AIAA JOURNAL OF PROPULSION AND POWER · Conceptual Study of a Combined-Cycle Engine for an...

AIAA JOURNAL OF PROPULSION AND POWER

http://www.aiaa.org/Research/index.hfm?res=13

Volume 19 Number 5 September 2003

Combustion Dynamics in Lean-Premixed Prevaporized (LPP) GasTurbines

Introduction: Combustion Dynamics in Lean-Premixed Prevaporized(LPP) Gas Turbines

721

Tim Lieuwen; Keith McManus

Combustion Dynamics and Instabilities: Elementary Coupling andDriving Mechanisms

722

Sébastien Ducruix; Thierry Schuller; Daniel Durox; Sébastien Candel

Experimental Diagnostics for the Study of Combustion Instabilities inLean Premixed Combustors

735

J. G. Lee; D. A. Santavicca

Acoustic Analysis of Gas Turbine Combustors 751

Ann P. Dowling; Simon R. Stow

Modeling Premixed Combustion-Acoustic Wave Interactions: A Review 765

T. Lieuwen

Large-Eddy Simulation of Combustion Dynamics of Lean-PremixedSwirl-Stabilized Combustor

782

Ying Huang; Hong-Gye Sung; Shih-Yang Hsieh; Vigor Yang

Passive Control of Combustion Dynamics in Stationary Gas Turbines 795

Geo A. Richards; Douglas L. Straub; Edward H. Robey

Factors Affecting the Control of Unstable Combustors 811

Jeffrey M. Cohen; Andrzej Banaszuk

Challenges and Progress in Controlling Dynamics in Gas TurbineCombustors

822

H. C. Mongia; T. J. Held; G. C. Hsiao; R. P. Pandalai

Full-length Papers

Time-Averaged Gradient Control of Thermoacoustic Instabilities 830

Michael A. Vaudrey; William T. Baumann; William R. Saunders

Premixed Flame Kinematics in a Longitudinal Acoustic Field 837

Doh-Hyoung Lee; Tim C. Lieuwen

Atomic Emission Spectrometry for Profiling High Temperatures inCombustion System

847

Shigeo Yatsu; Hiroyuki Oyama; Takunari Mizuno; Hideharu Kimura;Kuniyuki Kitagawa; Naoyuki Kayukawa

Ignition Characteristics of Methane and Hydrogen Using a PlasmaTorch in Supersonic Flow

853

Tomoaki Kitagawa; Atsushi Moriwaki; Koichi Murakami; Kenichi Takita;Goro Masuya

Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane 859

Takeshi Kanda; Kenji Kudo

Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator UsingComputation and Experiment

868

Birgit U. Reinartz; Carsten D. Herrmann; Josef Ballmann; Wolfgang W.Koschel

Effects of Injection Configuration on Performance of a StagedSupersonic Combustor

876

Sadatake Tomioka; Kan Kobayashi; Kenji Kudo; Atsuo Murakami;Tohru Mitani

Fuel Injection and Flame Stabilization in a Liquid-Kerosene-FueledSupersonic Combustor

885

G. Yu; J. G. Li; X. Y. Chang; L. H. Chen; C. J. Sung

Magnetohydrodynamic Power Generation Experiments with Fuji-1Blowdown Facility

894

Y. Okuno; T. Okamura; T. Suekane; H. Yamasaki; S. Kabashima; S.Shioda

Some Aspects of Chemical Kinetics in Chapman-Jouguet Detonation:Induction Length Analysis

901

Tianfeng Lu; Chung K. Law; Yiguang Ju

Partial Fuel Filling in Pulse Detonation Engines 908

Chiping Li; K. Kailasanath

Tailored Fuel Injection for Pulsed Detonation Engines via FeedbackControl

917

Alberto Aliseda; Kartik B. Ariyur; Olivier Sarrazin; Juan C. Lasheras;Miroslav Krstic

Two-Dimensional Compressible Non-Acoustic Modeling of StirlingMachine-Type Components

922

Roy C. Tew Jr; Mounir B. Ibrahim

Jet Engine Gas-Path Measurement Filtering Using Center WeightedIdempotent Median Filters

930

Ranjan Ganguli

Dynamic and Nonlinear Simulation of Liquid-Propellant Engines 938

H. Karimi; A. Nassirharand

Multi-Element Unstructured Methodology for Analysis ofTurbomachinery Systems

945

Vineet Ahuja; Jeremy D. Shipman; S. Arunajatesan; Ashvin Hosangadi

Numerical Parameter Studies of Ion-Thruster-Beam Neutralization 953

Carsten Othmer; Karl-Heinz Glassmeier; Uwe Motschmann; IngoRichter

Development of a Finite Element-Based Hall-Thruster Model 964

Subrata Roy; B. P. Pandey

Volume 19 Number 4 July 2003

Full-length Papers

Analysis of Inducer Recirculating Inlet Flow 521

François Bario; Thierry M. Faure; Emmanuel Jondeau; Jean-LucNormand; Jean-Michel Nguyen Duc

Theoretical Performance of a Magnetohydrodynamic-Bypass ScramjetEngine with Nonequilibrium Ionization

529

Chul Park; David W. Bogdanoff; Unmeel B. Mehta

Deceleration of Supersonic Plasma Flow by an Applied Magnetic Field 538

Sergei V. Bobashev; Yurii P. Golovachov; David M. Van Wie

Computational Fluid Dynamics Analysis of the Central Institute ofAviation Motors/NASA Scramjet

547

Carlos G. Rodriguez

System Performance and Thermodynamic Cycle Analysis ofAirbreathing Pulse Detonation Engines

556

Yuhui Wu; Fuhua Ma; Vigor Yang

Pulse Detonation Engine Characterization and Control Using TunableDiode-Laser Sensors

568

Daniel W. Mattison; Christopher M. Brophy; Scott T. Sanders; Lin Ma;Kevin M. Hinckley; Jay B. Jeffries; Ronald K. Hanson

Detonation Initiation by Controlled Triggering of Electric Discharges 573

S. M. Frolov; V. Y. Basevich; V. S. Aksenov; S. A. Polikhov

Constant-Frequency Hypervelocity Slings 581

D. A. Tidman

Measurements and Simulation of Orifice Flow for MicropropulsionTesting

588

A. A. Alexeenko; S. F. Gimelshein; D. A. Levin; A. D. Ketsdever; M. S.Ivanov

One-Dimensional Hollow Cathode Model 595

Ira Katz; John R. Anderson; James E. Polk; John R. Brophy

Ignition Delay for Jet Propellant 10/Air and Jet Propellant 10/High-Energy Density Fuel/Air Mixtures

601

David W. Mikolaitis; Corin Segal; Abhilash Chandy

Numerical Simulation of Ion Beam Optics for Multiple-Grid Systems 607

Yoshinori Nakayama; Paul J. Wilbur

Combustion and Thermal Studies on Al/Ti/Ni/Zr Composite ModifiedDouble-Base Systems

614

C. N. Divekar; S. N. Asthana; Haridwar Singh

Erosive Burning of Ammonium Perchlorate/Hydroxyl-Terminated-Polybutadiene Propellants Under Supersonic Crossflows

623

S. Krishnan; K. K. Rajesh

Characteristics of Liquid Film and Spray Injected from Swirl CoaxialInjector

632

Takao Inamura; Hiroshi Tamura; Hiroshi Sakamoto

Analytical and Experimental Studies of Tile-Shaped Aerospike Nozzles 640

Wu-Ye Dai; Yu Liu; Xian-Chen Cheng; Bin Ma

Closed-Loop Vectoring Control of a Turbulent Jet Using PeriodicExcitation

646

D. Rapoport; I. Fono; K. Cohen; A. Seifert

Flow Separation Inside a Supersonic Nozzle Exhausting into aSubsonic Compressible Crossflow

655

S. J. Beresh; J. F. Henfling; R. J. Erven

Improved Aerodynamic-Ramp Injector in Supersonic Flow 663

L. S. Jacobsen; S. D. Gallimore; J. A. Schetz; W. F. O'Brien

Rotordynamic Bearing Dampers for Cryogenic Rocket EngineTurbopumps

674

Bugra H. Ertas; Eyad Al-Khateeb; John M. Vance

Evaluating Experimental Data Requirements for Spatially VaryingTurbine Flowfields Through Uncertainty Analysis

683

Susan T. Hudson; Boon Liang Heng

Adjoint Calculation of Sensitivities of Turbomachinery ObjectiveFunctions

693

M. Sergio Campobasso; Mihai C. Duta; Michael B. Giles

Low-Engine-Order Excitation Mechanisms in Axial-FlowTurbomachinery

704

C. Bréard; J. S. Green; M. Imregun

Technical Notes

Combustion Effects of C60 Soot in Ammonium Nitrate Propellants 713

Brian E. Greiner; Robert A. Frederick Jr.; Marlow D. Moser

Performance Analysis of Short Takeoff and Vertical Landing AircraftNozzle in Hover

715

Frank K. Lu; Douglas A. Terrier

Erratum

Errata on Theoretical Performance of FrictionlessMagnetohydrodynamics-Bypass Scramjet

718

Chul Park; David Bogdanoff; Unmeel B. Mehta

Volume 19 Number 3 May 2003

Full-length Papers

Scalability for Rocket Nozzle Flows Based on Subscale and Full-ScaleTesting

321

Gerald Hagemann; Jan Alting; Dieter Preclik

Edge Diffusion Flame Stabilization Behind a Step over a LiquidReactant

332

Matthew Juniper; Sébastien Candel

Characterization of Cryogenic Injection at Supercritical Pressure 342

Richard Branam; Wolfgang Mayer

Improvement of Inlet Flow Characteristics of LE-7A Liquid HydrogenPump

356

Masaharu Uchiumi; Kenjiro Kamijo; Kunio Hirata; Akira Konno;Tomoyuki Hashimoto; Satoshi Kobayasi

Rocket Engine Turbine Blade Surface Pressure Distributions:Experiment and Computations

364

Susan T. Hudson; Thomas F. Zoladz; Daniel J. Dorney

Effect of Nozzle Cavity on Resonance in Large SRM: NumericalSimulations

374

J. Anthoine; J.-M. Buchlin; J.-F. Guéry

Two-Phase Vorticoacoustic Flow Interactions in Solid-Propellant RocketMotors

385

Weidong Cai; Fuhua Ma; Vigor Yang

Thermoviscoelastic Characterization of a Composite Solid PropellantUsing Tubular Test

397

V. R. Sanal Kumar

Constant Volume Explosions of Aerosols of Metallic Mechanical Alloysand Powder Blends

405

Mirko Schoenitz; Edward L. Dreizin; Emil Shtessel

Optimization of Electric Thrusters for Primary Propulsion Based on theRocket Equation

413

Monika Auweter-Kurtz; Helmut Kurtz

Model of an Electrothermal Pulsed Plasma Thruster 424

Michael Keidar; Iain D. Boyd; Isak I. Beilis

Scale Effects on Solid-Propellant Coaxial MagnetoplasmadynamicThruster Performance

431

Giorgio Paccani; Luigi Petrucci; William D. Deininger

Low-Current, Xenon Orificed Hollow Cathode Performance for In-SpaceApplications

438

Matthew T. Domonkos; Michael J. Patterson; Alec D. Gallimore

Conservation Coupling Technique for Dynamic Inlet-Engine Analyses 444

Keith Numbers; Awatef Hamed

Multicriteria Design Optimization of Integrated Three-DimensionalSupersonic Inlets

456

Arnaud Gaiddon; Doyle D. Knight

Normal Shock/Boundary-Layer Interaction Control Using AeroelasticMesoflaps

464

Everett S. Hafenrichter; Yeol Lee; J. Craig Dutton; Eric Loth

Computation of Transonic Diffuser Flows by a Lagged k-_ TurbulenceModel

473

Q. Xiao; H. M. Tsai; F. Liu

Characteristics and Control of Combustion Instabilities in a Swirl-Stabilized Spray Combustor

484

S. Acharya; S. Murugappan; M. O'Donnell; E. J. Gutmark

Study of Interspacecraft Coulomb Forces and Implications forFormation Flying

497

Lyon B. King; Gordon G. Parker; Satwik Deshmukh; Jer-Hong Chong

Hysteresis Effects on Thrust Measurement and its Uncertainty 506

Joseph D. Sims; Hugh W. Coleman

Technical Notes

Analysis of Entrainment in a Sudden-Expansion Channel with WallMass Transfer

514

Jing-Tang Yang; Shih-Chao Lee; Yei-Chin Chao

Leading-Edge Shape and Aeroengine Fan Blade Performance 517

A. I. Sayma; M. Kim; N. H. S. Smith

Volume 19 Number 2 March 2003

Full-length Papers

Conceptual Development of Quiet Turbofan Engines for SupersonicAircraft

161

Dimitri Papamoschou; Marco Debiasi

Integration of an Aeroramp Injector/Plasma Igniter for HydrocarbonScramjets

170

L. S. Jacobsen; S. D. Gallimore; J. A. Schetz; W. F. O'Brien

Operational Sensitivities of an Integrated Scramjet Ignition/Fuel-Injection System

183

S. D. Gallimore; L. S. Jacobsen; W. F. O'Brien; J. A. Schetz

High Ram Acceleration Using Open-Base Projectile 190

Yuichiro Hamate; Akihiro Sasoh; Kazuyoshi Takayama

Kinetic Model for Aluminum-Sensitized Ram Accelerator Combustion 196

Laurent Catoire; Jean-François Legendre; Marc Giraud

Study of Combustion Characteristics of AmmoniumDinitramide/Polycaprolactone Propellants

203

Oleg P. Korobeinichev; Alexander A. Paletsky; Alexander G.Tereschenko; Evgeny N. Volkov

Design and Use of a Batch Reactor for Catalytic Decomposition ofPropellants

213

Rachel Eloirdi; Sylvie Rossignol; Charles Kappenstein; Daniel Duprez;Nicolas Pillet

Stability of Hydrogen/Hydrocarbon Blended Fuel Flames 220

Ahsan R. Choudhuri; S. R. Gollahalli

Numerical Simulation of High-Pressure and Fuel-Rich TurbulentCombustion Field

226

Takurou Makita; Takahisa Yamamoto; Tomohiko Furuhata; Norio Arai

Two-Phase Computational Fluid Dynamics Analysis Applied toPrefilming Pure-Airblast Atomizer

235

Philip E. O. Buelow; Chien-Pei Mao; Steven Smith; David Bretz

Axial Compressor Blade-to-Blade Unsteady Aerodynamic Variability 242

Douglas M. Boyd; Sanford Fleeter

Effects of Flow Instabilities on the Linear Analysis of TurbomachineryAeroelasticity

250

M. Sergio Campobasso; Michael B. Giles

Numerical Simulation of Aerodynamic Damping for Flutter Analysis ofTurbomachinery Blade Rows

260

R. Srivastava; M. A. Bakhle; T. G. Keith Jr.

Proper Orthogonal Decomposition of Turbine Rotor-Stator Interaction 268

Paul G. A. Cizmas; Antonio Palacios

Inlet/Engine Interactions in an Axisymmetric Pulse Detonation EngineSystem

282

Jonas Gustavsson; Venkata Nori; Corin Segal

Vortex Shedding Induced Sound Inside a Cold-Flow Simulation ofSegmented Chamber

287

Alison Flatau; W. K. Van Moorhem

Numerical Simulations of Wall and Shear Layer Instabilities in ColdFlow Setup

297

Jérôme Vétel; Frédéric Plourde; Son Doan Kim; Jean-François Guery

Technical Notes

Analyzing Mistuning of Bladed Disks by Symmetry and Reduced-OrderAerodynamic Modeling

307

B. Shapiro; K. E. Willcox

Active Control of Compressor Instability and Surge by Stator BladesAdjustment

312

M. T. Schobeiri; M. Attia

Aerodynamic Design of a VerticalThrust Adapter for Jet Engines 317

T. Strand

Volume 19 Number 1 January 2003

Editorial

Announcements and Acknowledgments 1

Reviewers for October 2001-September 2002 11

Ethical Standards for Publication of Aeronautics and AstronauticsResearch

12

AIAA Manuscript Review Process 13

Full-length Papers

Assessing Jet-Induced Spatial Mixing in a Rich, Reacting Crossflow 14

T. N. Demayo; M. Y. Leong; G. S. Samuelsen; J. D. Holdeman

Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube 22

E. Wintenberger; J. M. Austin; M. Cooper; S. Jackson; J. E. Shepherd

Thrust-Vectoring Nozzle Performance Modeling 39

Erich A. Wilson; Dan Adler; Pinhas Bar-Yoseph

Numerical Simulation of Distributed Combustion in Solid Rocket Motorswith Metalized Propellant

48

Jayant S. Sabnis

Plateau Burning Behavior of Ammonium Perchlorate Sandwiches andPropellants at Elevated Pressures

56

Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman;Jerry M. Seitzman

Optical Fouling of the RB199 Pyrometer 66

Clive Kerr; Paul Ivey

Bypass-Regulated Solid Fuel Ramjet Combustor in Variable FlightConditions

73

Deborah Pelosi-Pinhas; Alon Gany

Investigation of Instabilities in a Lean, Premixed Step Combustor 81

Jeffrey M. Cohen; Brian E. Wake; Dochul Choi

Sensitivity of Hydrocarbon Combustion Modeling for Hypersonic MissileDesign

89

Ryan P. Starkey; Mark J. Lewis

Rocketdyne Hypersonic Flow Laboratory as High-PerformanceExpansion Tube for Scramjet Testing

98

Benjamin S. Stewart; Richard G. Morgan; Peter A. Jacobs

Sonic Injection from Diamond-Shaped Orifices into a SupersonicCrossflow

104

Sadatake Tomioka; Lance S. Jacobsen; Joseph A. Schetz

Mixing Augmentation of Transverse Injection in Scramjet Combustor 115

Sang-Hyeon Lee; Tohru Mitani

Combined/Simultaneous Gust and Oscillating Compressor BladeUnsteady Aerodynamics

125

Kuk Kim Frey; Sanford Fleeter

Traveling Wave Excitation System for Bladed Disks 135

Keith W. Jones; Charles J. Cross

Numerical Study of Cryogenic Jets Under Supercritical Conditions 142

J. M. M. Barata; A. R. R. Silva

Technical Notes

Optimal Actuator/Sensor Placement for Control of CombustionInstabilities

148

Nidal Al-Masoud; Tarunraj Singh

Modified Mixing Analogy for Studies of Mixing in Supersonic Flows 151

Sadatake Tomioka; Lance S. Jacobsen; Joseph A. Schetz

Technical Comments

Technical Comment on "Vorticity Dynamics in Isobarically ClosedPorous Channels, Part 1: Standard Perturbations,"

155

R. L. Glick

Reply to Robert L. Glick's Comment: Physicality of Core Flow Models inRocket Motors

156

Joseph Majdalani

Volume 18 Number 6 November 2002

Advanced Performance Modeling of Experimental Laser Lightcraft 1129

Ten-See Wang; Yen-Sen Chen; Jiwen Liu; Leik N. Myrabo; Franklin B.Mead Jr.

Analysis and Application of Chorochronic Periodicity inTurbomachinery Rotor/Stator Interaction Computations

1139

G. A. Gerolymos; G. J. Michon; J. Neubauer

Experimental Study of the Transient Underexpanded Jet Generatedby Electrothermal Capillary Plasma

1153

Jong-Uk Kim; N. T. Clemens; P. L. Varghese

Mass-Based Optimization of Thermal Management and PowerSystems for Space Applications

1161

K. D. Freudenberg; W. E. Lear; S. A. Sherif; E. L. Golliher

Thermodynamics of Airbreathing Pulse-Detonation Engines 1170

J. A. C. Kentfield

Thermodynamic Limits of Work and Pressure Gain in Combustion andEvaporation Processes

1176

M. Razi Nalim

Work Potential Perspective of Engine Component Performance 1183

Bryce Roth

Numerical Reconstruction of Ejector Rocket Experimental Tests 1191

A. Matesanz; A. Velazquez; J. Tizon; J. Montanes

Motor and Plume Particle Size Prediction in Solid-Propellant RocketMotors

1199

Oleg B. Kovalev

Casting Process Impact on Small-Scale Solid Rocket Motor BallisticPerformance

1211

P. Le Breton; D. Ribéreau

Comparison of Laser- and Pressure-Driven Thrust Response of HMX 1218

Gautam N. Kudva; Thomas A. Litzinger

Modeling Cavitating Venturi Flows 1227

Changhai Xu; Stephen D. Heister; Robert Field

Hydrogen Peroxide Decomposition on Various Supported CatalystsEffect of Stabilizers

1235

Laurence Pirault-Roy; Charles Kappenstein; Maurice Guérin; RachelEloirdi; Nicolas Pillet

Thermochemistry of Species Produced from Monomethylhydrazine inPropulsion and Space-Related Applications

1242

Laurent Catoire; Mark T. Swihart

Advanced Seals for Industrial Turbine Applications: Design Approachand Static Seal Development

1254

Mahmut F. Aksit; Raymond E. Chupp; O. Saim Dinc; MehmetDemiroglu

Advanced Seals for Industrial Turbine Applications: Dynamic SealDevelopment

1260

Raymond E. Chupp; Farshad Ghasripoor; Norman A. Turnquist;Mehmet Demiroglu; Mahmut F. Aksit

Measured Flow Oscillations and Instabilities in Labyrinth Seal Cavities 1267

David L. Rhode; J. Wayne Johnson

Effects of Blade Count on Linearized and Nonlinear Hot StreakClocking Simulations

1273

Douglas L. Sondak; Vipul Gupta; Paul D. Orkwis; Daniel J. Dorney

Airfoil Row/Wake Interactions in a High-Speed Axial Compressor 1280

Robert T. Johnston; Sanford Fleeter

Interaction of Decaying Freestream Turbulence with a Moving ShockWave: Pressure Field

1289

S. Xanthos; G. Briassulis; Y. Andreopoulos

Proportional Control of Combustion Instabilities in a Simulated Gas-Turbine Combustor

1298

Christian Oliver Paschereit; Ephraim Gutmark

Technical Notes

Effects of End Wall Geometry and Stacking on Supersonic TurbinePerformance

1305

Daniel J. Dorney; Lisa W. Griffin; Frank W. Huber; Douglas L. Sondak

Controlling Electron Backstreaming Phenomena Through the Use of aTransverse Magnetic Field

1308

John E. Foster; Michael J. Patterson

2002 Journal of Propulsion and Power Index

Subject Index 1312

Author Index 1318

Chronological Index 1320


Full-Length Papers

A PIV Investigation of Rotor-IGV Interactions in a TransonicCompressor

969

Albert J. Sanders; John Papalia; Sanford Fleeter

Turbomachine Blade Row Interaction Predictions with a Three-Dimensional Finite Element Method

978

Dana A. Gottfried; Sanford Fleeter

Analysis of Dual-Mode Hydrocarbon Scramjet Operation at Mach 4-6.5

990

R. A. Baurle; D. R. Eklund

Acoustic Flutter Control of Three-Dimensional Transonic Rotor Flow 1003

Pong-Jeu Lu; Dartzi Pan; Yi-Di Yu

High-Speed Centrifugal Compressor Surge Initiation Characterization 1012

William C. Oakes; Patrick B. Lawless; John R. Fagan; Sanford Fleeter

Gas Turbine Engine and Sensor Fault Diagnosis Using OptimizationTechniques

1019

Marco Zedda; Riti Singh

Effect of Integration of Scramjet into Airframe on Engine Performanceand Payload

1026

Daisuke Akihisa; Takeshi Kanda; Kouichiro Tani; Kenji Kudo; GoroMasuya

Direct Experimental Impulse Measurements for Detonations andDeflagrations

1033

M. Cooper; S. Jackson; J. Austin; E. Wintenberger; J. E. Shepherd

Numerical Simulation of a Pulse Detonation Engine with HydrogenFuels

1042

Houshang B. Ebrahimi; Charles L. Merkle

Influence of Radical Concentration and Fuel Decomposition onIgnition of Propane/Air Mixture

1049

Yuriy Ya. Buriko; Viacheslav A. Vinogradov; Valentin F. Goltsev; PaulJ. Waltrup

Effects of Halons and Halon Replacements on Hydrogen-FueledLaminar Premixed Flames

1059

C. H. Kim; O. C. Kwon; G. M. Faeth

Pilot Flame Effects on Gas Jet Flames in Crossflow 1068

Sien-Fong Goh; S. R. Gollahalli

Assessment of Combustion Characteristics and Mechanism ofHydroxylammonium Nitrate-Based Liquid Monopropellant

1076

Yi-Ping Chang; Kenneth K. Kuo

Nonlinear Heterogeneous Model of Composite Solid-PropellantCombustion

1086

B. Rasmussen; R. A. Frederick Jr.

Combustion Response of Ammonium Perchlorate CompositePropellants

1093

Michael Shusser; Fred E. C. Culick; Norman S. Cohen

Property Transformation of Thermotropic Liquid Crystals Polymers 1101

J. J. Rusek; K. P. Chaffee

High Strain-Rate Constitutive Models for Solid Rocket Propellants 1106

Sook-Ying Ho

Study of Flow Separation in Truncated Ideal Contour Nozzle 1112

S. B. Verma

Technical Notes

Experimental Investigation of End-Wall Flow in Turbine Rotor 1122

X. Xiao; B. Lakshminarayana

Effect of Transient Gasdynamic Processes on the Impulse of PulseDetonation Engines

1124

C. B. Kiyanda; V. Tanguay; A. J. Higgins; J. H. S. Lee

Supersonic Wave/Blade-Row Interactions Establish BoundaryConditions for Unsteady Inlet Flows

1126

Miklos Sajben


Special Section: Electric Propulsion Space Experiment (ESEX)Program

Electric Propulsion Space Experiment (ESEX) p721

Roger M. Myers

Review of the Electric Propulsion Space Experiment (ESEX) Program p723

D. R. Bromaghim; J. R. Leduc; R. M. Salasovich; G. G. Spanjers; J.M. Fife; M. J. Dulligan; J. H. Schilling; D. C. White; L. K. Johnson

System Engineering, Design, Integration, and Qualification of ElectricPropulsion Space Experiment

p731

Mary M. Kriebel

Development and Flight Qualification of a 26-Kilowatt ArcjetPropulsion Subsystem

p740

R. J. Cassady; W. A. Hoskins; C. E. Vaughan

Orbital Performance Measurements of Air Force Electric PropulsionSpace Experiment Ammonia Arcjet

p749

J. M. Fife; D. R. Bromaghim; D. A. Chart; W. A. Hoskins; C. E.Vaughan; L. K. Johnson

Effect of ESEX 26-kW Arcjet Operation on SpacecraftCommunications

p754

M. J. Dulligan; R. Bromaghim; J. A. Zimmerman; R. M. Salasovich; D.Hardesty; L. K. Johnson

On-Orbit Optical Observations of Electric Propulsion SpaceExperiment 26-Kilowatt Arcjet

p763

L. K. Johnson; G. G. Spanjers; D. R. Bromaghim; M. W. Dulligan; W.A. Hoskins

Solar Cell Degradation During the 26-Kilowatt Electric PropulsionSpace Experiment Flight

p768

J. H. Schilling; G. G. Spanjers; D. R. Bromaghim; L. K. Johnson

Mass Deposition Measurements from 26-Kilowatt Electric PropulsionSpace Experiment Flight

p772

G. G. Spanjers; J. H. Schilling; S. F. Engelman; D. R. Bromaghim; L.K. Johnson

Radiometric Analysis from the 26-Kilowatt Electric Propulsion SpaceExperiment Flight

p777

G. G. Spanjers; J. H. Schilling; D. R. Bromaghim; L. K. Johnson

Full-Length Papers

Observations of Soot in the Combustion of Methanol/Toluene SprayFlames

p781

C. T. Avedisian; C. Presser; A. K. Gupta

Computational-Fluid-Dynamics Investigation of Aeromechanics p788

Peter D. Silkowski; Chae M. Rhie; George S. Copeland; James A.Eley; James M. Bleeg

Facility Effects on Performance Measurements of MicropropulsionSystems that Utilize Gas Expansion

p797

Andrew D. Ketsdever

Sensitivity of Solid Rocket Motors to Electrostatic Discharge: Historyand Future

p805

Alain Davenas; Roger Rat

Announcements and Acknowledgments

Asphaltic Thermoplastic Propellants p810

John J. Rusek

Full-Length Papers

Model of Aluminum Agglomerate Evolution in Combustion Products ofSolid Rocket Propellant

p814

V. A. Babuk; V. A. Vasilyev

Chemical Speciation and Dynamics in the Surface Combustion Zoneof Energetic Materials

p824

Thomas B. Brill; Merrill C. Beckstead; Joseph E. Flanagan; M. C. Lin;Thomas A. Litzinger; R. H. Woodward Waesche; Charles A. Wight

Thermomechanical Analysis and Optimization of Cryogenic LiquidRocket Engines

p835

Detlef Kuhl; Jörg Riccius; Oskar J. Haidn

Effect of Momentum Ratio on the Mixing Performance of Unlike SplitTriplet Injectors

p847

Y. D. Won; Y. H. Cho; S. W. Lee; W. S. Yoon

Flourescence and Temperature Measurements in an Actively ForcedSwirl-Stabilized Spray Combustor

p855

V. Santhanam; F. C. Knopf; S. Acharya; E. Gutmark

Heat Release Rates of Burning Items in Fires p866

Hyeong-Jin Kim; David G. Lilley

New Fossil Power Systems and the Role of Open-CycleMagnetohydrodynamics Generators

p871

Naoyuki Kayukawa

Application of Autoassociative Neural Network on Gas-Path SensorData Validation

p879

Pong-Jeu Lu; Tzu-Cheng Hsu

Control of Low-Pressure Turbine Separation Using Vortex-GeneratorJets

p889

Rolf Sondergaard; Richard B. Rivir; Jeffrey P. Bons

Analysis and Multidisciplinary Optimization of Internal CoolantNetworks in Turbine Blades

p896

Thomas J. Martin; George S. Dulikravich

Optimum Mixing of Core and Bypass Streams in High-Bypass CivilTurbofan

p907

Vivek Sanghi; B. K. Lakshmanan; S. K. Sane

Automated Design Optimization of a Three-Dimensional S-ShapedSubsonic Diffuser

p913

Sophia Lefantzi; Doyle D. Knight

Inlet/Compressor System Response to Short-Duration AcousticDisturbances

p922

Anthony B. Opalski; Miklos Sajben

Analysis of a Fusion-Electric Airbreathing Earth to Orbit LaunchVehicle

p933

Robert B. Adams; D. Brian Landrum

Characterization of Expansion Tube Flows for HypervelocityCombustion Studies

p943

Adela Ben-Yakar; Ronald K. Hanson

Drag and Total Pressure Distributions in Scramjet Engines at Mach 8Flight

p953

Tohru Mitani; Tetsuo Hiraiwa; Yuichi Tarukawa; Goro Masuya

Technical Notes

Laser-Air Interactions in an Internal Supersonic Flowpath p961

Robert B. Adams; D. Brian Landrum

Timescaling Control Volumes During Real Time Digital Simulation of aMilitary Turbofan

p964

Vivek Sanghi; B. K. Lakshmanan

Technical Comments

Comment on "Equation for Additive Drag Coefficient at StaticConditions"

p967

William H. Heiser; Jack D. Mattingly

Reply to Technical Comment from William H. Heiser and Jack D.Mattingly

p968

K. L. Christensen


Full-Length Papers

Project Orion and Future Prospects for Nuclear Pulse Propulsion 497

G. R. Schmidt; J. A. Bonometti; C. A. Irvine

Study of the Phase-Lock Phenomenon for a Circular Slingatron 505

G. R. Cooper; D. A. Tidman

Shape Optimization of Supersonic Turbines Using GlobalApproximation Methods

509

Approximation Methods

Nilay Papila; Wei Shyy; Lisa Griffin; Daniel J. Dorney

Unsteady Cascade Aerodynamics in the Time Domain 519

Dana A. Gottfried; Sanford Fleeter

Multiobjective Optimization of Rocket Engine Pumps UsingEvolutionary Algorithm

528

Akira Oyama; Meng-Sing Liou

Three-Dimensional Hybrid Mesh Generation for TurbomachineryAirfoils

536

Kyu-Sup Kim; Paul G. A. Cizmas

Development of High-Performance Airfoils for Axial Flow CompressorsUsing Evolutionary Computation

544

Ernesto Benini; Andrea Toffolo

High-Pressure Steam Flow in Turbine Bypass Valve System Part 1:Valve Flow

555

R. S. Amano; G. R. Draxler

High-Pressure Steam Flow in Turbine Bypass Valve System Part 2:Pipe Flow

561

R. S. Amano; G. R. Draxler; J. M. Golembiewski

Acceptance Screening of Turbopump Gears Using the CepstrumMethod

572

S. J. DiMaggio

Appearance of Restricted Shock Separation in Rocket Nozzles 577

G. Hagemann; M. Frey; W. Koschel

Performance Analysis of Secondary Gas Injection into a Conical RocketNozzle

585

Hyun Ko; Woong-Sup Yoon

Ejector Primary Flow Molecular Weight Effects in an Ejector-RamRocket Engine

592

Sam Han; John Peddieson Jr.; David Gregory

Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines 600

William H. Knuth; Martin J. Chiaverini; J. Arthur Sauer; Daniel J.Gramer

Combustion of Liquefying Hybrid Propellants: Part 1, General Theory 610

M. A. Karabeyoglu; D. Altman; B. J. Cantwell

Combustion of Liquefying Hybrid Propellants: Part 2, Stability of LiquidFilms

621

M. A. Karabeyoglu; B. J. Cantwell

Burning Aluminum Particles Inside a Laboratory-Scale Solid RocketMotor

631

John C. Melcher; Herman Krier; Rodney L. Burton

Evaluation of Ultrasound Technique for Solid-Propellant Burning-RateResponse Measurements

641

Jeffrey J. Murphy; Herman Krier

Aerodynamic Optimization of Turbomachinery Cascades UsingEuler/Boundary-Layer Coupled Genetic Algorithms

652

Ozhan Oksuz; I. Sinan Akmandor; Mehmet S. Kavsaoglu

When Do Open-Loop Strategies for Combustion Control Work? 658

R. K. Prasanth; A. M. Annaswamy; J. P. Hathout; A. F. Ghoniem

Flashover: A Study of Parameter Effects on Time to Reach FlashoverConditions

669


Comparison of Criteria for Room Flashover 674


Effects of Airstream Mach Number on H2/N2 Plasma Igniter 679

Goro Masuya; Kenichi Takita; Katsuyoshi Takahashi; Fumio Takatori;Hiroyuki Ohzeki

Elliptic Coflow Effects on a Circular Gas Jet Flame 686

Ahsan R. Choudhuri; Sayela P. Luna; S. R. Gollahalli

Experimental Study of a 3-kW Stirling Engine 696

Noboru Kagawa

Improved Mean-Flow Solution for Slab Rocket Motors with RegressingWalls

703

Chong Zhou; Joseph Majdalani

Technical Notes

Geometric Evaluation of Axisymmetric Thrust-Vectoring Nozzles forAerodynamic Performance Predictions

712

Erich A. Wilson; Dan Adler; Pinhas Z. Bar-Yoseph

Combustion Characteristics of Ethylene in Scramjet Engines 716

A. A. Taha; S. N. Tiwari; T. O. Mohieldin

High-Intensity Sound Absorption at an Orifice with Bias Flow 718

Xiaodong Jing; Xiaofeng Sun


Full-Length Papers

Multilevel Analysis of Pulsed Detonation Engines 225

Houshang B. Ebrahimi; Rajendran Mohanraj; Charles L. Merkle

Development of Advanced Industrial Furnace Using Highly PreheatedCombustion Air

233

T. Hasegawa; S. Mochida; A. K. Gupta

Effects of Liquid-Oxygen Post Biasing on SSME Injector WallCompatibility

240

P. A. Strakey; D. G. Talley; L. K. Tseng; K. I. Miner

Time- and Length Scales of Combustion in Liquid Rocket ThrustChambers

247

B. Ivancic; W. Mayer

Computations of Axisymmetric Plug-Nozzle Flowfields: Flow Structuresand Thrust Performance

254

Takashi Ito; Kozo Fujii; A. Koich Hayashi

Numerical Simulation of Side Loads in an Ideal Truncated Nozzle 261

Sébastien Deck; Philippe Guillen

Design Analysis of a Satellite Hydrazine Propulsion System 270

An-Shik Yang; Tien-Chuan Kuo

Leak Fault Detection of Liquid Rocket Engine Based on StrongTracking Filter

280

Yu Daren; Wang Jianbo

Temperature-Dependent Modal Test/Analysis Correlation of X-34FASTRAC Composite Rocket Nozzle

284

Andrew M. Brown

Characteristic Analysis of Flow-Induced Vibrations on Inducer ofOxygen Pump

289

Liang Hengli; Chen Zuoyi

Numerical Predictions of Channel Flows with Fluid Injection UsingReynolds-Stress Model

295

Bruno Chaouat

Effect of Nozzle Cavity on Resonance in Large SRM: TheoreticalModeling

304

J. Anthoine; J-M. Buchlin; A. Hirschberg

Dynamic Combustion of Solid Propellants: Effects of UnsteadyCondensed Phase Degradation Layer

312

K. R. Anil Kumar; K. N. Lakshmisha

Slingatron: A High Velocity Rapid Fire Sling 322

Derek A. Tidman

Sizing a Slingatron-Based Space Launcher 330

Mark L. Bundy; Derek A. Tidman; Gene R. Cooper

Numerical Simulations of the Slingatron 338

G. R. Cooper; D. A. Tidman; M. L. Bundy

Ethylene Ignition and Detonation Chemistry, Part 1: Detailed Modelingand Experimental Comparison

344

B. Varatharajan; F. A. Williams

Ethylene Ignition and Detonation Chemistry, Part 2: Ignition Historiesand Reduced Mechanisms

352

B. Varatharajan; F. A. Williams

Study of the High-Temperature Autoignition of n-Alkane/O2/Ar Mixtures 363

D. C. Horning; D. F. Davidson; R. K. Hanson

Profiling of Redox Index During Combustion to Monitor C/C CompositeDegradation in Flames

372

Kuniyuki Kitagawa; Masao Kubota; Norio Arai; Ashwani K. Gupta

Chemiluminescence-Based Feedback Control of Equivalence Ratio fora Continuous Combustor

376

a Continuous Combustor

Douglas A. Scott; Galen B. King; Normand M. Laurendeau

Linear Deterministic Source Terms for Hot Streak Simulations 383

Paul D. Orkwis; Mark G. Turner; John W. Barter

Combustion Instability Active Control Using Periodic Fuel Injection 390

J. P. Hathout; M. Fleifil; A. M. Annaswamy; A. F. Ghoniem

Constant Volume Limit of Pulsed Propulsion for a Constant _ Ideal Gas 400

Douglas G. Talley; Edward B. Coy

Combustion Air Jet Influence on Primary Zone Characteristics for Gas-Turbine Combustors

407

S. Gogineni; D. Shouse; C. Frayne; J. Stutrud; G. Sturgess

Mach 8 Testing of a Scramjet Engine with Ramp Compression 417

Takeshi Kanda; Kouichiro Tani; Kan Kobayashi; Toshihito Saito; TetsujiSunami

Magnetohydrodynamic Power Extraction from Cold Hypersonic Airflowswith External Ionizers

424

Sergey O. MacHeret; Mikhail N. Shneider; Richard B. Miles

Analysis of a High-Efficiency Low-Emissions "Chemical Gas Turbine"System

432

Takahisa Yamamoto; Tomohiko Furuhata; Norio Arai; Noam Lior

Fuzzy Logic Intelligent System for Gas Turbine Module and SystemFault Isolation

440

Ranjan Ganguli

Particle Image Velocimetry Characterization of a Chordwise BendingCascade Flowfield

448

Daniel A. Ehrlich; Sanford Fleeter

Rotor Blade-to-Blade Wake Variability and Effect on Downstream VaneResponse

456

Albert J. Sanders; Sanford Fleeter

Massively Parallel Simulation of the Unsteady Flow in an Axial TurbineStage

465

Jixian Yao; Roger L. Davis; Juan J. Alonso; Antony Jameson

Impeller Blade Unsteady Aerodynamic Response to Vaned DiffuserPotential Fields

472

Dana Gottfried; Sanford Fleeter

Recent GRC Aerospace Technologies Applicable to Terrestrial EnergySystems

481

M. David Kankam; Valerie J. Lyons; Mark A. Hoberecht; Robert R.Tacina; Aloysius F. Hepp

Technical Notes

Correlating Laser Induced Fluorescence and Molecular Beam MassSpectrometry Ion Energy Distributions

489

George J. Williams; Timothy B. Smith; Frank S. Gulczinski; Alec D.Gallimore

Transonic Rotor Blade Pressure Measurement Using FluorescentPaints

491

T. Liu; S. Torgerson; J. Sullivan; R. Johnston; S. Fleeter

Unsteady Flow in a Supersonic Turbine with Variable Specific Heats 493

Daniel J. Dorney; Lisa W. Griffin; Frank Huber; Douglas L. Sondak


Editorial

Announcements and Acknowledgments 1

V. Yang


Editorial Policy Statement on Numerical Accuracy and ExperimentalUncertainty

11


12


Full-Length Papers

History of U.S. Navy Ramjet, Scramjet, and Mixed-Cycle PropulsionDevelopment

14

P. J. Waltrup; M. E. White; F. Zarlingo; E. S. Gravlin

Integrated Design and Analysis of Intakes and Nozzles in Air-BreathingEngines

28

M. Ferlauto; F. Larocca; L. Zannetti

Analytical Model of the Base Flow Between a Subsonic and SupersonicFlow

35

Doo S. Baik; Glen W. Zumwalt

Numerical Simulation of the Ram Accelerator Using a New ChemicalKinetics Mechanism

44

Michael J. Nusca

Scale-Up Experiments on Liquid-Fueled Active Combustion Control 53

Ken H. Yu; Ken J. Wilson

Experimental Investigation of Limit-Cycle Oscillations in an UnstableGas Turbine Combustor

61

Tim C. Lieuwen

Thermodynamic Cycle Analysis of Pulse Detonation Engines 68

William H. Heiser; David T. Pratt

Fundamentals of Idealized Airbreathing Pulse-Detonation Engines 77

J. A. C. Kentfield

Selection of Actuators and Sensors for Surge Control 84

Marc Van De Wal; Frank Willems; Bram De Jager

Flow Control via Rotor Trailing Edge Blowing in Rotor/Stator AxialCompressor

93

A. M. Wo; A. C. Lo; W. C. Chang

Active Control of Discrete-Frequency Noise Generated by Rotor-StatorInteractions

100

Scott Sawyer; Sanford Fleeter; John Simonich

Shock Fitting a Transonic Cascade Solution into an Inverse DesignTechnique

107

Jeffrey W. Yokota; Adam J. Medd

Experimental and Analytical Design Verification of the Dual-BellConcept

116

Gerald Hagemann; Michael Terhardt; Dietrich Haeseler; Manuel Frey

Effects of Grain Geometry on Pulse-Triggered Combustion Instability inRocket Motors

123

Mehdi Golafshani; Mohammad Farshchi; Hojat Ghassemi

Overview of the Development of Hydrazinium Nitroformate 131

H. F. R. Schöyer; W. H. M. Welland-Veltman; J. Louwers; P. A. O. G.Korting; A. E. D. M. van der Heijden; H. L. J. Keizers; R. P. van denBerg

Overview of the Development of Hydrazinium Nitroformate-BasedPropellants

138

H. F. R. Schöyer; W. H. M. Welland-Veltmans; J. Louwers; P. A. O. G.Korting; A. E. D. M. van der Heijden; H. L. J. Keizers; R. P. van denBerg

Design of a Fusion Propulsion System - Part 1: Gigawatt-LevelMagnetoplasmadynamic Source

146

Pavlos G. Mikellides; Peter J. Turchi; Ioannis G. Mikellides

Design of a Fusion Propulsion System - Part 2: Numerical Simulation ofMagnetic-Nozzle Flows

152

Ioannis G. Mikellides; Pavlos G. Mikellides; Peter J. Turchi; Thomas M.York

Interior and Exterior Laser-Induced Fluorescence and PlasmaMeasurements within a Hall Thruster

159

W. A. Hargus Jr; M. A. Cappelli

Verification Tests of Carbon-Carbon Composite Grids for MicrowaveDischarge Ion Thruster

169

I. Funaki; H. Kuninaka; K. Toki; Y. Shimizu; K. Nishiyama; Y. Horiuchi

Cascade Arc Studies of Hydrogen/Nitrogen Plasmas in Nonequilibrium 176

Trevor Moeller; Dennis Keefer; Robert Rhodes

Flow Past Stationary Spherical Particles with Streamwise VelocityFluctuation

184

A. Dasgupta; T. I-P. Shih

Reduced Chemical Kinetic Mechanisms for Hydrocarbon Fuels 192

Christopher J. Montgomery; Marc A. Cremer; Jyh-Yuan Chen; BerkeleyBerkeley; Charles K. Westbrook; Lourdes Q. Maurice

Two-Dimensional Spectroscopic Analysis of a Flame Using HighlyPreheated Combustion Air

199

Noriyuki Konishi; Kuniyuki Kitagawa; Norio Arai; Ashwani K. Gupta

Technical Notes

Anomalous Deflagration Behavior of Ammonium Perchlorate atElevated Pressures

205

Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman;Jeffrey M. Freeman

Effects of GH2/LOX Velocity and Momentum Ratios on Shear CoaxialInjector Atomization

209

M. Ferraro; R. J. Kujala; J.-L. Thomas; M. J. Glogowski; M. M. Micci

Equation for Additive Drag Coefficient at Static Conditions 211

K. L. Christensen

Intercusp Electron Transport in an NSTAR-Derivative Ion Thruster 213

John E. Foster

Optimal Three-Dimensional Nozzle Shape Design Using CFD andParallel Simulated Annealing

217

X. Wang; M. Damodaran

Propagation of Acoustic Waves in a Two-Phase Vaporizing Mixture 222

Joël Dupays; François Vuillot

Erratum 224

Progress in Hypersonic Science and Technology Development


Editorial 1137

History

Scramjet Engines: The First Forty Years 1138

Edward T. Curran

Program Overview and Case Studies

Two-Stage-to-Orbit Spaceplane Concept with Growth Potential 1149

Unmeel B. Mehta; Jeffrey V. Bowles

Testing Technologies and Flight Experiments

Numerical Research of Gaseous Fuel Preinjection in HypersonicThree-Dimensional Inlet

1162

O. V. Guoskov; V. I. Kopchenov; K. E. Lomkov; V. A. Vinogradov; P.J. Waltrup

Program Overview and Case Studies

Development of Hydrocarbon-Fueled Scramjet Engines: TheHypersonic Technology (HyTech) Program

1170

O. A. Powell; J. T. Edwards; R. B. Norris; K. E. Numbers; J. A. Pearce

French-Russian Partnership on Hypersonic Wide-Range Ramjets 1177

Marc Bouchez; François Falempin; Vadim Levine; Valery Avrashkov;Dmitri Davidenko

Multidisciplinary Optimization of Airbreathing Hypersonic Vehicles 1184

Kevin G. Bowcutt

Synthesis of a FESTIP Airbreathing TSTO Space TransportationSystem

1191

H. Grallert

System Performance Analysis and Concept Studies

Upper Bounds on the Flight Speed of Hydrocarbon-Fueled Scramjet-Powered Vehicles

1199

Paul J. Waltrup

Domain of the Scramjet 1205

L. H. Townend

Significance of Fuel Selection for Hypersonic Vehicle Range 1214

Mark J. Lewis

Structural Mechanics and Materials

Experimental Study of Scramjet Module 1222

Marat A. Goldfeld; Alexey V. Starov; Viacheslav V. Vinogradov

System Performance Analysis and Concept Studies

Strutjet Engine Performance 1227

Bryan T. Campbell; Adam Siebenhaar; Thong Nguyen

Structural Mechanics and Materials

Development Study of a Precooler for the Air-Turboramjet Expander-Cycle Engine

1233

Kenya Harada; Nobuhiro Tanatsugu; Tetsuya Sato

Combined Engine for Reusable Launch Vehicle (KLIN Cycle) 1239

V. V. Balepin; P. A. Czysz; R. H. Moszée

Advancement of Scramjet Magnetohydrodynamic Concept 1247

B. M. Burakhanov; A. P. Likhachev; S. A. Medin; V. A. Novikov; V. I.Okunev; V. Yu. Rickman; V. A. Zeigarnik

Fundamental Mechanisms: Combustion and Fuel Management

Initiators for Endothermic Fuels 1253

D. T. Wickham; J. R. Engel; B. D. Hitch; M. E. Karpuk

Thermal Stability of Energetic Hydrocarbon Fuels for Use in CombinedCycle Engines

1258

K. Wohlwend; L. Q. Maurice; T. Edwards; R. C. Striebich; M.Vangsness; A. S. Hill

Investigation of Kerosene Combustion Characteristics with PilotHydrogen in Model Supersonic Combustors

1263

G. Yu; J. G. Li; X. Y. Chang; L. H. Chen; C. J. Sung

Historical Survey on Enhanced Mixing in Scramjet Engines 1273

John M. Seiner; S. M. Dash; D. C. Kenzakowski

Effect of Flame-Holding Cavities on Supersonic-CombustionPerformance

1287

Ken H. Yu; Ken J. Wilson; Klaus C. Schadow

Newly Developed Direct-Connect High-Enthalpy SupersonicCombustion Research Facility

1296

Combustion Research Facility

Mark Gruber; Jeffrey Donbar; Kevin Jackson; Tarun Mathur; RobertBaurle; Dean Eklund; Charles Smith

Supersonic Combustion Experiments with a Cavity-Based FuelInjector

1305

Tarun Mathur; Mark Gruber; Kevin Jackson; Jeff Donbar; WayneDonaldson; Thomas Jackson; Fred Billig

Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-FlowFacility

1313

C. P. Goyne; J. C. McDaniel; T. M. Quagliaroli; R. H. Krauss; S. W.Day

Numerical Simulation of Supersonic Airflow with Transverse HydrogenInjection

1319

E. von Lavante; D. Zeitz; M. Kallenberg

Effects of Swirl and Skew Upon Supersonic Wall Jet in Crossflow 1327

A. D. Cutler; S. E. Doerner

Skin-Friction Measurements in a Supersonic Combustor withCrossflow Fuel Injection

1333

H. Tanno; A. Paull; R. J. Stalker

Thermal Analysis of Fluid-Structural Interaction in High-Speed EngineFlowfields

1339

Birgit U. Reinartz; Wolfgang W. Koschel

Fundamental Mechanisms: Inlet and Nozzle

Optimal Design of Plug Nozzles and Their Thrust Determination atStart

1347

A. N. Kraiko; N. I. Tillyayeva; S. V. Baftalovskii

Computation of a Nonequilibrium Expansion Flow in a SingleExpansion Ramp Nozzle

1353

Thomas Link; Wolfgang W. Koschel

Testing Technologies and Flight Experiments

Experimentation, Test, and Evaluation Requirements for FutureAirbreathing Hypersonic Systems

1361

Dan Marren; Mark Lewis; Lourdes Q. Maurice

Quasi-One-Dimensional High-Speed Engine Model with Finite-RateChemistry

1366

Timothy F. O'Brien; Ryan P. Starkey; Mark J. Lewis


Full-Length Papers

Hybrid (Particle-Fluid) Modeling of Pulsed Plasma Thruster Plumes 945

Nikolaos A. Gatsonis; Xuemin Yin

Heating and Plasma Properties in a Coaxial Gasdynamic PulsedPlasma Thruster

959

Stewart S. Bushman; Rodney L. Burton

Quasi-Steady Magnetoplasmadynamic Thruster PerformanceDatabase

967

E. Y. Choueiri; J. K. Ziemer

Electrospray as a Source of Nanoparticles for Efficient ColloidThrusters

977

M. Gamero-Castaño; V. Hruby

Impact of Energy Gain and Subsystem Characteristics on FusionPropulsion Performance

988

S. Chakrabarti; G. R. Schmidt

Development of a Resonance Igniter for GO2/Kerosene Ignition 995

Mario Niwa; A. Santana Jr.; Khoze Kessaev

Nonlinear Control of a Reusable Rocket Engine for Life Extension 998

Carl F. Lorenzo; Asok Ray; Michael S. Holmes

Flame-Spreading Phenomena in Fin Slots of a Solid Rocket Motor 1005

K. K. Kuo; R. A. Kokal; M. Paulauskas; P. Alaksin; L. S. Lee

Effects of Oxidizer Particle Size on Propellants Based on ModifiedPolyvinyl Chloride

1012

Vladica S. Bozic; Marko V. Milos

Burning-Rate Modifier Effects on a Modified Polyvinyl Chloride-BasedPropellants

1017

Vladica S. Bozic; Djordje Dj. Blagojevic

Development of Thermal Barriers for Solid Rocket Motor Nozzle Joints 1023

Bruce M. Steinetz; Patrick H. Dunlap Jr.

Flexibilized Novolac Epoxy Resin for Inhibition of CompositePropellants

1035

J. P. Agrawal; N. T. Agawane

Russian Research on Experimental Hydrogen-Fueled Dual-ModeScramjet: Conception and Preflight Tests

1041

Donat A. Ogorodnikov; Viacheslav A. Vinogradov; Yurii M. Shikhman;Vitaliy N. Strokin

Magnetohydrodynamics Energy Bypass Scramjet Performance withReal Gas Effects

1049

Chul Park; Unmeel B. Mehta; David W. Bogdanoff

Ignition and Flame Studies for an Accelerating Transonic Mixing Layer 1058

X. Fang; F. Liu; W. A. Sirignano

Underexpanded Jet for Testing Laser-Based Combustion Diagnostics 1067

K. G. Klavuhn; J. C. McDaniel

Effect of Ambient Pressure on an Airblast Spray Injected into aCrossflow

1076

May Y. Leong; Vincent G. McDonell; G. Scott Samuelsen

Ignition Delays in MMH + CH4 + O2 + Ar Mixtures 1085

Laurent Catoire; Gabrielle Dupré; Claude Paillard; Abdelkrim Elaissi

Acoustic-Wave/Blade-Row Interactions Establish Boundary Conditionsfor Unsteady Inlet Flows

1090

for Unsteady Inlet Flows

Miklos Sajben; Hazem Said

Mechanisms and Prediction Methods for Fan Blade Stall Flutter 1100

M. Vahdati; A. I. Sayma; J. G. Marshall; M. Imregun

Experimental Investigation of Lobed Mixer Performance 1109

A. Abolfadl; M. A. Metwally; A. M. El-Messiry; M. A. Ali

Optimum Fan Pressure Ratio for Bypass Engines with Separate orMixed Exhaust Streams

1117

Abhijit Guha

Optimization of Turbomachinery Airfoils with a Genetic/ Sequential-Quadratic-Programming Algorithm

1123

Brian H. Dennis; George S. Dulikravich; Zhen-Xue Han

Technical Notes

Mixing of Supersonic Jets in a Strutjet Propulsion System 1129

S. Muller; Clark W. Hawk; P. G. Bakker; D. Parkinson; M. Turner

Modular Ignition System Based on Resonance Igniter 1131

M. Niwa; A. Santana Jr.; K. Kessaev

Experimental Investigation of Pulsatile Flow in Circular Tubes 1133

Josef Adamec; Ji í No i ka; Daniel Hanus; Josef Ko ená


Full-Length Papers

Direct Flight to Pluto Using Solar Electric Propulsion 753

J. S. Meserole; W. R. Richards

Low Mass Components for Mars Ascent Propulsion 758

Keith Dyer; George Yankura; Jesus Acosta

Triple Langmuir Probe Measurements in the Plume of a Pulsed PlasmaThruster

762

Robert Eckman; Lawrence Byrne; Nikolaos A. Gatsonis; Eric J. Pencil

Computation of Hall Thruster Performance 772

L. Garrigues; I. D. Boyd; J. P. Boeuf

High-Pressure Bipropellant Microrocket Engine 780

A. P. London; A. H. Epstein; J. L. Kerrebrock

Experimental Study of Major Species and Temperature Profiles ofLiquid Oxygen/Gaseous Hydrogen Rocket Combustion

788

Serdar Yeralan; Sibtosh Pal; Robert J. Santoro

Propellant Atomization and Ignition Phenomena in LiquidOxygen/Gaseous Hydrogen Rocket Combustors

794

Wolfgang O. H. Mayer; Blazenko Ivancic; Axel Schik; Ulf Hornung

Combustion Behavior and Flame Structure of XM46 Liquid Propellant 800

Y.-P. Chang; E. Boyer; K. K. Kuo

Analysis of In-Flight Behavior of Truncated Plug Nozzles 809

F. Nasuti; M. Onofri

Evaporation of Sprays of Liquid Fuels and Liquid Oxidizers in a ShearLayer

818

D. Katoshevski; Y. Tambour

Sensitivity of Mixed Subsonic-Supersonic Turbulent Mixing Layers 823

D. Chad Cottrell III; Michael W. Plesniak

Computation of Compressible Flows Through a Chemical Laser Devicewith Crossflow Injection

836

James H. Miller; Joe S. Shang; Robert F. Tomaro; William Z. Strang

Convergence Behavior of Surface Evolver Applied to a GenericPropellant-Management Device

845

Steven H. Collicott

Combustion of Magnesium with Carbon Dioxide and Carbon Monoxideat Low Gravity

852

Angel Abbud-Madrid; Abhijit Modak; Melvyn C. Branch; John W. Daily

Combustion Characteristics of a Liquid-Fueled Ramjet Combustor 860

Takao Inamura; Mamoru Takahashi; Akinaga Kumakawa

Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets:An Overview

869

Adela Ben-Yakar; Ronald K. Hanson

Internally Mixed Liquid Injector for Active Control of AtomizationProcess

878

A. Kushari; Y. Neumeier; O. Israeli; E. Lubarsky; B. T. Zinn

Random Packs and Their Use in Modeling Heterogeneous SolidPropellant Combustion

883

S. Kochevets; J. Buckmaster; T. L. Jackson; A. Hegab

Blade-Row Interaction in a High-Pressure Turbine 892

V. S. P. Chaluvadi; A. I. Kalfas; M. R. Banieghbal; H. P. Hodson; J. D.Denton

Hub Wall Rotation Influence on High-Speed Compressor CascadePerformance

902

A. Doukelis; K. Mathioudakis; K. Papailiou

Nonlinear Dynamic Combustion in Solid Rockets: L* Effects 909

K. C. Tang; M. Q. Brewster

Actuator Duct Model of Turbomachinery Components for Powered-Nacelle Navier-Stokes Calculations

919

Entsung Hsiao; Mahmood Naimi; Jeffrey P. Lewis; Keith Dalbey; YifangGong; Choon Tan

Aeroacoustic Measurement of Transient Hot Nozzle Flows 928

Daniel R. Kirk; Douglas O. Creviston; Ian A. Waitz

Technical Notes

Downstream Gas Effect on Nozzle Flow-Separation Location 936

John W. Murdock; Richard P. Welle

Adaptive Analysis of the Inviscid Supersonic Flow over a Backward-Facing Step

938

S. Y. Yang

Effect of Reynolds Number on Pitot-Pressure Distributions inUnderexpanded Supersonic Freejets

940

Hiroshi Katanoda; Taro Handa; Yoshiaki Miyazato; Mitsuharu Masuda;Kazuyasu Matsuo

Numerical Evaluation of Inelastic Mechanisms in a Nitrogen Arcjet 943

Shigeru Kuchi-Ishi; Michio Nishida


Full-Length Papers

Laser Doppler Anemometry Measurements in an Axial CompressorStage

481

Thierry M. Faure; Guy-Jean Michon; Hubert Miton; Nicolas Vassilieff

Shape Parameterization and Optimization of a Two-Stroke Engine 492

Angelos P. Mimis; Malcolm I. G. Bloor; Michael J. Wilson

Mars-Earth Rapid Interplanetary Tether Transport System: I. InitialFeasibility Analysis

499

Gerald D. Nordley; Robert L. Forward

Spectral Content of Solar Radiation on Martian Surface Based on MarsPathfinder

508

J. Appelbaum; A. Steiner; G. A. Landis; C. R. Baraona; T. Segalov

Ion Propulsion Development Projects in U.S.: Space Electric RocketTest I to Deep Space 1

517

James S. Sovey; Vincent K. Rawlin; Michael J. Patterson

Development and Validation of Fluid/Thermodynamic Models forSpacecraft Propulsion Systems

527

Henry C. Hearn

Safe Testing of Nuclear Rockets 534

Steven D. Howe; Bryan Travis; David K. Zerkle

Search for Nuclear Isotopes for Use in a Nuclear Battery 540

B. D. Guenther; H. R. Weller; Jennifer L. Godwin

Review of Refractory Materials for Alkali Metal Thermal-to-ElectricConversion Cells

547

Jeffrey C. King; Mohamed S. El-Genk

Stress and Buckling Analyses of Multitube, Vapor-Anode, Nb-1Zr/C-103AMTEC Cells

557

Jeffrey C. King; Mohamed S. El-Genk

Analysis of Heat-Driven Jet-Pumped Cooling System for SpaceThermal Management

566

J. W. Nord; W. E. Lear; S. A. Sherif

Computational Optimization of a Hypersonic Rectangular-to-CircularInlet

571

John W. Sabean; Mark J. Lewis

Sidewall Interaction in an Asymmetric Simulated Scramjet InletConfiguration

579

D. V. Gaitonde; M. R. Visbal; J. S. Shang; A. A. Zheltovodov; A. I.Maksimov

Manipulation of Shock/Boundary-Layer Interactions in Hypersonic Inlets 585

D. Schulte; A. Henckels; R. Neubacher

Theoretical Performance of Frictionless Magnetohydrodynamic-BypassScramjets

591

Chul Park; David Bogdanoff; Unmeel B. Mehta

Propulsive Performance of Hypersonic Oblique Detonation Wave andShock-Induced Combustion Ramjets

599

J. P. Sislian; H. Schirmer; R. Dudebout; J. Schumacher

Effects of Fuel Preinjection on Mixing in Mach 1.6 Airflow 605

Michael Owens; Sudarshan Mullagiri; Corin Segal; Viacheslav A.Vinogradov

Thermal Choking Analyses in a Supersonic Combustor 611

M. G. Owens; S. Mullagiri; C. Segal; P. J. Ortwerth; A. B. Mathur

Thrust, Lift, and Pitching Moment of a Scramjet Engine 617

Takashi Shimura; Noboru Sakuranaka; Tetsuji Sunami; Kouichiro Tani

Small-Bore Ram Accelerator Operation 622

A. Sasoh; Y. Hamate; K. Takayama

Aerothermal Model for Real-Time Digital Simulation of a Mixed-FlowTurbofan Engine

629

Vivek Sanghi; B. K. Lakshmanan; R. Rajasekaran

Unified Treatment of Flow Instabilities of Turbomachines 636

Yoshinobu Tsujimoto; Kenjiro Kamijo; Christopher E. Brennen

Tip Leakage Flow in a Radial Inflow Turbine with Varying Gap Height 644

R. Dambach; H. P. Hodson

Analysis of Unsteady Blade Row Interaction Using Nonlinear HarmonicApproach

651

T. Chen; P. Vasanthakumar; L. He

Development and Validation of a Massively Parallel Flow Solver forTurbomachinery Flows

659

Jixian Yao; Antony Jameson; Juan J. Alonso; Feng Liu

Redesigning Gas-Generator Turbines for Improved UnsteadyAerodynamic Performance Using Neural Networks

669

Nateri K. Madavan; Man Mohan Rai; Frank W. Huber

Influence of Compressor Exit Conditions on Combustor AnnularDiffusers, Part 1: Diffuser Performance

678

A. G. Barker; J. F. Carrotte

Influence of Compressor Exit Conditions on Combustor AnnularDiffusers Part II: Flow Redistribution

687

A. G. Barker; J. F. Carrotte

Turbojet and Turbofan Engine Performance Increases Through TurbineBurners

695

F. Liu; W. A. Sirignano

Pressure Waves in Volume Effect in Gas-Turbine Transient-Performance Models

706

Y. G. Li; N. R. L. MacCallum; P. Pilidis

Pressure Drop Across a Double-Outlet Vortex Chamber 711

Georgios H. Vatistas; Peter Sakaris

Parametric Study of the Swirler/Venturi Spray Injectors 717

Kyoung-Su Im; Hoisan Kim; Ming-Chia Lai; Robert Tacina

On the Breakup of Viscous Liquid Sheets by Dual-Mode LinearAnalysis

728

Sushanta K. Mitra; Xianguo Li; Metin Renksizbulut

Mixing Mechanisms in a Pair of Impinging Jets 736

Nasser Ashgriz; William Brocklehurst; Douglas Talley

Technical Note

Studies on Performance of Airblast Atomizer Under Varying Flow andGeometric Conditions

750

S. N. Sridhara; B. N. Raghunandan


Full-Length Papers

Gear Fault Detection in Rocket Engine Turbomachinery 225

S. J. Dimaggio; S. Rubin; B. H. Sako

Oscillating Airfoil Aerodynamics of a Rotating Compressor Blade Row 232

Kuk Kim Frey; Sanford Fleeter

240

Michael K. Fabian; Eric A. Falk; Eric J. Jumper

Control of Blade Flutter by Smart-Casing Treatment 248

Xiaofeng Sun; Xiaodong Jing; Hongwu Zhao

Comparison of Methods for Calculating Turbine Work in the AirTurborocket

256

K. L. Christensen

Upstream-Propagating Potential Disturbances in the F109 TurbofanEngine Inlet Flow

262

Eric A. Falk; Eric J. Jumper; Michael K. Fabian; Jerry Stermer

Analysis of a Device for Generating Perturbations in Supersonic WindTunnels

270

Kevin J. Melcher; Mounir B. Ibrahim

Experimental Testing of a Hypersonic Inlet with Rectangular-to-EllipticalShape Transition

276

M. K. Smart

Mole-Fraction-Sensitive Imaging of Hypermixing Shear Layers 284

J. S. Fox; A. F. P. Houwing; P. M. Danehy; M. J. Gaston; N. R.Mudford; S. L. Gai

Combustion Tests of a Staged Supersonic Combustor with a Strut 293

Sadatake Tomioka; Atsuo Murakami; Kenji Kudo; Tohru Mitani

Combustion Efficiencies of Supersonic Flames 301

Albert Ratner; James F. Driscoll; Hwanil Huh; Rodney A. Bryant

Reaction and Mixing-Controlled Combustion in Scramjet Engines 308

Tohru Mitani; Nobuo Chinzei; Takeshi Kanda

Scramjet Fuels Autoignition Study 315

Meredith B. Colket III; Louis J. Spadaccini

Comparison of Thermodynamic Loss Models Suitable for Gas TurbinePropulsion

324

Bryce A. Roth; Dimitri N. Mavris

SCCREAM: A Conceptual Rocket-Based Combined-Cycle EnginePerformance Analysis Tool

333

John R. Olds; John E. Bradford

High-Energy-Utilization, Dual-Mode System Concept for Mars Missions 340

Mohamed S. El-Genk

Structural Dynamic Analysis of Solid Rocket Motor Resonant Burning 347

K. W. Dotson; J. M. Womack; P. J. Grosserode

Vorticity Dynamics in Isobarically Closed Porous Channels Part I:Standard Perturbations

355

J. Majdalani

Vorticity Dynamics in Isobarically Closed Porous Channels Part II:Space-Reductive Perturbations

363

J. Majdalani; T. S. Roh

Periodic Propellant Flames and Fluid-Mechanical Effects 371

T. L. Jackson; J. Buckmaster; A. Hegab

Study of a New Kind of Multipulse Rocket Motor 380

Mingde Song; Dingyou Ye

Numerical Modeling of Pressurization of a Propellant Tank 385

Alok Majumdar; Todd Steadman

Response Surface and Neural Network Techniques for Rocket EngineInjector Optimization

391

Wei Shyy; P. Kevin Tucker; Rajkumar Vaidyanathan

Mixing Characteristics of Coaxial Injectors at High Gas/LiquidMomentum Ratios

402

P. A. Strakey; D. G. Talley; J. J. Hutt

Advanced Sub-Model for Airblast Atomizers 411

Y. Liao; S. M. Jeng; M. A. Jog; M. A. Benjamin

Near-Field Ion Energy and Species Measurements of a 5-kW HallThruster

418

Frank S. Gulczinski III; Alec D. Gallimore

Internal Plasma Properties and Enhanced Performance of 8-CentimeterIon Thruster Discharge

428

John E. Foster; Michael J. Patterson

Plasma Confinement in the Whistler Wave Plasma Thruster 433

B. W. Stallard; E. B. Hooper Jr; J. L. Power

Thermal Decomposition of RDX in the Presence of Added K2B12H12 441

Michael A. Schroeder; Robert A. Fifer; Pamela J. Kaste; Shirley A.Liebman

Direct Evidence of Spatial Burning Rate Variation as Cause of MidwebAnomaly

449

Desh Deepak; R. Jeenu; P. Sridharan; M. S. Padmanabhan

Combustion of Kerosene in Counterflow Diffusion Flames 453

P. M. Patterson; A. G. Kyne; M. Pourkashanian; A. Williams; C. W.Wilson

Surrogate Mixtures to Represent Complex Aviation and Rocket Fuels 461

Tim Edwards; Lourdes Q. Maurice

Analysis and Design of the Inductor-Current-Sensing Peak-Power-Tracking Solar-Array Regulator

467

Yoon-Jay Cho; Bo-Hyung Cho

Technical Notes

Optimal Geometry of Self-Field Magnetoplasmadynamic Thrusters 472

Guido Colasurdo; Lorenzo Casalino

Transonic Compressor Influences on Upstream Surface Pressures withAxial Spacing

474

Peter J. Koch; Douglas P. Probasco; J. Mitch Wolff; William W.Copenhaver; Randall M. Chriss

Thermodynamic Cycle Analysis of Magnetohydrodynamic-BypassHypersonic Airbreathing Engines

477

Ron J. Litchford; John W. Cole; Valentine A. Bityurin; John T. Lineberry


Editorial

A Distinguished Career. . .and a New Beginning 1

Roger L. Simpson

To Everything There Is a Season 2

R. H. Woodward Waesche

Thank You and Best Wishes to Dr. R. H. Woodward Waesche 3

Vigor Yang



9


10


Full-Length Papers

Erosion Resistance of Carbon-Carbon Ion Optics 12

J. S. Meserole

Magnetohydrodynamics Generator with Plasma Layers as PowerSource Aboard a Hypersonic Airplane

19

Vadim S. Slavin; Valery M. Gavrilov; Nikolay I. Zelinsky; Alexandr R.Bozhkov

Development of Ultraviolet Raman Diagnostics for Rocket EngineInjector Analysis

27

Joseph A. Wehrmeyer; John M. Cramer; Richard H. Eskridge; Chris C.Dobson

Fuel Regression Rate in Hydroxyl-Terminated-Polybutadiene/Gaseous-Oxygen Hybrid Rocket Motors

35

Philmon George; S. Krishnan; P. M. Varkey; M. Ravindran; LalithaRamachandran

Upstream Wake Influences on the Measured Performance of aTransonic Compressor Stage

43

Steven E. Gorrell; William W. Copenhaver; Randall M. Chriss

Flow and Acoustic Properties of Underexpanded Elliptic-Slot Jets 49

S. B. Verma; E. Rathakrishnan

Studies on Combustion of Metallized RDX-Based Composite ModifiedDouble-Base Propellants

58

C. N. Divekar; S. N. Asthana; Haridwar Singh

Transient Force Reduction in Electromechanical Actuators for Thrust-Vector Control

65

Dale E. Schinstock; Douglas A. Scott; Tim A. Haskew

Flame Spread with Sudden Expansions of Ports of Solid PropellantRockets

73

B. N. Raghunandan; V. R. Sanal Kumar; C. Unnikrishnan; C. Sanjeev

Scalar Variance Transport in the Turbulence Modeling of PropulsiveJets

79

N. Chidambaram; S. M. Dash; D. C. Kenzakowski

Optimization for Aircraft Engines with Regression and Neural-NetworkAnalysis Approximators

85

Surya N. Patnaik; James D. Guptill; Dale A. Hopkins; Thomas M.Lavelle

Multidisciplinary Approach to Linear Aerospike Nozzle Design 93

J. J. Korte; A. O. Salas; H. J. Dunn; N. M. Alexandrov; W. W. Follett; G.E. Orient; A. H. Hadid

Regression-Rate and Heat-Transfer Correlations for Hybrid RocketCombustion

99

Martin J. Chiaverini; Kenneth K. Kuo; Arie Peretz; George C. Harting

Computational Assessment of Afterburning Cessation Mechanisms inFuel-Rich Rocket Exhaust Plumes

111

William H. Calhoon Jr

Gun Interior Ballistic Performance with Ammonium Nitrate-AlcoholPropellants

120

Akihiro Sasoh; Toshihiro Ogawa; Kazuyoshi Takayama; Kazunari Ikuta;Nobuo Nagayasu; Shinobu Ohtsubo

Model of Particulate Interaction with Plasma in a Teflon Pulsed PlasmaThruster

125

Michael Keidar; Iain D. Boyd; Isak I. Beilis

Mach 8 Testing of a Scramjet Engine Model 132

Takeshi Kanda; Tetsuji Sunami; Sadatake Tomioka; Kouichiro Tani;Tohru Mitani

Effect of Sides-Spillage from Airframe on Scramjet Engine Performance 139

Kouichiro Tani; Takeshi Kanda; Kenji Kudo; Daisuke Akihisa

Fundamental Studies of Cavity-Based Flameholder Concepts forSupersonic Combustors

146

M. R. Gruber; R. A. Baurle; T. Mathur; K.-Y. Hsu

Effect of Reynolds Number on Separation Bubbles on CompressorBlades in Cascade

154

Garth V. Hobson; Denis J. Hansen; David G. Schnorenberg; Darren V.Grove

Amine Sensitization Studies of Secondary Explosives Using Laser-Induced Ignition

163

A. L. Ramaswamy; T. Mukundan; M. M. Chaudhri

Effects of Interjet Spacing on Burning Multiple Sprays 169

K. Parvez; S. R. Gollahalli

Application of Artificial Neural Networks to the Design ofTurbomachinery Airfoils

176

Man Mohan Rai; Nateri K. Madavan

Novel Electroexplosive Device Incorporating a Reactive LaminatedMetallic Bridge

184

Thomas A. Baginski; Steven L. Taliaferro; Wm. David Fahey

Pressure Effects on Geometry and Structure of Gas Jet Flames inCrossflow

190

Ahsan R. Choudhuri; S. R. Gollahalli

Velocity and Temperature Statistics in Reacting Droplet-LadenHomogeneous Shear Turbulence

197

Farzad Mashayek

Origins of Accelerator Grid Current: Analysis of T5 Grid Test Results 203

Mark W. Crofton; Iain D. Boyd

Technical Notes

Fluid Property Effects on Sheet Disintegration of a Simplex Pressure-Swirl Atomizer

212

I-Ping Chung; Cary Presser

Characteristic Gap: A New Design Criterion for Solid Rocket Motors 216

Daniel Chasman

Concentration Measurements in a Mixing Module for Lean, Premixed,Gas-Turbine Combustors

218

R. V. Ravikrishna; D. Douglas Thomsen; Clayton S. Cooper; YananJiang; Normand M. Laurendeau

Radiation and NOx Pathways in Nonpremixed Turbulent Flames 222

D. Lentini; I. K. Puri


Full-Length Papers

Optimization of Orifice Geometry for Crossflow Mixing in a CylindricalDuct

929

J. T. Kroll; W. A. Sowa; G. S. Samuelsen; J. D. Holdeman

Comparison of Spray/Wall Impingement Models with ExperimentalData

939

Seong Hyuk Lee; Hong Sun Ryou

Numerical Study of Fuel Mixing Enhancement Using an ObliqueShock/Vortex Interaction

946

Ashish Nedungadi; Mark J. Lewis

Maximum Mixing Times of Methane and Air 956

Dan Brasoveanu; Ashwani K. Gupta

Multicomponent-Fuel Film-Vaporization Model for MultidimensionalComputations

964

Yangbing Zeng; Chia-Fon Lee

Soot Patterns Around Suspended n-Heptane Droplet Flames in aConvection-Free Environment

974

C. Thomas Avedisian; Gregory S. Jackson

Effect of Sauter Mean Diameter on the Combustion RelatedParameters in Heavy-Duty Diesel Engines

980

Stanislav N. Danov; Ashwani K. Gupta

Predicting Effectiveness of H2O Injection for NOx Reduction inStationary Gas Turbines

988

A. M. Mellor

Broadband Infrared Absorption Sensor for High-Pressure CombustorControl

994

J. M. Seitzman; B. T. Scully

Computation of Gas-Liquid Droplet Cascade Flows Using MultigridAdaptive Unstructured Grid

1002

Ki-Cheol Park; Keun-Shik Chang

Performance of Evaporative Cycle Gas Turbines Derived fromAeroengines

1011

Sergio Mario Camporeale; Bernardo Fortunato

Determination of Triggering Condition of Vortex-Driven AcousticCombustion Instability in Rocket Motors

1022

Wen-Jing Wu; Li-Chung Kung

Computational Analysis for Rocket-Based Combined-Cycle SystemsDuring Rocket-Only Operation

1030

C. J. Steffen Jr; T. D. Smith; S. Yungster; D. J. Keller

Starting Envelope of the Subdetonative Ram Accelerator 1040

E. Schultz; C. Knowlen; A. P. Bruckner

Work Interaction in Quasi-One-Dimensional Flows 1053

Thomas Scott; David W. Riggins

Longitudinally Stratified Combustion in Wave Rotors 1060

M. Razi Nalim

Solid-Fuel Ramjet Regulation by Means of an Air-Division Valve 1069

Deborah Pelosi-Pinhas; Alon Gany

Impingement Heating and Ignition of Condensed-Phase EnergeticMaterials

1075

Mohammad K. Alkam; P. Barry Butler

Development of the Low-Power Xenon Ion Thruster for LightweightSatellites

1083

O. A. Gorshkov; V. G. Grigor'yan; V. A. Muravlev

Mass Spectral Measurements in the Plume of an SPT-100 HallThruster

1086

Lyon B. King; Alec D. Gallimore

Electrical Characteristics of Magnetohydrodynamic-GeneratorSidewalls with Segmented Z-Bar Design

1093

Carlson C. P. Pian; Stanley W. Petty

Pulsed Fusion Propulsion System for Rapid Interstellar Missions 1100

Terry Kammash

Regenerative Solid Oxide Fuel Cells for Mars Exploration 1105

K. R. Sridhar; R. Foerstner

Optimal Allocation with Network Limitation for Autonomous SpacePower System

1112

James A. Momoh; Jizhong Zhu; Jim L. Dolce

Application of Bethe-Zel'dovich-Thompson Fluids in Organic RankineCycle Engines

1118

Brady P. Brown; Brian M. Argrow

Performance Analysis for High-Speed Missile Inlets 1125

Christophe Bourdeau; Michaël Blaize; Doyle Knight

Automated Design of a Three-Dimensional Subsonic Diffuser 1132

Wei-Li Zhang; Doyle D. Knight; Don Smith

Simulation of Coupled Unsteady Flow and Heat Conduction in TurbineStage

1141

Douglas L. Sondak; Daniel J. Dorney

Mechanical Coupling Effects on Turbomachine Mistuned Response 1149

James A. Kenyon; Charles J. Cross; Gregory R. Minkiewicz

Hub-Based Vibration Control of Multiple Rotating Airfoils 1155

György Szász; George T. Flowers; Roy J. Hartfield

Linear Versus Quadratic Amplitude Feedback in Active Control ofCompressor Rotating Stall

1164

Nikos Markopoulos; Yedidia Neumeier; J. V. R. Prasad; Ben T. Zinn

Three-Dimensional Automatic Optimization Method forTurbomachinery Blade Design

1174

K. F. C. Yiu; M. Zangeneh

Technical Note

Thixotropic Effect of Inorganic Gel Fuels 1182

Shai Rahimi; Benveniste Natan


Full-Length Papers

Optimization of Jet Mixing into a Rich, Reacting Crossflow 729

M. Y. Leong; G. S. Samuelsen; J. D. Holdeman

Propagation of Spinning Acoustic Modes in Turbofan Exhaust Ducts 736

M. Nallasamy; D. L. Sutliff; L. J. Heidelberg

Unsteady Viscous Flow Causing Rotor-Stator Interaction in Turbines,Part 1: Data, Code Pressure

744

B. Lakshminarayana; A. Chernobrovkin; D. Ristic

Unsteady Viscous Flow Causing Rotor-Stator Interaction in Turbines,Part 2: Simulation, Integrated Flowfield, and Interpretation

751

A. Chernobrovkin; B. Lakshminarayana

Analytical and Experimental Assessment of Two Methods ofDetermining Turbine Efficiency

760

Susan T. Hudson; Hugh W. Coleman

Unsteady Blade-Row Flow Calculations Using a Low-Reynolds-NumberTurbulence Model

768

Chang Ho Choi; Jung Yul Yoo

Fluid Circuit Model for Long-Bearing Squeeze Film DamperRotordynamics

777

Paul A. Schallhorn; David A. Elrod; David G. Goggin; Alok K. Majumdar

Bleed Valve Rate Requirements Evaluation in Rotating Stall Control onAxial Compressors

781

Simon Yeung; Yong Wang; Richard M. Murray

Dynamic Simulation of a Wave-Rotor-Topped Turboshaft Engine 792

R. B. Greendyke; D. E. Paxson; M. T. Schobeiri

Survey of Advancements in Jet-Engine Thermodynamic Simulation 797

Vivek Sanghi; B. K. Lakshmanan; V. Sundararajan

Analysis of Transient Thermal Choking Processes in a Model ScramjetEngine

808

S. O'Byrne; M. Doolan; S. R. Olsen; A. F. P. Houwing

Design and Control of Solid-Fuel Ramjet for PseudovacuumTrajectories

815

S. Krishnan; Philmon George; S. Sathyan

Injection and Mixing Processes in High-Pressure LiquidOxygen/Gaseous Hydrogen Rocket Combustors

823

W. Mayer; A. Schik; M. Schäffler; H. Tamura

Analysis of Gaseous Fuel and Air Mixing in Flames and FlameQuenching

829

Dan Brasoveanu; Ashwani K. Gupta

Effect of Inlet Turbulence and Premixer Length on Fuel Distribution inSwirling Gas-Turbine Premixer

837

S. F. Frey; A. R. Eaton; D. M. Cusano; M. W. Plesniak; P. E. Sojka

Role of Oxygen-Enriched Atomization in Kerosene Spray Flames 845

A. K. Gupta; T. Damm; S. R. Charagundla; C. Presser

Overview of World Space Launches 853

I-Shih Chang

Oscillatory Combustion of Fine-AP/HTPB Propellants: DisproportionatePyrolysis Response

867

S. R. Hickman; M. Q. Brewster

Prediction of the Dissipation of a Solid-Rocket Contrail 874

Eugene Miller

On-Orbit Demonstration of a Pulsed Self-Field MagnetoplasmadynamicThruster System

880

K. Toki; Y. Shimizu; K. Kuriki

Applied-Field Magnetoplasmadynamic Thrusters, Part 1: NumericalSimulations Using the MACH2 Code

887

Pavlos G. Mikellides; Peter J. Turchi; Norman F. Roderick

Applied-Field Magnetoplasmadynamic Thrusters, Part 2: AnalyticExpressions for Thrust and Voltage

894

Pavlos G. Mikellides; Peter J. Turchi

Computation of the Plume of an Anode-Layer Hall Thruster 902

Iain D. Boyd

Investigation of the Operating Characteristics of a High-Power HallEffect Thruster

910

Boris Arhipov; Leonid Krochak; Nikolay Maslennikov; Fabrizio Scortecci

Ion-Energy Diagnostics in the Plasma Exhaust Plume of a Hall Thruster 916

Lyon B. King; Alec D. Gallimore

Antimatter Requirements and Energy Costs for Near-Term PropulsionApplications

923

G. R. Schmidt; H. P. Gerrish; J. J. Martin; G. A. Smith; K. J. Meyer


Editorial 545

Norio Arai; Kuni Kitagawa; Ashwani K. Gupta

Advanced Terrestrial Energy Conversion

Advanced Power Generation 545


Utilization of High-Density Strained Hydrocarbon Fuels for Propulsion 546

Gabriel D. Roy

Analysis of Combustion Characteristics of Coaxial Jet Diffusion Flamewith Steam Addition

552

D. Zhao; H. Yamashita; T. Furuhata; N. Arai

Power Generation Analysis for High-Temperature Gas Turbine inThermodynamic Process

557

Hiroshi Taniguchi; Sigehiro Miyamae; Norio Arai; Noam Lior

Double Reheat Rankine Cycle for Hydrogen-Combustion, TurbinePower Plants

562

Masafumi Fukuda; Yoshikazu Dozono

Enhancing Direct-Fired Power Plants Performance by Use of GasTurbine Technology

568

Mikhail Korobitsyn

Status and Perspective of Externally Fired Gas Turbines 572

J. Yan; L. Eidensten

Miniaturization Technologies for Advanced Energy Conversion andTransfer Systems

577

Timothy A. Ameel; Ian Papautsky; Robert O. Warrington; Robert S.Wegeng; M. Kevin Drost

Gas Turbine Heat Transfer: Past and Future Challenges 583

Ralf Schiele; Sigmar Wittig

Investigation of Regenerative Combustion Using a Heavy Fuel Oil 590

I-Te Huang; Wen-Chen Chang; Wei-Min Chern; Rey-Chein Chang

Visualization of Fuel Jet in Conditions of Highly Preheated AirCombustion

595

S. Lille; T. Dobski; W. Blasiak

Characteristics of Pulverized Coal Combustion in High-TemperaturePreheated Air

601

Takashi Kiga; Kunio Yoshikawa; Masaru Sakai; Susumu Mochida

Gasification Characteristics of Biomass Wastes in Fluidized BedGasifier

606

Ping Liu; Xiaofen Guo; Chuangzhi Wu; Yong Chen; Norio Arai

Modeling of Oxy-Natural Gas Combustion Chemistry 609

Anders Brink; Mikko Hupa; Frederic Breussin; Nicolas Lallemant;Roman Weber

Thermal Destruction of Cellulose and Surrogate Solid Wastes 615

Ashwani K. Gupta

Stability of Plane Liquid Sheets in Compressible Gas Streams 623

Jianming Cao; Xianguo Li

Recent Advances in Soot Formation from Spherical Droplet Flames atAtmospheric Pressure

628

C. Thomas Avedisian

Influence of Exhaust Aftertreatment Devices on Heavy-Duty DieselEngine's Particulate Emissions

636

George Toussimis; Euripides Lois; Hartmut Lüders

Fire Development Calculations 641

David G. Lilley

Minimum Safe Distance from Pool Fires 649

David G. Lilley

Transition in Boundary Layers on a Concave Surface 653

S. H. Winoto; D. H. Zhang; Y. T. Chew

Full-Length Papers

Localized Thermal Buckling Due to Hot Streaks in a Combustor Liner 661

W. Z. Zhuang; N. S. Swansson

Thermal State-of-Charge of Space Solar Dynamic Heat Receivers 666

Carsie A. Hall III; Emmanuel K. Glakpe; Joseph N. Cannon; Thomas W.Kerslake

Effect of Initial Velocity Profile on the Development of Round Jets 676

E. Ferdman; M. V. Ötügen; S. Kim

Feasibility Study for Performance Prediction of CircumferentiallyCompound-Stage Model Turbines

687

André P. Saxer; Hélène M. Saxer-Felici; Damian M. A. Vogt; MichaelSell; George Gyarmathy

Numerical Investigation of Installation Effects in Turbofan Engines 697

W. G. Joo

Energy Management in Rocket Propulsion 705

Guido Colasurdo; Lorenzo Casalino

Comparison of Supersonic Combustion Between Impulse and Vitiation-Heated Facilities

709

R. R. Boyce; A. Paull; R. J. Stalker; M. Wendt; N. Chinzei; H. Miyajima

Technical Notes

Unstarted Inlet for Direct-Connect Combustor Experiments in a ShockTunnel

718

R. R. Boyce; A. Paull; R. J. Stalker

Reference Spray Combustion Facility for Computational FluidDynamics Model Validation

720

John F. Widmann; S. Rao Charagundla; Cary Presser

Role of Curing Agents on Decomposition and Explosion of GlycidylAzide Polymers

723

Surendra P. Panda; Sanjay K. Sahu; Dinkar S. Sadafule; Jyotsna V.Thakur

Numerical Simulation of Axisymmetric Solid Rocket Motor IgnitionTransient with Radiation Effect

725

In Hyun Cho; Seung Wook Baek


Full-Length Papers

Effects of Radial Location on the Migration of Hot Streaks in a Turbine 377

Karen L. Gundy-Burlet; Daniel J. Dorney

Viscous Three-Dimensional Simulation of Transonic Compressor Stageon Parallel Hardware

388

Gerd Fritsch; Martin Hoeger; Cristoph Blaha; Dirk Bauer

Incidence Effects on Wake-Induced Transition on an Axial CompressorBlade

397

W. J. Solomon; G. J. Walker

Experiment to Support the Formulation and Validation of Compressor-Face Boundary Conditions

406

Donald Freund; Miklos Sajben

Adiabatic Interaction of Particles with a Compressible Flow: BasicMechanics

415

Francisco Ruiz

Experimental Investigation of Rotor-Inlet Guide Vane Interactions inTransonic Axial-Flow Compressor

421


Evaluating Efficiencies of Turbofan Jet Engines: A Data EnvelopmentAnalysis Approach

431

Sean Bulla; William W. Cooper; Dennis Wilson; Kyung Sam Park

Scarfing and Scalloping Effects on Lobed Forced Mixer at Low-SpeedConditions

440

S. C. M. Yu; Y. Hou; W. K. Chan

Transverse Injection from Circular and Elliptic Nozzles into aSupersonic Crossflow

449

M. R. Gruber; A. S. Nejad; T. H. Chen; J. C. Dutton

Flow of Gel Fuels in Tapered Injectors 458

Shai Rahimi; Benveniste Natan

Streamline Tracing: Technique for Designing Hypersonic Vehicles 465

Frederick S. Billig; Ajay P. Kothari

Wall Drag in Internal Mach-2 Flow with Cavity and TranspirationInjection

472

Linda A. Castiglone; G. Burton Northam; Ned R. Baker; Larry A. Roe

Restricted Shock Separation in Rocket Nozzles 478

Manuel Frey; Gerald Hagemann

Combustor Model for Simulation of Combustion Instabilities and TheirActive Control

485

Rajendran Mohanraj; Yedidia Neumeier; Ben T. Zinn

Convergence of Two Analytical Flowfield Models Predicting aDestabilizing Agent in Rocket Combustion

492

J. Majdalani; G. A. Flandro; T. S. Roh

Nonpremixed Periodic Flames Supported by HeterogeneousPropellants

498

T. L. Jackson; J. Buckmaster

Line-of-Sight Variations of Temperature and Species in Solid PropellantFlames

505

Carl F. Mallery Jr.; Stefan T. Thynell

Flame/Stretch Interactions of Premixed Fuel-Vapor/O2/N2 Flames 513

O. C. Kwon; M. I. Hassan; G. M. Faeth

Ultrasonic Method Applied to Full-Scale Solid Rocket Motors 523

Franck Cauty

Measurements of Ions from High-Current Hollow Cathodes UsingElectrostatic Energy Analyzer

529

Ikuya Kameyama; Paul J. Wilbur

Three-Dimensional Numerical Simulation of Field-Emission-Electric-Propulsion Neutralization

536

M. Tajmar; J. Wang


Full-Length Papers

Confined Swirling Flows with Heat Release and Mixing 169

David S. Underwood; Ian A. Waitz; Edward M. Greitzer

Numerical Investigation of Twin-Nozzle Rocket Plume Phenomenology 178

Houshang B. Ebrahimi; Jay Levine; Alan Kawasaki

Detailed Chemical-Kinetic Model for Aviation Fuels 187

R. P. Lindstedt; L. Q. Maurice

Thrust Vector Control for (Clustered Modules) Plug Nozzles: SomeConsiderations

196

H. F. R. Schöyer

Optimizing Subcritical-Flow Thrust-Vectoring of Converging-DivergingNozzles

202

Nozzles

Erich A. Wilson; Dan Adler; Benjamin Z. Bal-Or; Valery Sherbaum;Michael Lichtsinder

Direct Computation of Jet Noise Produced by Large-ScaleAxisymmetric Structures

207

R. R. Mankbadi; H. Shih; R. Hixon; L. A. Povinelli

Flowfield near a Mulitiport Injector Array in a Supersonic Flow 216

L. S. Jacobsen; J. A. Schetz; W. F. Ng

Ignition Characteristics of Plasma Torch for Hydrogen Jet in anAirstream

227

Kenichi Takita; Tomokazu Uemoto; Takahiro Sato; Yiguang Ju; GoroMasuya; Katsura Ohwaki

Two-Dimensional Nonadiabatic Injection into a Supersonic Freestream 234

Rodney D. W. Bowersox; K. Colin Tucker; Christopher D. Whitcomb

Propulsion System for Hypersonic Space Planes 243

Michael Zeutzius; Toshiaki Setoguchi; Kunio Terao; Hideo Miyanishi

Pulse Detonation Magnetohydrodynamic Power 251

Ron J. Litchford; Bryan R. Thompson; John T. Lineberry

Magnetocombustion: A Thermodynamic Analysis 263

John Baker; Kozo Saito

Optimization of Ram Accelerator Systems Design 269

Xiaojian Wang; Elyeser Spiegler; Yaakov M. Timnat

Experimental Investigation of the Evaporation of Droplets in AxialAcoustic Fields

278

R. I. Sujith; G. A. Waldherr; J. I. Jagoda; B. T. Zinn

Effect of Inlet Conditions on Endwall Secondary Flows 286

Kristina S. Hermanson; Karen A. Thole

Effect of Inner and Outer Airflow Characteristics on High LiquidPressure Prefilming Airblast Atomization

297

J. S. Chin; N. K. Rizk; M. K. Razdan

Progress in Modeling Pressure Oscillations in Regenerative LiquidPropellant Guns

302

T. P. Coffee

Eulerian Approach for Unsteady Two-Phase Solid Rocket Flows withAluminum Particles

309

Eric Daniel

Combustion Experiments in Hydrogen Peroxide/Polyethylene HybridRocket with Catalytic Ignition

318

E. J. Wernimont; S. D. Heister

Time-Accurate Three-Dimensional Navier-Stokes Analysis of One-and-One-Half Stage Axial-Flow Turbine

327

Thomas W. Volmar; Bernard Brouillet; Heinz E. Gallus; HannesBenetschik

Modeling of Turbine Engine Axial-Flow Compressor and TurbineCharacteristics

336

Marek Orkisz; Slawomir Stawarz

New Gear-Fault-Detection Parameter by Use of Joint Time-FrequencyDistribution

340

V. V. Polyshchuk; F. K. Choy; M. J. Braun

Feasibility Assessment of Thermal Barriers for Extreme TransientTemperatures

347

Bruce M. Steinetz; Patrick H. Dunlap Jr

Numerical Thermal Model of NASA Solar Electric PropulsionTechnology Application Readiness Ion Thruster

357

Jonathan Van Noord; Alec Gallimore; Vincent K. Rawlin

Technical Notes

Joint Jet-A/Silane/Hydrogen Reaction Mechanism 365

Mark J. Lewis; Jee Su Chang

Lithium Peroxide Fuel Cells for Electric Vehicle Propulsion 367

Gautum Agarwal

Simulations of the Flow in Supersonic Turbines with Straight CenterlineNozzles

370

Daniel J. Dorney; Lisa W. Griffin; Karen L. Gundy-Burlet

Burning Behavior of Composite Propellants with Fast-BurningInclusions

374

A. E. Fogelzang; A. P. Denisyuk; V. V. Serushkin; V. Yu. Egorshev; V.P. Sinditskii; A. D. Margolin


Editorial

Forward into the New Millennium 1




7


8


Full-Length Papers

Aerodynamic Analysis of an Installed Thrust Reverser 10

Daniel J. Strash; J. Michael Summa; Joel H. Frank; Robert Standish

Numerical Simulations and Planar Laser-Induced FluorescenceImaging Results of Hypersonic Reactive Flows

16

Kazu Toshimitsu; Akiko Matsuo; Michel R. Kamel; Christopher I. Morris;Ronald K. Hanson

Numerical Investigation of Hydrogen Strut Injections into SupersonicAirflows

22

P. Gerlinger; D. Brüggemann

Fuel Injection into a Supersonic Airflow by Means of Pylons 29

C. Gruenig; V. Avrashkov; F. Mayinger

Self-Ignition and Supersonic Reaction of Pylon-Injected Hydrogen Fuel 35

C. Gruenig; V. Avrashkov; F. Mayinger

Incomplete Mixing and Off-Design Effects on Shock-InducedCombustion Ramjet Performance

41

J. P. Sislian; R. Dudebout; J. Schumacher; M. Islam; T. Redford

Three-Dimensional Flow Analysis of Turbine Blade Cascades withLeading-Edge Ejection

49

Dieter Bohn; Volker Becker; Karsten Kusterer; Leonhard Fottner;Sabine Ardey

Trailing-Edge Blowing for Reduction of Turbomachinery Fan Noise 57

J. M. Brookfield; I. A. Waitz

Computational Analysis of Stall and Separation Control in CentrifugalCompressors

65

Alex Stein; Saeid Niazi; L. N. Sankar

Evaluation of Boundary Conditions for the Gust-Cascade Problem 72

R. Hixon; S.-H. Shih; R. R. Mankbadi

Identifying Optimal Fan Compressor Pressure Ratios for the Mixed-Stream Turbofan Engine

79

Paul T. Millhouse; Stuart C. Kramer; Paul I. King; Edward F. Mykytka

Engine Case Externals Challenges and Opportunities 87

Mike Miller; Jeff Colehour; Ken Dunkelberg

Very-Near-Field Plume Investigation of the Anode Layer Thruster 91

Matthew T. Domonkos; Alec D. Gallimore; Colleen M. Marrese; JamesM. Haas

Third Way of Development of Single-Stage-to-Orbit Propulsion 99

V. V. Balepin; M. Maita; S. N. B. Murthy

Ideal Gas Thermodynamic Properties of Propellants and ExplosiveCompounds

105

Alexander Burcat

Mass Production of Antimatter for High-Energy Propulsion 119

Brice N. Cassenti

Regression Rate Behavior of Hybrid Rocket Solid Fuels 125

Martin J. Chiaverini; Nadir Serin; David K. Johnson; Yeu-Cherng Lu;Kenneth K. Kuo; Grant A. Risha

Phase-Stabilized Ammonium Nitrate-Based Propellants Using Binderswith N-N Bonds

133

Charlie Oommen; Sampat R. Jain

Improvements in the Chemical Stability of Double-Base Solid RocketPropellants

139

M. H. Sammour

Technical Notes

Wall Curvature Effects on External Burning in Supersonic Flow 147

Giuseppe Bussi; Dario Pastrone; Lorenzo Casalino

Three-Dimensional Disturbance Vortex Method for SimulatingRotor/Stator Interaction in Turbomachinery

150

Xian Hong Wu; Mao Zhang Chen

Measurements of Turbulent Flow Structure in Supersonic Curved WallBoundary Layers

153

R. D. W. Bowersox; R. C. Wier; D. D. Glawe; S. Gogineni

Trajectory of a Liquid Jet Traversing Subsonic Airstreams 155

Takao Inamura

Preliminary Mass Spectrometry of a Xenon Hollow Cathode 157

Mark W. Crofton

Study of Boundary-Layer Development in a Two-Stage Low-PressureTurbine

160

Daniel J. Dorney; David E. Ashpis; David E. Halstead; David C. Wisler

Technical Comments

Comment on “Triggering of Longitudinal Combustion Instabilities inRocket Motors: Nonlinear Combustion Response”

164

V. S. Burnley; F. E. C. Culick

Reply by the Authors to V. S. Burnley and F. E. C. Culick 165

J. M. Wicker; V. Yang

Comment on “Shock-Loss Model for Transonic and Supersonic AxialCompressors with Curved Blades”

166

N. A. Cumpsty; C. Freeman

Reply by the Author to N. A. Cumpsty and C. Freeman 168

M.T. Schobeiri


Full-Length Papers

Mixing of Jet Air with a Fuel-Rich, Reacting Crossflow 617

M. Y. Leong; G. S. Samuelsen; J. D. Holdeman

Aerodynamic Synthesis of a Centrifugal Impeller Using ComputationalFluid Dynamics and Measurements

623

L. M. Larosiliere; G. J. Skoch

Surface Pressure Measurements in Supersonic Transverse InjectionFlowfields

633

M. R. Gruber; L. P. Goss

Expansion and Mixing Processes of Underexpanded Supercritical FuelJets Injected into Superheated Conditions

642

Pei-Kuan Wu; Mehrdad Shahnam; Kevin A. Kirkendall; Campbell D.Carter; Abdollah S. Nejad

Vane Row Indexing for Passive Vibration Control of Axial-FlowTurbomachine Rotors

650


Probabilistic Analysis of Aircraft Gas Turbine Disk Life and Reliability 658

Matthew E. Melis; Erwin V. Zaretsky; Richard August

Effect of Variable Axial Chord on a Low-Pressure Turbine Blade 667

C. G. Murawski; K. Vafai

Aerodynamic Effects on Blade Vibratory Stress Variations 675

James A. Kenyon; Douglas C. Rabe; Sanford Fleeter

Individual Cylinder Model of a General Aviation Aircraft Engine 681

Gary Parker; Giorgio Rizzoni

Apparent Failure of Scaling Methods in Ramjet Connected-Pipe Testing 689

John A. Blevins; Hugh W. Coleman

Shock-Tunnel Skin-Friction Measurement 699

C. P. Goyne; R. J. Stalker; A. Paull

Air Turborocket/Vehicle Performance Comparison 706

Kirk Christensen

Industrial Constraints for Developing Solid Propellants with EnergeticMaterials

713

Bruno D'Andrea; Francesca Lillo

Methodology for Analysis of Postshock Oscillations During Pulse-Triggered Instability

719

P. G. Harris; A. De Champlain

Technical Notes 729


Full-Length Papers

Interferometric Study of Unsteady Passing Shock Flow in a TurbineCascade

489

A. Wesner; J. A. Schetz; H. Grabowski

Fixed-Pitch Propeller/Piston Aircraft Operations at Partial Throttle 497

John T. Lowry

Review of Computational Aeroacoustics in Propulsion Systems 504

R. R. Mankbadi

Numerical Study of Cavitation in the Wake of a HypervelocityUnderwater Projectile

513

Richard Saurel; Pierre Cocchi; P. Barry Butler

Influence of Turbulence Modeling on the Performance Prediction forRocket Engine Nozzles

523

Frank A. Haidinger

Hybrid Monte Carlo-Particle-in-Cell Simulation of an Ion Thruster Plume 530

Douglas B. Vangilder; Gabriel I. Font; Iain D. Boyd

Simulation of Unsteady Flow in Nozzle-Ejector Mixer 539

Thomas Z. Dong; Reda R. Mankbadi

Theoretical Analysis and Engineering Modeling of Flowfields inClustered Module Plug Nozzles

544

Francesco Nasuti; Marcello Onofri

Analysis of a Hybrid Dual-Combustion-Chamber Solid-Propellant GasGenerator

552

Jon J. Freesmeier; P. Barry Butler

Dynamic Modeling of Hybrid Rocket Combustion 562

M. Arif Karabeyoglu; D. Altman

Analyses and Application of Gas Sampling to Scramjet Engine Testing 572

Tohru Mitani; Masahiro Takahashi; Sadatake Tomioka; Tetsuo Hiraiwa;Kouichiro Tani

Drags in Scramjet Engine Testing: Experimental and ComputationalFluid Dynamics Studies

578

Tohru Mitani; Takeshi Kanda; Tetsuo Hiraiwa; Yasutaka Igarashi;Kazuhiro Nakahashi

Closed-Loop Active Control of Combustion Instabilities UsingSubharmonic Secondary Fuel Injection

584

C. M. Jones; J. G. Lee; D. A. Santavicca

Reduced Kinetics Mechanisms for Ram Accelerator Combustion 591

Eric L. Petersen; Ronald K. Hanson

Unified Computer Model for Predicting Thermochemical Erosion in GunBarrels

601

S. Sopok; P. O'Hara; G. Pflegl; S. Dunn; D. Coats; G. Nickerson

Technical Note

Determination of Unsteady Heat Release Distribution in UnstableCombustor from Acoustic Pressure Measurements

613

Timothy C. Lieuwen; Yedidia Neumeier; Ben T. Zinn


Full-Length Papers

Liquid Jet Atomization in a Compressible Gas Stream 369

Tingbao Chen; Xianguo Li

Ion Beamlet Divergence Characteristics of Two-Grid Multiple-Hole Ion-Accelerator Systems

377

Yukio Hayakawa; Shoji Kitamura

Adaptive Control of Combustion Instability with On-Line SystemIdentification

383

Shozo Koshigoe; Toshihiko Komatsuzaki; Vigor Yang

Computation of Vortex Shedding in Solid Rocket Motors Using Time-Dependent Turbulence Model

390

A. Kourta

Performance Evaluation of Scramjet Combustors Using Kinetic Energyand Combustion Efficiencies

401

Goro Masuya; Tomokazu Uemoto; Yoshihiro Wakana; Kenji Kudou;Atsuo Murakami; Tomoyuki Komuro

Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition

408

M. K. Smart

Free-Flight Experiment and Numerical Simulation for Cold ThrusterPlume

417

M. S. Ivanov; G. N. Markelov; Yu. I. Gerasimov; A. N. Krylov; L. V.Mishina; E. I. Sokolov

Startup Modeling of the Receiver of NASA's 2-Kilowatt Solar DynamicPower System

424

Guido W. Lopez

Experimental Investigation of the Role of Downstream Ramps on aSupersonic Injection Plume

432

Mark P. Wilson; Rodney D. W. Bowersox; Diana D. Glawe

Low-Power Helium Pulsed Arcjet 440

Gary F. Willmes; Rodney L. Burton

Comparative Study of Coupled-Mode Flutter-Analysis Methods for FanConfigurations

447

R. Srivastava; T. S. R. Reddy

Predicted Combined Effects of Purge Flow and Rotor-CasingEccentricity on Ingress Heating

454

Zhou Guo; David L. Rhode

Modified Through-Flow Wave-Rotor Cycle with Combustor-BypassDucts

462

Daniel E. Paxson; M. Razi Nalim

Launch Vehicle Dynamic and Control Effects from Solid Rocket MotorSlag Ejection

468

K. W. Dotson; J. W. Murdock; D. K. Kamimoto

Technical Papers

Biharmonic Three-Dimensional Grid Generation for AxialTurbomachinery with Tip Clearance

476

G. A. Gerolymos; G. Tsanga

Technical Notes

Adaptive Analysis of Oscillating Cascade Flows on a Quadrilateral-Triangular Mesh

479

S. Y. Yang

Theoretical Prediction of Mean Droplet Size of Y-Jet Atomizers 481

H. S. Couto; J. A. Carvalho Jr.; M. Q. McQuay; P. T. Lacava

Optimal Performance of Enthalpy Rocket 485

Lorenzo Casalino; Guido Colasurdo

Volume 15 Number 2 – Not AvailableVolume 15 Number 1 – Not AvailableVolume 14 Number 6 – Not Available


Editorial

Another Landmark Collection 585


Space Propulsion Development for the 21st Century 586

Xinmin Ren

Preface 587

Vigor Yang; Guoqiu Liu; William E. Anderson; Mohammed Habiballah

Full-Length Papers

Cycles for Earth-to-Orbit Propulsion 588

Detlef Manski; Christoph Goertz; Hagen-D. Saßnick; James R. Hulka;B. David Goracke; Daniel J. H. Levack

Combined Rocket and Airbreathing Propulsion Systems for Space-Launch Applications

605

Russell Daines; Corin Segal

Preliminary Analysis of an Airbreathing and Rocket Combined-CycleEngine

613

Feng Qi; Jue Wang; Chien-Pin Chen

Advanced Rocket Nozzles 620

Gerald Hagemann; Hans Immich; Thong Van Nguyen; Gennady E.Dumnov

Dynamic Amplification of Fluid Pressure in a Propellant Feed Line 635

T. V. Nguyen; W. E. Huffman

Propellant Technologies: Far-Reaching Benefits for Aeronautical andSpace-Vehicle Propulsion

641

Bryan Palaszewski; Leonid S. Ianovski; Patrick Carrick

Propellant Management in Booster and Upper-Stage PropulsionSystems

649

Mark F. Fisher

Liquid-Propellant Rocket Engine Health-Monitoring Techniques 657

Yulin Zhang; Jianjun Wu; Minchao Huang; Hengwei Zhu; Qizhi Chen

Quality Issues in Propulsion 664

John P. McCarty; Garry M. Lyles

Status and Issues Related to In-Space Propulsion Systems 669

R. L. Sackheim; D. C. Byers

Nontoxic Orbital Maneuvering and Reaction Control Systems forReusable Spacecraft

676

Eric Hurlbert; John Applewhite; Tien Nguyen; Brian Reed; ZhangBaojiong; Wang Yue

Baojiong; Wang Yue

Spacecraft Electric Propulsion - An Overview 688

M. Martinez-Sanchez; J. E. Pollard

Electric Propulsion for Solar System Exploration 700

John R. Brophy; Muriel Noca

Ion Thruster Development Trends and Status in the United States 708

Paul J. Wilbur; Vincent K. Rawlin; J. R. Beattie

Pulsed Plasma Thruster 716

R. L. Burton; P. J. Turchi

Main Physical Features and Processes Determining the Performance ofStationary Plasma Thrusters

736

Vladimir Kim

Scaling of Thrust in Self-Field Magnetoplasmadynamic Thrusters 744

Edgar Choueiri

Technology and Application Aspects of Applied FieldMagnetoplasmadynamic Propulsion

754

Gerd Krülle; Monika Auweter-Kurtz; Akihiro Sasoh

High-Power Hydrogen Arcjet Thrusters 764

Monika Auweter-Kurtz; Thomas Gölz; Harald Habiger; Frank Hammer;Helmut Kurtz; Martin Riehle; Christian Sleziona

Experimental Performance of Field Emission Microthrusters 774

Salvo Marcuccio; Angelo Genovese; Mariano Andrenucci

Research as a Key in the Design Methodology of Liquid-PropellantCombustion Devices

782

M. Habiballah; L. Vingert; V. Duthoit; P. Vuillermoz

Investigation of Heat Transfer and Coking Characteristics ofHydrocarbon Fuels

789

Keming Liang; Baoe Yang; Zhongli Zhang

Liquid-Propellant Rocket Engine Injector Dynamics 797

Vladimir G. Bazarov; Vigor Yang

Mixing and Spray Formation in Coaxial Jets 807

Emmanuel Villermaux

Effects of Periodic Atomization on Combustion Instability in Liquid-Fueled Propulsion Systems

818

W. E. Anderson; K. L. Miller; H. M. Ryan; S. Pal; R. J. Santoro; J. L.Dressler

Experimental Investigation of Shear Coaxial Cryogenic Jet Flames 826

S. Candel; G. Herding; R. Synder; P. Scouflaire; C. Rolon; L. Vingert;M. Habiballah; F. Grisch; M. Péalat; P. Bouchardy; D. Stepowski; A.Cessou; P. Colin

Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions

835

Wolfgang O. H. Mayer; Axel H. A. Schik; Bruno Vielle; ChristianChauveau; Iskender Gökalp; Douglas G. Talley; Rodger D. Woodward

Chauveau; Iskender Gökalp; Douglas G. Talley; Rodger D. Woodward

Modeling High-Pressure Mixing and Combustion Processes in LiquidRocket Engines

843

Joseph C. Oefelein; Vigor Yang

Technical Notes 858


Full-Length Papers

Modified Fracture Mechanics Approach in Structural Analysis of Solid-Rocket Motors

409

Sook-Ying Ho; Gerard Carè

Experimental Study on Boron-Potassium Nitrate Initiated by Shock 416

Liqiong Wang; Changgen Feng; Changsheng Han

Measurement System for Determining Solid Propellant Burning RateUsing Transmission Microwave Interferometry

421

Vladica S. Bozic; Djordje D. Blagojevic; Bozidar A. Anicin

429

P. G. Harris; A. De Champlain

Modeling and Estimation for Electromechanical Thrust Vector Control ofRocket Engines

440

Dale E. Schinstock; Douglas A. Scott; Tim A. Haskew

Investigation of a Solid Fuel Scramjet Combustor 447

Adela Ben-Yakar; Benveniste Natan; Alon Gany

Flame-Holding Configurations for Kerosene Combustion in a Mach 1.8Airflow

456

Michael G. Owens; Sharam Tehranian; Corin Segal; Viatcheslav A.Vinogradov

New Model for Intense Self-Similar Vortices 462

Georgios H. Vatistas

Shock-Loss Model for Transonic and Supersonic Axial Compressorswith Curved Blades

470

M. T. Schobeiri

Properties of Laminar Premixed Hydrocarbon/Air Flames at VariousPressures

479

M. I. Hassan; K. T. Aung; O. C. Kwon; G. M. Faeth

Strategies for Pulsed Detonation Engine Performance Optimization 489

J.-L. Cambier; J. K. Tegnér

Reflections on Free-Piston Stirling Engines, Part 1: Cyclic SteadyOperation

499

F. De Monte; G. Benvenuto

Reflections on Free-Piston Stirling Engines, Part 2: Stable Operation 509

F. De Monte; G. Benvenuto

Generic Magnetic Fusion Rocket Model 519

John F. Santarius; B. Grant Logan

Simplified Approach to Performance Evaluation of Nuclear andElectrical Propulsion Systems

525

Fernando De Souza Costa; João Andrade De Carvalho Jr

Vortex Formation and Stability in a Scaled Gas-Core Nuclear RocketConfiguration

530

L. E. Thode; M. C. Cline; S. D. Howe

Slingatron Mass Launchers 537

Derek A. Tidman

Effect of Propellant Temperature on Efficiency in the Pulsed PlasmaThruster

545

Gregory G. Spanjers; Jamie B. Malak; Robert J. Leiweke; Ronald A.Spores

Propellant Losses Because of Particulate Emission in a Pulsed PlasmaThruster

554

Gregory G. Spanjers; Jason S. Lotspeich; Keith A. McFall; Ronald A.Spores

Arcjet Anode Plasma Measurements Using Electrostatic Probes 560

Nicholas T. Tiliakos; Rodney L. Burton; Herman Krier

Beamlet Profiles from Multiple-Hole Ion-Extraction Systems 568

Yukio Hayakawa; Shoji Kitamura; Katsuhiro Miyazaki

Technical Notes 575


Full-Length Papers

Study on Trapped-Vortex Combustor - Effect of Injection on FlowDynamics

273

Viswanath R. Katta; W. M. Roquemore

Transition Characteristics of Flowfield in a Simulated Solid-RocketMotor

282

Tong-Miin Liou; Wan-Yih Lien; Po-Wen Hwang

Determination of Pressure Dependence of Burning Rate in Solid MotorsUsing Ultrasonic Technique

290

Desh Deepak; R. Jeenu; P. Sridharan; M. S. Padmanabhan

Effect of Catalyst Addition on Subatmospheric Burning SurfaceTemperature of Composite Propellants

295

S. Krishnan; R. D. Swami

Temperature and Species Measurements in a Low-ThrustHydrogen/Oxygen Rocket Engine

301

Wilhelmus A. de Groot

Model of Turbulent Mixing and Reaction for H2-Air Combustion 309

Marc A. Cremer; Patrick A. McMurtry

Methodology to Solve Flowfields of Plug Nozzles for Future Launchers 318

Francesco Nasuti; Marcello Onofri

Transport-Property Measurements in the Plume of an SPT-100 HallThruster

327

Lyon B. King; Alec D. Gallimore; Colleen M. Marrese

Surface Modification Measurements in the T5 Ion Thruster Plume 336

L. Najeeb Ahmed; Mark W. Crofton

Load Oscillations Caused by Unstart of Hypersonic Wind Tunnels andEngines

348

Takashi Shimura; Tohru Mitani; Noboru Sakuranaka; Muneo Izumikawa

Symmetry Approach to Extension of Flutter Boundaries via Mistuning 354

B. Shapiro

Numerical Simulation of Incompressible Two-Blade Rotor Flowfields 367

John A. Ekaterinaris

Stability Behavior of a Shaft-Disk System Subjected to LongitudinalForce

375

Lien-Wen Chen; Hong-Cheng Sheu

Heat Transfer in Counterswirled Coaxial Jet Mixing 384

J. L. Sanger; P. A. Dellenback

Sound-Pressure-Level Variations in a Supersonic Rectangular Cavity atYaw

392

Peter J. Disimile; Paul D. Orkwis

Application of Two-Variable Fuzzy-PI Control in an Aeroengine 399

Fang Zhongxiang; Wu Chihua

Analysis of Ar-Cs Magnetohydrodynamics Disk Generator with StrongInteraction

403

Motoo Ishikawa; Takuro Shiomi; Yoshitaka Inui; Hiroyuki Yamasaki


Full-Length Papers

Jet-Engine Test Cell Augmenter Performance 129

C. A. Kodres; G. L. Murphy

Comparison of Physical and Aerodynamic Ramps as Fuel Injectors inSupersonic Flow

135

Raymond P. Fuller; Pei-Kuan Wu; Abdollah S. Nejad; Joseph A. Schetz

Investigation of Cryogenic Propellant Flames Using ComputerizedTomography of Emission Images

146

Gerald Herding; Ray Snyder; Carlos Rolon; Sebastien Candel

Competitive Reactivity of Stabilizers and Ballistic Modifiers DuringSimulated Aging of Propellants

152

M. H. Sammour

Leading-Edge Flame Detachment: Effect on Pressure-CoupledCombustion Response

160

C. A. Beiter; E. W. Price

Ignition Dynamics of Boron Particles in a Shock Tube 166

Herman Krier; R. L. Burton; M. J. Spalding; T. J. Rood

Spray Structures of Liquid Jets Atomized in Subsonic Crossflows 173

Pei-Kuan Wu; Kevin A. Kirkendall; Raymond P. Fuller; Abdollah S.Nejad

Three-Dimensional Turbine Rotor Forcing Functions and Linear TheoryAnalysis

183

David A. Johnston; Sanford Fleeter

Measured Rotor Wake and Potential Forcing Functions, Including BladeRow Interactions

191

Robert T. Johnston; John M. Feiereisen; Sanford Fleeter

Blading Response to Potential Field Interactions in Axial- and Radial-Flow Turbomachinery

199


Preliminary Estimation of Engine Gas-Flow-Path Size and Weight 208

Vivek Sanghi; S. Kishore Kumar; V. Sundararajan; S. K. Sane

Wake Decay: Effect of Freestream Swirl 215

J. M. Brookfield; I. A. Waitz; J. Sell

Aerodynamic Shape Optimization of a Subsonic Inlet Using Three-Dimensional Euler Computation

225

D. R. Reddy; E. S. Reddy; R. E. Moody

Overexpanded Two-Dimensional Convergent-Divergent NozzlePerformance, Effects of Three-Dimensional Flow Interactions

234

A. Hamed; C. Vogiatzis

Aerodynamics Performance Prediction of Thrust-Vectoring Nozzles 241

A. Matesanz; A. Velazquez; M. Rodriguez

Propellant Utilization in Hall Thrusters 247

Y. Raitses; J. Ashkenazy; M. Guelman

Quasisteady Ablative Magnetoplasmadynamic Thruster Performancewith Different Propellants

254

Giorgio Paccani; Ugo Chiarotti; William D. Deininger

Laser Propulsion System for Space Vehicles 261

Aviad Brandstein; Yeshayahou Levy

Technical Notes

Rocket Propulsion Strategy Based on Kinetic Energy Management 270

Merrill K. King


Editorial 1

Full-Length Papers

Reacting Flow Establishment in Ram Accelerators: A Numerical Study 10

S. Yungster; K. Radhakrishnan; M. J. Rabinowitz

Control of Flame-Holding in Supersonic Airflow by Secondary AirInjection

18

Shuhei Takahashi; Naohiro Sato; Mitsuhiro Tsue; Michikata Kono;Masahiko Nakamura; Hiroshi Kondo; Yasushige Ujiie

Improved Physics Model for the Gasdynamic Mirror Fusion PropulsionSystem

24

Terry Kammash; David L. Galbraith

Modeling Plasma Processes in 1-Kilowatt Hydrazine Arcjet Thrusters 29

Thomas W. Megli; Junqing Lu; Herman Krier; Rodney L. Burton

Thermal Decomposition of 3,3_-Bis-Azidomethyl-Oxetane 37

Young Joo Lee; Ching-Jen Tang; Gautam Kudva; Thomas A. Litzinger

Droplet Combustion, Microexplosion, and Sooting Characteristics ofSeveral Energetic Liquid Propellants

45

T. X. Li; D. L. Zhu; C. K. Law

Characterization of Fuel Regression in a Radial Flow Hybrid Rocket 51

J. R. Caravella Jr; S. D. Heister; E. J. Wernimont

Characteristics of a Trapped-Vortex Combustor 57

K.-Y. Hsu; L. P. Goss; W. M. Roquemore

Assessment of a Radiative Heat Transfer Model for Gas TurbineCombustor Preliminary Design

66

Peter J. Stuttaford; Philip A. Rubini

Digital Simulator for Steady-State Performance Prediction of MilitaryTurbofan Engine

74

Vivek Sanghi; B. K. Lakshmanan; V. Sundararajan

Influence of Inlet Pressure Distortion on a Convertible Engine Fan 82

Tarik Kaya

Numerical Investigation of Inlet Buzz Flow 90

Pong-Jeu Lu; Ling-Tzong Jain

Method for Noise Suppressing Nozzle Calculation and First Results ofIts Implementation

101

S. Bosniakov; S. Fonov; V. Jitenev; A. Shenkin; V. Vlasenko; N.Yatskevich

Experimental Analysis of the Turbulent Shear Stresses for DistortedSupersonic Boundary Layers

110

Joel J. Luker; Chad S. Hale; Rodney D. W. Bowersox

Solar Cell Temperature on Mars 119

E. Matz; J. Appelbaum; Y. Taitel; D. J. Flood

Mars Dust-Removal Technology 126

Geoffrey A. Landis


FULL-LENGTH PAPERS

Study of a Supersonic Combustor Employing Swept Ramp FuelInjectors

697

Dean R. Eklund; Scott D. Stouffer; G. Burton Northam

Open-Loop Performance of a Fast-Response, Actively Controlled FuelInjector Actuator

705

Yedidia Neumeier; Aharon Nabi; Amos Arbel; Moti Vertzberger; Ben T.Zinn

Effects of Inlet Configuration on Ignition and Fuel Regression Behind aBackstep

714

Cliff Yuh-Yih Wu; Jing-Tang Yang

Laser-Induced Spark Flameholding in Supercritical, Subsonic Flow 721

Lara D. Medoff; Andrew McIlroy

Uncertainty Assessment of Ramjet Performance Determination inConnected-Pipe Testing

730

John A. Blevins; Hugh W. Coleman

Assessment of Jet Noise Analysis Codes for Multistream Axisymmetricand Forced Mixer Nozzles

737

T. J. Barber; L. M. Chiappetta; S. H. Zysman

Zonal Approach for Prediction of Jet Noise 745

S. H. Shih; D. R. Hixon; R. R. Mankbadi

Effect of Wall Roughness on the Flow Through Converging - DivergingNozzles

753

Venkata S. Krishnamurty; Wei Shyy

Absolute Instability in a Supersonic Shear Layer and Mixing Control 763

Long-Shin Lee; Philip J. Morris

Velocity and Temperature Measurements in a Low-Power HydrazineArcjet

768

S. A. Bufton; R. L. Burton

Extensive Validation of a Monte Carlo Model for Hydrogen ArcjetFlowfields

775

Iain D. Boyd

Measurements of Electron Density in the Charge Exchange Plasma ofan Ion Thruster

783

P. C. T. De Boer

Numerical Analysis of a Two-Dimensional MagnetoplasmadynamicArcjet

789

I. Funaki; K. Toki; K. Kuriki

Prediction of Pressurant Mass Requirements for Axisymmetric LiquidHydrogen Tanks

796

Neil T. Van Dresar

TECHNICAL NOTES

Cored Brick Storage Heater Analysis 800

Robert H. Korkegi

Operation of Quasi-Two-Dimensional Projectiles in a Ram Accelerator 802

Xinyu Chang; Andrew Higgins; Eric Schultz; Adam Bruckner

Further Examination of Enthalpy Rocket Performance 804

Merrill K. King

Effects of Kinetic Rate Uncertainty on the Predicted Performance ofSolar Thermal Rockets

806

D. Brian Landrum; Robert M. Beard

Off-Design Performance Prediction of Single-Spool Turbojets UsingGasdynamics

808

Mirza F. Baig; H. I. H. Saravanamuttoo

ERRATA

Compatibility of Gelled Inhibited Red Fuming Nitric Acid with AluminumAlloys

811

Barry D. Allan; and


FULL-LENGTH PAPERS

Challenge to Create the Space Drive 577

Marc G. Millis

Performance Limits for Projectile Flight in the Ram and ExternalPropulsion Accelerators

583

J. Rom

Performance Optimization of a Supersonic Combustion RamAccelerator Projectile

592

John W. Sabean; Mark J. Lewis

Analytical Solution of the Type IV Shock Interaction 601

Michael J. Frame; Mark J. Lewis

Applications of Algebraic Reynolds Stress Turbulence Models Part 1:Incompressible Flat Plate

610

John R. Carlson

Applications of Algebraic Reynolds Stress Turbulence Models Part 2:Transonic Shock-Separated Afterbody

620

John R. Carlson

Plug Nozzle Flowfield Analysis 629

T. Rommel; G. Hagemann; C.-A. Schley; G. Krülle; D. Manski

Comparison of Scramjet Engine Performance in Mach 6 Vitiated andStorage-Heated Air

635

Tohru Mitani; Tetsuo Hiraiwa; Shigeru Sato; Sadatake Tomioka;Takeshi Kanda; Kouichiro Tani

Flammability Limits and Probability Density Functions in SimulatedSolid-Fuel Ramjet Combustors

643

Tong-Miin Liou; Wan-Yih Lien; Po-Wen Hwang

Performance and Acceleration Process of QuasisteadyMagnetoplasmadynamic Arcjets with Applied Magnetic Fields

651

Hirokazu Tahara; Yoichi Kagaya; Takao Yoshikawa

Experimental Study of Hydrogen Heating in Powerful Electric DischargeLauncher

659

Ph. G. Rutberg; A. A. Bogomaz; A. V. Budin; V. A. Kolikov; A. G.Kuprin; A. A. Pozubenkov

Jet Engine Component Maps for Performance Modeling and Diagnosis 665

G. Sieros; A. Stamatis; K. Mathioudakis

High-Temperature Braided Rope Seals for Static Sealing Applications 675

Bruce M. Steinetz; Michael L. Adams; Paul A. Bartolotta; Ram Darolia;Andrew Olsen

Identification of Continuous-Time, Linear, and Nonlinear Models of anElectromechanical Actuator

683

Dale E. Schinstock; Tim A. Haskew

Theoretical Formulation for Sauter Mean Diameter of Pressure-SwirlAtomizers

691

H. S. Couto; J. A. Carvalho Jr; D. Bastos-Netto


FULL-LENGTH PAPERS

Measurement System for Determining Solid Rocket Propellant BurningRate Using Reflection Microwave Interferometry

457

Vladica S. Bozic; Djordje Dj. Blagojevi; Bozidar A. Anicin

High-Speed Photographic Study of the Impact Response of AmmoniumDinitramide and Glycidyl Azide Polymer

463

J. P. Agrawal; S. M. Walley; J. E. Field

Mechanism of Burning Rate Enhancement of Composite SolidPropellants by Ferric Oxide

471

Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman

Compatibility of Gelled Inhibited Red Fuming Nitric Acid with AluminumAlloys

481

Ramona E. Arndt Hallit; Clark W. Hawk

Experimental Study on Rotating Cavitation of Rocket Propellant PumpInducers

488

T. Hashimoto; M. Yoshida; M. Watanabe

Hybrid Friction - Impact Vibration Damper for Cryogenic RotatingMachinery

495

J. Jeffrey Moore; Alan B.; Ravindera K. Gadangi

Mean Stator Loading Effect on the Acoustic Response of a RotatingCascade

502

Scott Sawyer; Sanford Fleeter

Macroscopic Balance Model for Wave Rotors 508

Gerard E. Welch

Turbulent Mixing of Coaxial Nozzle Flows with a Central-Lobed Mixer 517

S. C. M. Yu; X. G. Xu

Effects of Mixing Schemes on Kerosene Combustion in a SupersonicAirstream

525

M. Owens; C. Segal; A. H. Auslender

Hydrogen Autoignition and Combustion in Supersonic Flow at LowEquivalence Ratio

532

Giulio Riva; Giambattista Daminelli; Adolfo Reggiori

Experimental Studies on Self-Ignition of Hydrogen/Air SupersonicCombustion

538

Li Jian-Guo; Yu Gong; Zhang Yue; Li Ying; Qian Da-Xing

Mach 6 Testing of a Scramjet Engine Model 543

Takeshi Kanda; Tetsuo Hiraiwa; Tohru Mitani; Sadatake Tomioka;Nobuo Chinzei

Uncertainty Assessment of Performance Evaluation Methods for SolarThermal Absorber/Thruster Testing

552

Pete Markopoulos; Hugh W. Coleman; Clark W. Hawk

Solar Space Power System Optimization with Ultralight Radiator 560

A. F. Massardo; L. A. Tagliafico; M. Fossa; A. Agazzani

Biphase Inverter Based on Cesium Plasma Switches 565

N. I. Alekseyev; V. B. Kaplan; A. M. Martsinovskij; S. V. Electrov

United States Laboratory Element Electrical Power System VerificationApproach

570

Herb W. Wallen; S. Johnny Fu

TECHNICAL NOTES

Thrust Enhancement in Hypervelocity Nozzles by Chemical Catalysis 574

D. J. Singh; Mark H. Carpenter; J. P. Drummond


Full-Length Papers

Unsteady Aerodynamic Flow Phenomena in a Transonic CompressorStage

329

Chunnil Hah; Steven L. Puterbaugh; William W. Copenhaver

Modular Prediction Scheme for Blade Row Interaction Noise 334

A. B. Parry

Skin-Friction Predictions in a Crossing-Shock Turbulent Interaction 342

Datta Gaitonde; J. S. Shang

Stability Testing of Full-Scale Tactical Motors 349

F. S. Blomshield; J. E. Crump; H. B. Mathes; Richard A. Stalnaker; M.W. Beckstead

Nonlinear Stability Testing of Full-Scale Tactical Motors 356

F. S. Blomshield; H. B. Mathes; J. E. Crump; C. A. Beiter; M. W.Beckstead

Beckstead

Modeling and Experiments of Laser-Induced Ignition of NitraminePropellants

367

S. J. Ritchie; S. T. Thynell; K. K. Kuo

Improvements to Steady-State Combustion Modeling ofCyclotrimethylenetrinitramine

375

Jeffrey E. Davidson; M. W. Beckstead

Fiber-Optic Probe for Laser-Induced Fluorescence Measurements ofthe Fuel-Air Distribution in Gas-Turbine Combustors

384

Jong Guen Lee; Domenic A. Santavicca

Optical and Pressure Measurements in Shock Tunnel Testing of aModel Scramjet Combustor

388

T. J. McIntyre; A. F. P. Houwing; P. C. Palma; P. A. B. Rabbath; J. S.Fox

Comparison of Potential Fuels for Martian Rockets Using CO2 395

Evgeny Ya. Shafirovich; Udo I. Goldshleger

Partial Differential Equation Surface Generation and Functional ShapeOptimization of a Swirl Port

398

C. W. Dekanski; M. I. G. Bloor; M. J. Wilson

Thermal Analysis of the Heat Exchangers and Regenerator in StirlingCycle Machines

404

Filippo de Monte

Counterflow Thrust Vector Control of Subsonic Jets: Continuous andBistable Regimes

412

M. R. Van der Veer; P. J. Strykowski

High-Thrust-High-Specific Impulse Gasdynamic Fusion PropulsionSystem

421

Terry Kammash; Myoung-Jae Lee; David I. Poston

Antiproton Catalyzed Fusion Propulsion for Interplanetary Missions 428

B. N. Cassenti; T. Kammash; D. L. Galbraith

Fundamental Constraints on Large-Scale Antimatter Rocket Propulsion 435

Todd H. Rider

Technical Notes

Overexpanded Two-Dimensional-Convergent-Divergent Nozzle FlowSimulations, Assessment of Turbulence Models

444

A. Hamed; C. Vogiatzis

Lobed Mixers Using Simultaneous Laser-Induced Fluorescence andMie Scattering

445

David M. Milam; Mo Samimy; Steven Martens

Combustion and Microexplosion of Han-Based Liquid Gun Propellantsat Elevated Pressures

448

C. Call; D. L. Zhu; C. K. Law; S. C. Deevi

Interpretation of Finite Element Analysis Results of ScramacceleratorThrust

451

Josef Rom; Mark J. Lewis

Technical Comments

Comment on "Intrinsic Combustion Instability of Solid EnergeticMaterials"

454

M. Q. Brewster; S. F. Son

Reply by the Author to M. Q. Brewster and S. F. Son 456

L. DeLuca


Full-Length Papers

Exit Flowfield of an Embedded Stator in a Multistage Axial FlowCompressor

169

J. Prato; B. Lakshminarayana; N. Suryavamshi

Gust Response Decomposition in a Stator/Rotor Axial Compressor withVarying Axial Gap

178

Andrew M. Wo; Meng-Hsuan Chung; Shu-Tzung Hsu

Multiple-Scales Solution to the Acoustic Boundary Layer in SolidRocket Motors

186

J. Majdalani; W. K. van Moorhem

Flow Analysis of a Solid Propellant Rocket Motor with Aft Fins 194

Bruno Chaouat

Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at theSegment Interfaces

197

K. W. Dotson; S. Koshigoe; K. K. Pace

Effect of Catalyst Mixing Procedure on Subatmospheric CombustionCharacteristics of Composite Propellants

207

S. Krishnan; R. D. Swami

Combustion Initiated by a Porous Ceramic Regenerator in aReciprocating Engine Environment

213

Steven Sepka; Francisco Ruiz

Monte Carlo Probability Density Function Method for Gas TurbineCombustor Flowfield Predictions

218

Anil K. Tolpadi; Sanjay M. Correa; David L. Burrus; Hukam C. Mongia

Partially Premixed Laminar Gas Flames from Triangular Burners 226

S. R. Gollahalli; Samir Subba

Counterflow Diffusion Flame of Methane and Methane/Hydrogen MixedFuel in Supersonic Flow

233

Kenichi Takita; Takashi Niioka

Properties of Laminar Premixed CO/H2/Air Flames at VariousPressures

239

M. I. Hassan; K. T. Aung; G. M. Faeth

Ignition Characteristics of a New High-Energy Density Fuel in High-Speed Flows

246

C. Segal; M. J. Friedauer; H. S. Udaykumar; W. Shyy; A. P. Marchand

Spray Characteristics of Liquid Jet Traversing Subsonic Airstreams 250

Takao Inamura; Nobuki Nagai

Normal, Sonic Helium Injection Through a Wedge-Shaped Orifice intoSupersonic Flow

257

Matthew J. Barber; Joseph A. Schetz; Larry A. Roe

Velocity Measurements of a Jet Injected into a Supersonic Crossflow 264

Juan Gabriel Santiago; J. Craig Dutton

Fuel Stagnation Temperature Effects on Mixing with SupersonicCombustion Flows

274

M. N. Wendt; R. J. Stalker; P. A. Jacobs

Thrust Losses in Hypersonic Engines Part 1: Methodology 281

D. W. Riggins; C. R. McClinton; P. H. Vitt

Thrust Losses in Hypersonic Engines Part 2: Applications 288

D. W. Riggins

Evaluation of Performance Loss Methods for High-Speed Engines andEngine Components

296

D. W. Riggins

Mixing Characteristics of Forced Mixers with Scalloped Lobes 305

Simon C. M. Yu; T. H. Yip; C. Y. Liu

Flow Through a Rectangular-to-Semiannular Diffusing Transition Duct 312

Jeff Foster; Bruce J. Wendt; Bruce A. Reichert; Theodore H. Okiishi

Power System Analysis of Multikilowatt Space/Planet Stations 318

George L. Kusic; Ronald C. Cull

Technical Notes 324


Editorial 1

Full-Length Papers

Analytical Model of Unsteady Shock Motion on Hypersonic Forebodies 10

Sowmyalatha Jayaraman; Mark J. Lewis

Unsteady Flow and Shock Motion in a Transonic Compressor Rotor 17

W. W. Copenhaver; S. L. Puterbaugh; C. Hah

Tip Clearance Flow-Shock Interaction in a Transonic Compressor Rotor 24

S. L. Puterbaugh; M. Brendel

Computational Study of Rotating-Stall Inception in Axial Compressors 31

L. He

Chordwise Bending Cascade Unsteady Aerodynamics by anExperimental Influence Coefficient Technique

39

Daniel A. Ehrlich; Sanford Fleeter

Secondary Flow Computation Using an Inviscid Multigrid Finite VolumeLambda Formulation

49

Francesco Casalini; Andrea Dadone

Tangential Injection from Overlaid Slots into a Supersonic Stream 59

David P. Lewis; Joseph A. Schetz

Breakup Processes of Liquid Jets in Subsonic Crossflows 64

Pei-Kuan Wu; Kevin A. Kirkendall; Raymond P. Fuller; Abdollah S.Nejad

Stability of Thin Liquid Sheet Flows 74

Marc W. McConley; Donald L. Chubb; Matthew S. McMaster; AbdollahA. Afjeh

Effect of Acoustic Perturbations on Liquid Jet Atomization 82

S. D. Heister; M. W. Rutz; J. H. Hilbing

Droplet Autoignition in a Reactive Oxidant/Fuel-Vapor/InertEnvironment

89

Xianguo Li

Mass-Flux-Based Implicit Multigrid Method for ModelingMultidimensional Combustion

97

Xiaoqing Zheng; Changming Liao; Zhining Liu; Chaoqun Liu

Comparison Between Presumed and Monte Carlo Probability DensityFunction Combustion Models

109

Fernando Biagioli

Prediction of Soot Emissions in Gas-Turbine Combustors 117

A. de Champlain; D. Kretschmer; J. Tsogo; G. F. Pearce

Multidimensional Modeling of Fuel Effects and Split Injections on DieselEngine Cold-Starting

123

Nabil S. Ayoub; Rolf D. Reitz

Numerical Study of Hypervelocity Flows Through a ScramjetCombustor

131

R. Krishnamurthy; R. C. Rogers; S. N. Tiwari

Experimental Studies on Piloted Supersonic Combustion Using thePetal Nozzle

142

Anil K. Narayanan; K. A. Damodaran

Mixed Integer Programming-Based Power Scheduler for the SpaceStation

150

James Momoh; D. Chattopadhyay; James L. Dolce

Optimal Control of Quasi-One-Dimensional Self-FieldMagnetoplasmadynamic Arcjet Flowfields

157

Kyoichiro Toki

Technical Notes 162

Technical Comments 167

AIAA JOURNAL OF PROPULSION AND POWER · Conceptual Study of a Combined-Cycle Engine for an...

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