sane

trik, M

., 12

4-APA

-15Sa

njaya

, D.,

95-CF

D-9Sa

njose

, M.,

227-A

A-32

Sank

aran,

V., 1

32-CF

D-15

Sano

, A.,

41-AA

-10Sa

ntos,

J., 3

0-MST

-1, 2

82-LT

A-2Sa

ntos,

L., 1

17-AC

D-3, 2

13-M

AO-7

Santo

s, P.,

43-A

FM-3

Santo

s Pere

ira, R

., 28

6-PDL

-13Sa

raf, A

., 16

-ATIO

-1, 5

1-ATIO

-5, 9

1-ATIO

-9Sa

ric, W

., 61

-FD-7,

137

-FD-16

Sarka

r, S.,

136-F

D-15

Sarra

dj, E.

, 186

-AA-27

, 231

-AA-36

Sarto

r, F.,

96-CF

D-10

Sasa

ki, J.

, 293

-ACD-8

Sasa

ki, K.

, 5-AA

-3Sa

sana

puri,

B., 1

78-M

ST-8

Sasid

haran

Nair

, U.,

80-AA

-14Sa

soh,

A., 8

9-APA

-11, 1

38-FD

-17Sa

ssanis

, V.,

209-F

D-24

Sato,

M.,

60-FD

-6/PD

L-2Sa

tori, S

., 29

3-ACD

-8

129

Auth

or/S

essio

n Ch

air In

dex

Satte

lmay

er, T.

, 41-A

A-10,

113

-AA-17

, 185

-AA-26

Saun

ders,

D.,

182-T

P-9, 2

17-TP

-11Sa

urav,

S., 1

25-AP

A-16

Saw,

Z., 2

65-AC

D-7Sa

whill,

B.,

16-AT

IO-1

Sawy

er, J.

, 181

-PDL-9

/TP-8

Scan

lan, J

., 12

8-ATIO

-14, 3

08-M

AO-13

Scara

no, F

., 38

-AA-7,

192

-AMT-1

2/GT

-12,

266

-AMT-1

3/GT

-13Sc

haefe

r, J.,

58-CF

D-8Sc

haefe

r, M.,

299-A

TIO-28

Scha

uerha

mer, D

., 26

9-APA

-31Sc

heel,

H.,

7-AA-5

Sche

rer S

chwe

ning,

G., 1

04-M

AO-3

Sche

tz, J.

, 29-M

AO-1,

46-A

MT-4/

GT-4

Schia

vo, L

., 98

-CFD-1

2Sc

hiavo

ne, N

., 13

6-FD-1

5Sc

hindle

r, M.,

18-AT

IO-3

Schin

wald,

C., 9

1-ATIO

-9Sc

hlimm

, K.,

166-A

TIO-17

Schli

mpert

, S.,

41-AA

-10Sc

hlottk

e, M.

, 229

-AA-34

Schlu

ter, J

., 47

-APA-5

, 269

-APA-3

1Sc

hmidt

, A.,

177-M

ST-7

Schm

idt, B

., 11

-AMT-2

/GT-2

Schm

idt, H

., 10

5-MST

-5, 1

95-AP

A-23

Schm

idt-Sk

ipiol,

F., 1

66-AT

IO-17

Schm

isseu

r, J.,

10-AM

T-1/G

T-1Sc

hmitt,

F., 9

1-ATIO

-9Sc

hmoll

grube

r, P.,

82-AC

D-2Sc

hneid

er, S

., 28-F

D-4, 6

1-FD-7

, 137

-FD-16

, 209

-FD-24

Schn

eiders

, L.,

305-C

FD-35

Scho

lz, P.

, 125

-APA-1

6, 1

59-AM

T-10/

GT-10

Scho

mberg

, T.,

22-CF

D-2, 9

6-CFD

-10Sc

hönle

itner,

F., 1

51-AA

-21Sc

hram,

C., 3

-AA-1,

79-AA

-13, 1

12-AA

-16, 2

31-AA

-36Sc

hrijer

, F.,

138-F

D-17

Schro

ck, C

., 20

1-CFD

-21Sc

hroed

er, A.

, 159

-AMT-1

0/GT

-10Sc

hroed

er, W

., 6-A

A-4, 2

6-FD-2

, 38-A

A-7, 4

1-AA-1

0,

79-A

A-13,

80-A

A-14,

229

-AA-34

, 305

-CFD-3

5Sc

hülei

n, E.,

138

-FD-17

Schu

ltz, M

., 16

4-ATIO

-15Sc

hultz

, V.,

274-A

TIO-24

Schu

lze, M

., 11

3-AA-1

7Sc

huma

n, W.

, 280

-FT-2/

GT-14

Schu

ster, D

., 23

3-APA

-25Sc

huste

r, W.,

151-A

A-21,

198

-ATIO

-19Sc

hutte

, J.,

239-A

TIO-22

Schw

artze

ntrub

er, T.

, 256

-TP-12

Schw

er, D

., 10

2-FD-1

3Sc

iacch

itano

, A.,

266-A

MT-13

/GT-1

3

Sclaf

ani, A

., 87

-APA-9

, 233

-APA-2

5Sc

oggin

s, J.,

217

-TP-11

Scola

n, E.,

46-A

MT-4/

GT-4

Scott

, R.,

124-A

PA-15

Scull

y, R.,

273

-ASE-5

Secco

, N.,

307-M

AO-12

Seck

in, S

., 17

4-FD-2

0Se

eley,

B., 2

39-AT

IO-22

Seide

l, J.,

12-AP

A-1, 1

25-AP

A-16,

236

-APA-2

8Se

itzma

n, J.,

159

-AMT-1

0/GT

-10Se

khar,

S.,

58-CF

D-8Se

lf, R.,

5-AA

-3, 3

9-AA-8

, 227

-AA-32

Selfri

dge,

J., 1

27-AT

IO-13

Selic,

T., 1

51-AA

-21Se

lig, M

., 15

-APA-4

, 87-A

PA-9,

297

-APA-3

7Se

milet

ov, V

., 6-A

A-4, 8

0-AA-1

4, 2

28-AA

-33Se

mmelm

ann,

J., 8

5-AMT

-5/GT

-5Se

mper,

M.,

278-F

D-30

Seng

issen

, A.,

188-A

A-29

Sepk

a, S.

, 68-T

P-3, 1

08-TP

-5Se

rafini,

J., 1

62-AP

A-19

Serpi

eri, J

., 38

-AA-7,

88-A

PA-10

Serre

, G.,

187-A

A-28

Sescu

, A., 2

4-CFD

-4, 41

-AA-10

, 81-A

A-15,

98-CF

D-12,

2

09-FD

-24Se

sterhe

nn, J

., 30

6-CFD

-36Se

vil, H

., 12

8-ATIO

-14Se

zer, E

., 66

-MST

-4Sh

a, Z.,

52-A

TIO-6

Shah

, G.,1

54-AF

M-9

Shah

, H.,

203-C

FD-23

Shah

par, S

., 25

1-MAO

-8Sh

arbatd

ar, M

., 13

1-CFD

-14Sh

arma,

H., 2

35-AP

A-27

Sharm

a, R.,

300

-ATIO

-29Sh

arma,

S., 2

39-AT

IO-22

Shee

he, S

., 11

-AMT-2

/GT-2

Shen

, Q.,

191-A

MT-11

/GT-1

1Sh

eng,

C., 1

22-AP

A-13,

194

-APA-2

2Sh

ephe

rd, J.

, 11-A

MT-2/

GT-2

Sherr

y, L.,

52-A

TIO-6,

117

-ACD-3

Shes

hadri

, T.,

67-PD

L-3Sh

eta, E

., 19

5-APA

-23Sh

eth, K

., 12

6-ATIO

-12Sh

i, R.,

190-A

CD-5,

251

-MAO

-8Sh

i, S.,

107-P

DL-4

Shi, Y

., 25

-FD-1

Shih,

A., 1

64-AT

IO-15

Shim

osaw

a, Y.,

286

-PDL-1

3Sh

imoy

ama,

K., 1

25-AP

A-16

Shin,

S.,

126-A

TIO-12

Shipt

on, L

., 12

8-ATIO

-14

Shive

ly, J.

, 274

-ATIO

-24Sh

milov

ich, A

., 27

1-APA

-33Sh

neide

r, M.,

216-T

P-10/

PDL-1

0Sh

oda,

T., 1

38-FD

-17Sh

ort, E

., 14

5-TP-7

Shuk

la, H

., 9-A

FM-2

Shyy

, W.,

97-CF

D-11,

268

-APA-3

0Sia

la, F.

, 234

-APA-2

6Sid

diqi, S

., 3-A

A-1Sid

harth

, G.,

139-F

D-18

Sidiro

poulo

s, S.

, 198

-ATIO

-19Sie

bert,

J., 2

30-AA

-35Sie

rcke,

M., 7

-AA-5

Siiko

nen,

T., 1

39-FD

-18Sij

tsma,

P., 1

15-AA

-19Sil

leken

s, P.,

91-A

TIO-9

Silton

, S.,

90-AP

A-12,

195

-APA-2

3, 2

46-FD

-27,

271

-APA-3

3Sil

va, R

., 11

7-ACD

-3Sil

va, S

., 15

6-ACD

-4Sil

va, W

., 12

4-APA

-15, 2

73-AS

E-5Sil

vestr

e, F.,

5-AA

-3, 9

-AFM-

2Sil

vestr

e, M.

, 104

-MAO

-3Sim

ao Fe

rreira

, C.,

279-F

D-31

Simerl

y, S.

, 158

-AMT-9

/GT-9

Simõe

s, L.,

4-AA

-2Sim

on, F

., 26

2-AA-4

0Sin

ayok

o, S.

, 38-A

A-7, 1

87-AA

-28Sin

gh, A

., 27

9-FD-3

1Sin

gh, B

., 25

5-PDL

-12Sin

gh, K

., 9-A

FM-2

Singh

, M.,

235-A

PA-27

Singh

, R.,

162-A

PA-19

, 268

-APA-3

0Sin

gh, S

., 84

-AFM-

6Sin

ha, A

., 22

8-AA-3

3Sin

ha, K

., 28

-FD-4

Sinha

, P.,

276-A

TIO-26

Sinnig

e, T.,

37-A

A-6Sio

zos-R

ouso

ulis,

L., 1

52-AA

-22Sir

ohi, J

., 16

2-APA

-19Sit

arama

n, J.,

21-C

FD-1

Sivan

eri, V

., 10

1-FD-1

2Siv

asub

raman

ian, J

., 10

2-FD-1

3Sjo

green

, B.,

24-CF

D-4Sk

ies, F

., 13

2-CFD

-15Sk

inner,

J., 1

17-AC

D-3Sk

vorts

ov, R

., 18

7-AA-2

8Sla

boch

, P.,

303-C

FD-33

Slagle

, A.,

226-A

A-31

Slater

, J.,

279-F

D-31

Slege

rs, N

., 30

-MST

-1Slo

tnick

, J.,

47-AP

A-5, 3

01-CF

D-31

Smelt

zer, S

., 28

1-GEP

C-1Sm

ith, A

., 11

7-ACD

-3Sm

ith, B

., 17

2-CFD

-20Sm

ith, D

., 68

-TP-3,

108

-TP-5,

158

-AMT-9

/GT-9

, 2

10-FD

-25Sm

ith, J

., 65

-MST

-3, 1

42-M

ST-6,

278

-FD-30

Smith

, K.,

145-T

P-7Sm

ith, M

., 25

9-AA-3

7Sm

olarki

ewicz

, P.,

163-A

SE-1

Snyd

er, M

., 23

6-APA

-28So

honi,

N.,

37-AA

-6Şö

hret,

Y., 2

73-AS

E-5So

ler, L

., 27

5-ATIO

-25So

lodov

nikov

, S.,

193-A

PA-21

Son,

P., 1

38-FD

-17So

ng, J

., 10

0-FD-1

1So

ntag,

J., 2

55-PD

L-12

Soria

, J.,

153-A

A-23

Sorok

ach,

M., 2

14-M

ST-9

Souc

asse

, L.,

217-T

P-11

Soufi

ani, A

., 21

7-TP-1

1So

uza,

D., 2

30-AA

-35Sp

agno

lo, S

., 20

5-CFD

-25Sp

alart,

P., 1

23-AP

A-14,

211

-FD-26

Spalt

, T.,

259-A

A-37

Spec

k, S.

, 88-A

PA-10

Spee

r, S.,

302-C

FD-32

Speh

r, C.,

186-A

A-27,

260

-AA-38

Spen

cer, T

., 30

0-ATIO

-29Sp

iegel,

S.,

55-CF

D-5, 1

30-CF

D-13

Spieg

elberg

, H.,

297-A

PA-37

Spille

rs, R.

, 62-F

D-8, 1

75-FD

-22Sp

inelli,

A., 2

6-FD-2

Sprav

ka, J

., 24

9-FT-1

Sree

nivas

, K.,

15-AP

A-4, 1

22-AP

A-13,

297

-APA-3

7Sr

idhar,

B.,

18-AT

IO-3,

92-A

TIO-10

Sridh

aran,

A., 1

62-AP

A-19

Srigr

arom,

S.,

162-A

PA-19

, 234

-APA-2

6, 2

65-AC

D-7Sr

iniva

san,

C., 1

81-PD

L-9/T

P-8Sr

iniva

san,

E., 5

0-APA

-8Sr

ivasta

va, A

., 13

8-FD-1

7St

achu

ra, M

., 15

7-AFM

-9St

agni,

A., 2

44-CF

D-29

Stale

y, A.,

299

-ATIO

-28St

alnov

, O.,

7-AA-5

, 38-A

A-7, 7

9-AA-1

3St

anek

, M.,

33-PD

L-1/F

D-5St

anfor

d, B.

, 49-A

PA-7,

124

-APA-1

5St

angfe

ld, C.

, 208

-FD-23

Steig

er, R.

, 46-A

MT-4/

GT-4

Stein

, F.,

88-AP

A-10

Stein

brenn

er, J.

, 23-C

FD-3

Step

han,

A., 1

96-AS

E-2, 2

37-AS

E-3

Step

hani,

K., 2

16-TP

-10/P

DL-10

, 288

-TP-13

Step

hen,

S., 2

09-FD

-24St

ephe

ns, D

., 11

4-AA-1

8St

ephe

ns, J

., 19

1-AMT

-11/G

T-11

Stev

ens,

M., 2

74-AT

IO-24

Stoe

llinge

r, M.,

172-C

FD-20

Stoh

r, M.,

266-A

MT-13

/GT-1

3St

oll, A

., 24

0-ATIO

-23, 2

76-AT

IO-26

Ston

e, C.,

203

-CFD-2

3, 3

02-CF

D-32

Storo

zhev

, D.,

216-T

P-10/

PDL-1

0St

ouffe

r, V.,

65-M

ST-3,

142

-MST

-6, 1

99-AT

IO-20

, 2

75-AT

IO-25

Stou

t, T.,

40-A

A-9St

rande

, P.,

237-A

SE-3

Stran

gfeld,

C., 1

01-FD

-12St

raub,

S., 9

1-ATIO

-9St

reett,

C., 2

33-AP

A-25

Strga

nac,

T., 9

-AFM-

2, 1

24-AP

A-15,

270

-APA-3

2St

uchli

k, D.

, 200

-BAL-2

Stue

rmer,

A., 1

62-AP

A-19

Su, H

., 25

2-MAO

-9Su

, L.,

181-P

DL-9/

TP-8

Su, W

., 25

-FD-1,

105

-MST

-5Su

bbara

o, K.,

48-A

PA-6,

157

-AFM-

9Su

bbare

ddy,

P., 2

44-CF

D-29,

246

-FD-27

, 278

-FD-30

Subra

mania

n, N.

, 3-AA

-1, 1

52-AA

-22Su

brama

nyam

, A.,

153-A

A-23

Suda

ni, J.

, 205

-CFD-2

5Su

i, D.,

65-M

ST-3

Sun,

D., 1

6-ATIO

-1Su

n, H.

, 95-C

FD-9

Sun,

Y., 4

-AA-2,

6-AA

-4, 3

1-MST

-2, 2

48-FD

-29Su

n, Z.,

130

-CFD-1

3Su

ndstr

öm, E

., 11

2-AA-1

6Su

ñol, A

., 25

0-LTA

-1Su

raj N

andig

anah

alli, J

., 31

-MST

-2Su

rakitb

anha

rn, C.

, 166

-ATIO

-17Su

ryadi,

A., 1

15-AA

-19Su

ryaku

mar, V

., 9-A

FM-2,

124

-APA-1

5, 2

70-AP

A-32

Surzh

ikov,

S., 69

-TP-4,

193-A

PA-21

, 216

-TP-10

/PDL

-10Su

tliff,

D., 7

8-AA-1

2, 1

16-AA

-20Su

zuki,

K., 3

3-PDL

-1/FD

-5, 8

9-APA

-11, 1

02-FD

-13Su

zuki,

T., 6

8-TP-3

Swam

inatha

n Gop

alan,

K., 2

88-TP

-13Sw

ann,

M., 2

93-AC

D-8Sw

iering

a, K.,

18-A

TIO-3,

298

-ATIO

-27Sw

ift, S

., 11

3-AA-1

7Sy

tsma,

M., 1

58-AM

T-9/G

T-9Sz

melte

r, J.,

163-A

SE-1

Taba

nli, H

., 17

4-FD-2

0Ta

ha, H

., 23

6-APA

-28Ta

i, J.,

308-M

AO-13

130

Auth

or/S

essio

n Ch

air In

dex

Taira

, K.,

101-F

D-12,

136

-FD-15

, 248

-FD-29

Taka

hash

i, T.,

117-A

CD-3,

190

-ACD-5

, 232

-ACD-6

, 2

86-PD

L-13,

293

-ACD-8

Taka

ishi, T

., 23

0-AA-3

5Ta

kaki,

R., 2

3-CFD

-3Ta

kaya

nagi,

H.,

69-TP

-4Ta

l, E.,

124-A

PA-15

Tam,

C., 4

1-AA-1

0, 6

7-PDL

-3, 1

85-AA

-26Ta

maki,

Y., 2

41-CF

D-26

Tama

skar,

S.,

239-A

TIO-22

Tamb

a, T.,

138

-FD-17

Tamu

ra, M

., 14

4-PDL

-7Ta

mura,

T., 1

82-TP

-9Ta

naka

, Y.,

182-T

P-9Ta

ng, C

., 16

2-APA

-19Ta

ng, H

., 17

-ATIO

-2, 1

45-TP

-7, 1

73-FD

-19Ta

ng, S

., 10

5-MST

-5Ta

ng, W

., 26

7-APA

-29Ta

ng, Y

., 10

5-MST

-5Ta

nner,

P., 1

20-AM

T-7/G

T-7Ta

nno,

H., 6

9-TP-4

Tao,

F., 7

-AA-5

Tao,

G., 1

27-AT

IO-13

Tao,

L., 2

04-CF

D-24,

245

-CFD-3

0Ta

pken

, U.,

173-F

D-19

Taqu

in, G

., 83

-AFM-

5Ta

rter, J

., 14

0-ITA

R-2Ta

tsuka

wa, T

., 11

4-AA-1

8Ta

verne

tti, W

., 27

8-FD-3

0Ta

y, W.

, 22-C

FD-2

Taylo

r, C.,

275-A

TIO-25

Taylo

r, L.,

15-AP

A-4, 2

97-AP

A-37

Taylo

r, N.,

301-C

FD-31

Taylo

r, S.,

273-A

SE-5

Tchatc

huen

g Kam

megn

e, M.

, 66-M

ST-4

Tchipe

v, N.

, 237

-ASE-3

Teare

, D.,

214-M

ST-9

Temm

ler, C

., 11

3-AA-1

7Te

nsud

a, B.

, 304

-CFD-3

4Te

rakad

o, D.

, 169

-CFD-1

7Te

rnisie

n, L.,

18-A

TIO-3

Terra

col, M

., 15

4-AA-2

4, 2

29-AA

-34Te

rraza

s-Sali

nas,

I., 1

08-TP

-5Te

sfahu

negn

, Y.,

307-M

AO-12

Testa

, C.,

263-A

A-41

Teste

r, B.,

186-A

A-27

Thais

s, C.,

83-A

FM-5

Tham

sen,

P., 1

73-FD

-19Th

aniga

iaras

u, S.

, 50-A

PA-8

Thek

inen,

J., 5

2-ATIO

-6Th

eodo

re, C.

, 281

-GEPC

-1Th

eunis

sen,

R., 3

-AA-1

Thiel

e, F.,

112

-AA-16

, 306

-CFD-3

6Th

ielec

ke, F

., 8-A

FM-1

Thier

ry, M

., 10

8-TP-5

Thipy

opas

, C.,

234-A

PA-26

Thob

ois, L

., 27

2-ASE

-4, 2

98-AT

IO-27

Thom

as, J

., 30

7-MAO

-12Th

omps

on, D

., 23

-CFD-3

, 97-C

FD-11

Thom

pson

, F.,

104-M

AO-3

Thom

pson

, R.,

67-PD

L-3, 2

44-CF

D-29

Thom

pson

, T.,

42-AC

D-1Th

ornbe

r, B.,

306-C

FD-36

Thorn

e, J.,

243

-CFD-2

8Th

orsen

, A.,

83-AF

M-5

Thum

iah, D

., 86

-AMT-6

/GT-6

Thuro

w, B

., 67

-PDL-3

Tian,

P., 4

3-AFM

-3Tia

n, Y.,

44-A

FM-4

Tian,

Z., 2

44-CF

D-29

Tibor,

E., 2

12-M

AO-6

Tilma

nn, C

., 27

1-APA

-33Tim

me, S

., 96

-CFD-1

0Tim

ofeev

, E.,

102-F

D-13

Ting,

E., 1

24-AP

A-15

Tisso

t, G.

, 5-AA

-3Tit

arev,

V., 1

87-AA

-28Tit

tswort

h, J.,

237

-ASE-3

Tkac

henk

o, O.

, 31-M

ST-2

Tkac

ik, P.

, 282

-LTA-2

Toba

lske,

B., 1

00-FD

-11To

giti, V

., 17

2-CFD

-20To

lomell

i, L.,

181-P

DL-9/

TP-8

Toma

c, M.

, 160

-APA-1

7To

ng, F

., 15

1-AA-2

1, 2

60-AA

-38To

ng, O

., 21

-CFD-1

Tong

, W.,

176-M

AO-5

Torde

ux, S

., 26

2-AA-4

0To

ropov

, V.,

5-AA-3

, 251

-MAO

-8To

rres,

S., 9

2-ATIO

-10To

ubin,

H.,

161-A

PA-18

Tous

saint

, C.,

83-AF

M-5

Tous

saint

, S.,

300-A

TIO-29

Town

e, A.,

5-AA

-3Tra

n, D.

, 99-F

D-10

Tran,

L., 1

65-AT

IO-16

Trani,

A., 3

00-AT

IO-29

Treve

, V.,

51-AT

IO-5

Trevin

o, L.,

214

-MST

-9Tri

nh, K

., 12

4-APA

-15Tri

tschle

r, J.,

43-AF

M-3

Trolin

ger, J

., 11

-AMT-2

/GT-2

Trollin

ger, L

., 50

-APA-8

Trope

a, C.,

50-A

PA-8,

271

-APA-3

3, 2

97-AP

A-37

Troxe

l, S.,

163-A

SE-1

Trujill

o, A.,

199

-ATIO

-20Tru

ong,

A., 2

64-AA

-42Tsa

i, C.,

304-C

FD-34

Tsao,

S., 9

2-ATIO

-10, 1

97-AT

IO-18

Tsotsk

as, C

., 29

-MAO

-1Tsu

boku

ra, M

., 27

0-APA

-32Tsu

chiya

, T.,

51-AT

IO-5

Tsutsu

mi, S

., 23

-CFD-3

Tufts

, M.,

137-F

D-16

Tuins

tra, M

., 11

5-AA-1

9Tu

le, C.

, 157

-AFM-

9Tu

na, B

., 10

1-FD-1

2, 2

48-FD

-29Tu

rchi, A

., 34

-TP-1

Turow

ski, M

., 85

-AMT-5

/GT-5

Tuttle

, J.,

167-B

AL-1

Tyag

i, A.,

198-A

TIO-19

, 300

-ATIO

-29Ty

sell,

L., 1

54-AA

-24Ty

son,

W., 9

7-CFD

-11Ud

din, M

., 30

6-CFD

-36Ue

ckerm

ann,

M., 3

3-PDL

-1/FD

-5Ue

hara,

A., 3

1-MST

-2Uk

eiley

, L.,

48-AP

A-6, 1

95-AP

A-23,

248

-FD-29

Ulbric

h, N.

, 294

-AMT-1

4/GT

-15Ull

rich,

W., 4

1-AA-1

0, 1

85-AA

-26Un

derbr

ink, J

., 18

6-AA-2

7, 2

62-AA

-40Un

derw

ood,

M., 2

99-AT

IO-28

Upalk

ar, B

., 14

5-TP-7

Ura,

H., 2

30-AA

-35Ur

nes,

J., 4

9-APA

-7Va

lavan

is, K.

, 88-A

PA-10

Valen

tini, P

., 25

6-TP-1

2Va

lla, M

., 27

2-ASE

-4va

n Bus

sel, G

., 12

2-APA

-13, 2

79-FD

-31va

n de V

en, T

., 23

0-AA-3

5va

n der

Velde

n, W.

, 38-A

A-7va

n Kuij

k, J.,

37-A

A-6va

n Oud

heus

den,

B., 97

-CFD-1

1, 13

8-FD-1

7, 20

8-FD-2

3va

n Too

ren, M

., 64

-MAO

-2Va

n Treu

ren, K

., 15

-APA-4

Van T

reuren

, R.,

250-L

TA-1

van Z

uijlen

, A.,

38-AA

-7, 1

22-AP

A-13

Vand

en, K

., 27

0-APA

-32Va

nderw

el, C.

, 3-AA

-1, 3

8-AA-7

, 152

-AA-22

Vans

tone,

L., 1

74-FD

-20Va

nValk

enbu

rg, R.

, 237

-ASE-3

Varga

, D.,

200-B

AL-2

Varga

s, A.,

167

-BAL-1

Varga

s, M.

, 196

-ASE-2

Vargh

ese,

P., 2

88-TP

-13Va

rgo, E

., 27

5-ATIO

-25Va

rma,

D., 1

25-AP

A-16

Varne

y, M.

, 31-M

ST-2

Vasci

k, P.,

52-A

TIO-6

Vash

ishtha

, A.,

102-F

D-13

Vasile

, M.,

214-M

ST-9

Vassa

ux, D

., 16

7-BAL

-1Va

tsa, V

., 13

3-CFD

-16, 2

59-AA

-37Va

ugha

n, W.

, 196

-ASE-2

, 273

-ASE-5

Vaux

, S.,

249-F

T-1Ve

karia

, S.,

235-A

PA-27

Veldh

uis, L

., 37

-AA-6,

269

-APA-3

1Ve

muri,

S., 2

34-AP

A-26

Vene

l, S.,

167-B

AL-1

Venk

atach

ari, B

., 19

3-APA

-21, 2

11-FD

-26Ve

nkata

krish

nan,

L., 2

27-AA

-32Ve

nkate

sh, B

., 39

-AA-8

Venk

atram

an, S

., 50

-APA-8

Venu

ti, J.,

51-A

TIO-5

Vera,

J., 5

-AA-3

Vergi

ne, F

., 20

5-CFD

-25Ve

rmeir

e, B.

, 130

-CFD-1

3, 2

02-CF

D-22

Verm

illion

, C.,

282-L

TA-2

Vey,

S., 2

6-FD-2

, 297

-APA-3

7Vil

adeg

ut, A.

, 216

-TP-10

/PDL

-10Vil

la, C.

, 65-M

ST-3

Vince

nt, P.

, 130

-CFD-1

3, 2

02-CF

D-22,

242

-CFD-2

7Vis

bal, M

., 101

-FD-12

, 102

-FD-13

, 170

-CFD-1

8,

208

-FD-23

, 255

-PDL-1

2, 26

6-AMT

-13/G

T-13,

2

70-AP

A-32

Viswa

nath,

K., 2

33-AP

A-25

Vitale

, S.,

133-C

FD-16

Vitzil

aios,

N., 8

8-APA

-10Vo

, H.,

60-FD

-6/PD

L-2Vo

s, R.,

42-A

CD-1

Vrcho

ta, P.

, 233

-APA-2

5Vu

, B.,

56-CF

D-6Vu

cinic,

D.,

250-L

TA-1

Vuillo

t, F.,

39-A

A-8, 2

59-AA

-37Wa

che,

L., 5

2-ATIO

-6Wa

dding

ton, M

., 82

-ACD-2

Wagle

, N.,

157-A

FM-9

Wagn

er, C.

, 252

-MAO

-9Wa

gner,

J., 6

2-FD-8

, 175

-FD-22

Wagn

ild, R

., 10

3-ITA

R-1, 2

56-TP

-12Wa

indim

, M.,

245-C

FD-30

Waith

e, K.,

14-A

PA-3,

89-A

PA-11

Waka

yama

, S.,

267-A

PA-29

Wake

field,

D.,

167-B

AL-1

Walke

r, A.,

88-AP

A-10,

214

-MST

-9Wa

lker, M

., 50

-APA-8

Wall,

A., 4

0-AA-9

Wan,

Y., 6

5-MST

-3, 2

75-AT

IO-25

Wang

, C.,

161-A

PA-18

, 213

-MAO

-7, 2

69-AP

A-31

Wang

, F.,

85-AM

T-5/G

T-5, 1

91-AM

T-11/

GT-11

, 2

37-AS

E-3, 2

95-AP

A-34

Wang

, G.,

265-A

CD-7

Wang

, H.,

84-AF

M-6,

244

-CFD-2

9Wa

ng, J

., 33

-PDL-1

/FD-5

, 84-A

FM-6,

180

-PDL-8

/AP

A-20,

187

-AA-28

, 271

-APA-3

3Wa

ng, K

., 18

7-AA-2

8, 2

55-PD

L-12

Wang

, L.,

151-A

A-21,

260

-AA-38

Wang

, M.,

187-A

A-28,

255

-PDL-1

2, 2

63-AA

-41,

265

-ACD-7

Wang

, P.,

128-A

TIO-14

Wang

, Q.,

80-AA

-14, 1

73-FD

-19, 2

02-CF

D-22,

2

41-CF

D-26

Wang

, S.,

62-FD

-8, 1

19-AF

M-8

Wang

, X.,

122-A

PA-13

, 132

-CFD-1

5, 2

50-LT

A-1,

260

-AA-38

Wang

, Y., 9

-AFM-

2, 22

-CFD-2

, 30-M

ST-1,

131-C

FD-14

, 2

13-M

AO-7

Wang

, Z., 2

3-CFD

-3, 25

-FD-1,

56-CF

D-6, 9

9-FD-1

0,

130

-CFD-1

3, 13

8-FD-1

7, 17

0-CFD

-18, 2

42-CF

D-27,

303

-CFD-3

3Wa

nke,

C., 2

75-AT

IO-25

Ward,

C., 1

37-FD

-16Wa

tanab

e, Y.,

33-P

DL-1/

FD-5,

102

-FD-13

Watso

n, J.,

104

-MAO

-3Wa

tson,

W., 7

-AA-5,

116

-AA-20

, 262

-AA-40

Weav

er, A.

, 35-T

P-2We

bb, N

., 33

-PDL-1

/FD-5

Webs

ter, R

., 12

2-APA

-13We

i, Q.,

7-AA-5

Wei ta

o, Z.,

303

-CFD-3

3We

instei

n, R.,

50-A

PA-8

Weiss

, B.,

91-AT

IO-9

Weiss

, M.,

239-A

TIO-22

Wells,

D.,

42-AC

D-1We

n, Y.,

250

-LTA-1

Wend

orff,

A., 2

12-M

AO-6,

308

-MAO

-13We

ng, H

., 68

-TP-3

Werne

r, T.,

151-A

A-21

Werne

t, M.

, 227

-AA-32

Werte

r, N.,

29-M

AO-1

West,

A., 3

9-AA-8

, 230

-AA-35

West,

J., 1

71-CF

D-19

West,

T., 5

8-CFD

-8We

y, P.,

45-A

MT-3/

GT-3,

47-A

PA-5

Wha

len, E

., 24

8-FD-2

9, 2

71-AP

A-33

Whe

aton,

B., 1

03-IT

AR-1,

278

-FD-30

Whit

e, E.,

158

-AMT-9

/GT-9

, 209

-FD-24

, 267

-APA-2

9W

hite,

J., 1

33-CF

D-16

Whit

e, M.

, 67-P

DL-3,

255

-PDL-1

2W

hite,

T., 6

8-TP-3

, 108

-TP-5,

217

-TP-11

Wiar

t, L.,

13-A

PA-2

131

Auth

or/S

essio

n Ch

air In

dex

Wiel

and,

F., 1

98-AT

IO-19

, 300

-ATIO

-29W

ilcoxe

n, M.

, 17-A

TIO-2

Wild

, J.,

125-A

PA-16

, 230

-AA-35

Wild

er, M

., 18

2-TP-9

Wild

er, W

., 91

-ATIO

-9W

ildsch

ek, A

., 64

-MAO

-2W

ilkins

on, S

., 24

8-FD-2

9W

illiam

s, A.,

35-T

P-2W

illiam

s, D.

, 60-F

D-6/P

DL-2,

101

-FD-12

, 136

-FD-15

Willi

ams,

N., 2

44-CF

D-29

Willi

amsch

en, M

., 26

3-AA-4

1W

ilson,

A., 1

98-AT

IO-19

Wine

r, E.,

104-M

AO-3,

141

-MAO

-4, 1

76-M

AO-5,

2

12-M

AO-6

Wing

, A.,

239-A

TIO-22

Wing

, D.,

299-A

TIO-28

Wink

el, R.

, 60-F

D-6/P

DL-2

Wint

er, M

., 10

8-TP-5

, 121

-AMT-8

/FD-1

4/TP

-6/GT

-8,

181

-PDL-9

/TP-8

Wint

zer, M

., 14

-APA-3

Wisd

a, D.

, 114

-AA-18

, 187

-AA-28

Wisn

iewsk

i, C.,

15-AP

A-4W

isniew

ski, N

., 15

-APA-4

Wiss

a, A.,

12-A

PA-1

Wiss

ink, A

., 20

1-CFD

-21W

itherd

en, F

., 13

0-CFD

-13, 2

02-CF

D-22

Witti

g, S.

, 46-A

MT-4/

GT-4

Wlez

ien, R

., 13

7-FD-1

6Wo

hlbran

dt, A.

, 41-A

A-10

Wolf,

W., 3

8-AA-7

, 41-A

A-10,

189-A

A-30,

260-A

A-38,

2

70-AP

A-32

Woo,

G., 2

95-AP

A-34

Woop

en, M

., 95

-CFD-9

Wortm

ann,

A., 4

2-ACD

-1W

ray, A

., 24

-CFD-4

Wray

, T.,

139-F

D-18,

211

-FD-26

Wrig

ht, M

., 85

-AMT-5

/GT-5

Wrig

hton,

C., 2

27-AA

-32W

ronow

ski, K

., 28

0-FT-2

/GT-1

4W

u, D.

, 213

-MAO

-7W

u, J.,

25-F

D-1, 2

65-AC

D-7W

u, X.

, 99-F

D-10

Wu,

Y., 1

81-PD

L-9/T

P-8W

u, Z.,

250

-LTA-1

Wün

sch, O

., 22

-CFD-2

, 96-C

FD-10

Wys

zogro

dzki,

A., 1

63-AS

E-1Xia

, Y.,

55-CF

D-5Xia

ng, J

., 47

-APA-5

Xiao,

F., 1

30-CF

D-13

Xiao,

T., 9

7-CFD

-11Xia

o, Y.,

296

-APA-3

5Xia

ojie,

Q., 1

05-M

ST-5

Xie, J

., 65

-MST

-3Xie

, K.,

191-A

MT-11

/GT-1

1Xu

, F.,

57-CF

D-7Xu

, J.,

116-A

A-20,

241

-CFD-2

6Xu

, K.,

107-P

DL-4,

143

-PDL-6

Xu, Z

., 10

5-MST

-5, 2

41-CF

D-26

Xue,

M., 1

6-ATIO

-1Ya

dlin,

Y., 2

71-AP

A-33

Yagiz

, B.,

304-C

FD-34

Yakh

ina, G

., 79

-AA-13

Yako

vlev,

P., 2

28-AA

-33Ya

lin, A

., 10

7-PDL

-4Ya

mada

, K.,

144-P

DL-7

Yama

gishi,

K., 1

82-TP

-9Ya

mamo

to, K.

, 23-C

FD-3,

229

-AA-34

, 230

-AA-35

Yama

shita

, R.,

89-AP

A-11

Yama

uchi,

G.,

192-A

MT-12

/GT-1

2Ya

moun

i, S.,

270-A

PA-32

Yan,

F., 1

28-AT

IO-14

Yan,

G., 1

31-CF

D-14

Yan,

K., 2

50-LT

A-1Ya

n, W.

, 178

-MST

-8Ya

n, X.

, 180

-PDL-8

/APA

-20Ya

ng, C

., 14

5-TP-7

Yang

, D.,

204-C

FD-24

Yang

, H.,

197-A

TIO-18

, 241

-CFD-2

6, 3

04-CF

D-34

Yang

, M.,

119-A

FM-8

Yang

, T.,

250-L

TA-1

Yang

, W.,

105-M

ST-5

Yang

, X.,

98-CF

D-12,

171

-CFD-1

9Ya

ng, Y

., 4-A

A-2, 6

-AA-4,

97-C

FD-11

, 162

-APA-1

9,

178

-MST

-8, 2

69-AP

A-31

Yang

, Z.,

159-A

MT-10

/GT-1

0, 2

68-AP

A-30

Yao,

C., 5

7-CFD

-7, 1

88-AA

-29Ya

o, H.

, 6-AA

-4, 1

15-AA

-19, 1

54-AA

-24Ya

o, W.

, 56-C

FD-6

Yarus

evyc

h, S.

, 100

-FD-11

, 208

-FD-23

Yauw

enas

, Y.,

115-A

A-19

Yayla

, S.,

25-FD

-1Ya

zdan

i, S.,

229-A

A-34

Ye, C

., 19

8-ATIO

-19Ye

chou

t, T.,

64-M

AO-2

Yee,

H., 2

4-CFD

-4Ye

e, P.,

108

-TP-5

Yen,

C., 7

8-AA-1

2Ye

ste-O

jeda,

O., 2

15-M

ST-10

Yi, S

., 12

-APA-1

Yode

r, D.,

58-CF

D-8, 1

20-AM

T-7/G

T-7Yo

koka

wa, Y

., 23

0-AA-3

5Yo

on, S

., 13

6-FD-1

5Yo

shida

, S.,

43-AF

M-3

Yosh

ikawa

, E.,

298-A

TIO-27

Yosh

ino, T

., 28

6-PDL

-13Yo

ung,

D., 2

5-FD-1

Youn

g, E.,

200

-BAL-2

Youn

g, L.,

117

-ACD-3

Youn

g, R.,

281

-GEPC

-1Yo

ung,

S., 1

66-AT

IO-17

Youn

g, T.,

48-A

PA-6,

102

-FD-13

Yu, H

., 15

9-AMT

-10/G

T-10

Yu, J

., 12

2-APA

-13Yu

, L.,

145-T

P-7Yu

, M.,

243-C

FD-28

, 279

-FD-31

Yu, S

., 26

9-APA

-31Yu

, W.,

7-AA-5

Yuan

, C.,

248-F

D-29

Yuan

-pei, S

., 25

2-MAO

-9Yu

ceil,

K., 1

74-FD

-20Yu

e, C.,

280

-FT-2/

GT-14

Yue,

Z., 6

5-MST

-3Za

chos

, P.,

270-A

PA-32

Zaidi

, T.,

52-AT

IO-6

Zajac

zkow

ski, F

., 14

0-ITA

R-2Za

karia

, M.,

236-A

PA-28

Zama

n, K.,

189

-AA-30

Zamb

rano,

J., 2

15-M

ST-10

Zane

tte, J

., 24

9-FT-1

Zang

, T.,

308-M

AO-13

Zawo

dny,

N., 1

55-AA

-25Za

ytsev

, M.,

187-A

A-28,

189

-AA-30

Zehn

er, P.

, 154

-AA-24

Zelen

ak, D

., 14

3-PDL

-6Ze

linsk

i, S.,

16-AT

IO-1

Zeng

, D.,

239-A

TIO-22

Zeng

, Q.,

30-M

ST-1

Zerob

in, S

., 15

1-AA-2

1Zh

a, G.

, 90-A

PA-12

, 125

-APA-1

6Zh

ai, Q

., 67

-PDL-3

Zhai,

Z., 2

15-M

ST-10

Zhan

g, B.

, 16-A

TIO-1

Zhan

g, C.,

253

-MST

-11, 2

95-AP

A-34

Zhan

g, D.

, 180

-PDL-8

/APA

-20, 2

71-AP

A-33

Zhan

g, F.,

47-A

PA-5

Zhan

g, G.

, 57-C

FD-7

Zhan

g, H.

, 208

-FD-23

Zhan

g, J.,

65-M

ST-3,

203

-CFD-2

3, 2

65-AC

D-7Zh

ang,

L., 2

15-M

ST-10

Zhan

g, M.

, 5-AA

-3Zh

ang,

S., 3

03-CF

D-33

Zhan

g, X.

, 7-AA

-5, 2

2-CFD

-2, 2

5-FD-1

, 112

-AA-16

, 1

13-AA

-17, 1

52-AA

-22, 2

05-CF

D-25,

214

-MST

-9,

259

-AA-37

, 263

-AA-41

Zhan

g, Y.,

31-M

ST-2,

122

-APA-1

3, 1

98-AT

IO-19

, 2

48-FD

-29

Zhan

g, Z.,

46-A

MT-4/

GT-4,

58-C

FD-8,

67-P

DL-3,

1

38-FD

-17, 1

81-PD

L-9/T

P-8Zh

ao, C

., 12

8-ATIO

-14Zh

ao, D

., 11

6-AA-2

0, 1

62-AP

A-19

Zhao

, J.,

33-PD

L-1/F

D-5Zh

ao, K

., 16

1-APA

-18, 2

00-BA

L-2Zh

ao, Q

., 19

4-APA

-22, 2

41-CF

D-26

Zhao

, W.,

51-AT

IO-5

Zhao

, X.,

303-C

FD-33

Zhao

, Y.,

35-TP

-2, 1

45-TP

-7Zh

elonk

in, M

., 31

-MST

-2Zh

elonk

in, V.

, 31-M

ST-2

Zhen

g, J.,

185

-AA-26

Zhen

g, Y.,

44-A

FM-4

Zhen

g, Z.,

43-AF

M-3,

62-FD

-8, 24

6-FD-2

7, 25

0-LTA-

1,

261

-AA-39

, 272

-ASE-4

Zhon

g, X.

, 209

-FD-24

Zhou

, B.,

79-AA

-13, 2

83-M

AO-10

Zhou

, H.,

250-L

TA-1

Zhou

, J.,

208-F

D-23

Zhou

, L.,

7-AA-5

Zhou

, P.,

250-L

TA-1

Zhu,

J., 2

5-FD-1

Zhu,

M., 2

50-LT

A-1Zh

u, T.,

69-T

P-4Zie

ntarsk

i, L.,

191-A

MT-11

/GT-1

1Zim

merm

an, J

., 10

7-PDL

-4Zin

gg, D

., 13

2-CFD

-15, 1

69-CF

D-17,

204

-CFD-2

4,

242

-CFD-2

7, 2

67-AP

A-29

Zishk

a, E.,

182

-TP-9

Zocca

, M.,

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Technical ZonesAVIATION 2015 Technical Zones (see Venue Map)

The technical program, which consists of more than 1,500 papers in over 20 technical tracks, has been placed within the hotel in zones to keep related session topics and technical conferences together. Please visit one of the zones to listen to a technical paper that is of interest to you!

Zone 121st AIAA/CEAS Aeroacoustics Conference 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference15th AIAA Aviation Technology, Integration, and Operations Conference AIAA Balloon Systems Conference AIAA Flight Testing Conference 22nd AIAA Lighter-Than-Air Systems Technology Conference AIAA Modeling and Simulation Technologies Conference 45th AIAA Thermophysics Conference

Zone 215th AIAA Aviation Technology, Integration, and Operations Conference AIAA Complex Aerospace Systems Exchange45th AIAA Fluid Dynamics Conference 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 46th AIAA Plasmadynamics and Lasers Conference45th AIAA Thermophysics Conference

Zone 333rd AIAA Applied Aerodynamics Conference

Zone 431st AIAA Aerodynamic Measurement Technology and Ground Testing ConferenceAIAA Atmospheric Flight Mechanics Conference 7th AIAA Atmospheric and Space Environments Conference AIAA Complex Aerospace Systems Exchange22nd AIAA Computational Fluid Dynamics Conference45th AIAA Fluid Dynamics Conference


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Hilton Anatole

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aiaa-aviation.org/FutureEvents

Reserve your sponsorship and exhibit space today!Contact Tobey Jackson, 703.264.7570 or [email protected]

2O1613–17 JUNE 2016 WASHINGTON, D.C.

See You Next Year!We hope that you learned something new, achieved your goals, caught up with colleagues, and made new connections. We look forward to seeing you next year in the Nation’s capital!

32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference

34th AIAA Applied Aerodynamics Conference

AIAA Atmospheric Flight Mechanics Conference

8th AIAA Atmospheric and Space Environments Conference

16th AIAA Aviation Technology, Integration, and Operations Conference

AIAA Flight Testing Conference

8th AIAA Flow Control Conference

46th AIAA Fluid Dynamics Conference

17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

AIAA Modeling and Simulation Technologies Conference

47th AIAA Plasmadynamics and Lasers Conference

46th AIAA Thermophysics Conference

It’s the perfect place to combine business and family fun. It is home to Congress, NASA Headquarters, NASA Goddard, NOAA, the FAA, NSSC, NRL, and the Pentagon. There are more than 100 free things to do in Washington, D.C.— including most of the Smithsonian (with TWO air and space museums, art galleries, and the National Zoo) and scores of famous landmarks—most within walking distance of one another.

Technical Conferences

Why Washington, D.C.?

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