telfona: testing for laminar flow on new aircraft

download telfona: testing for laminar flow on new aircraft

of 4

Transcript of telfona: testing for laminar flow on new aircraft

  • 8/8/2019 telfona: testing for laminar flow on new aircraft

    1/4

    Testing For Laminar Flow On New Aircraft

    A European project supported within the Sixth Framework Programme for Research and Technological Development

  • 8/8/2019 telfona: testing for laminar flow on new aircraft

    2/4

    The requirement to improve upon the environmental performance of aircraft is one of a number of key goals

    of the Advisory Council for Aeronautics Research in Europes (ACARE) Strategic Research Agenda.

    The environmental challenge is to meet continually rising demand for air travel whilst demonstrating

    sensitivity to societys needs by reducing the environmental impact of operating, maintaining, manufacturing

    and disposing of aircraft and associated systems.

    Specific environmental goals have been defined :

    To reduce fuel consumption and CO2 emissions by 50%.

    To reduce perceived external noise by 50%.

    To reduce NOx by 80%.

    To make substantial progress in reducing the

    environmental impact of the manufacture, maintenance

    and disposal of aircraft and related products.

    Airbus and its European research partners are

    making signicant investments to meet these

    challenges. In the area of aerodynamic cruise

    performance, the goal is to reduce the fuel

    consumption. This can be done by improving the

    efciency of the engines and by introducing drag

    reduction technologies.

    The European FP6 project TELFONA will contribute to

    these research activities by examining the opportunities

    related to the concept of a Natural Laminar Flow large

    commercial aircraft. This technology is in service today on

    small business aircraft such as the Piaggio P180. The task

    for the TELFONA project team is to understand whether

    this technology can be scaled up to a large aircraft and then

    to assess the drag reduction potential of this concept.

    Context

    Similar goals have been dened by ACARE in the areas

    of Quality and Affordability, Safety, Air Transport

    System efciency and Security.

  • 8/8/2019 telfona: testing for laminar flow on new aircraft

    3/4

    Expected Results

    In order to ensure the success of the project in delivering

    against the overall objective, the technological development

    and innovation-related activities within the project have been

    divided into 5 Work Packages. In order to ensure a clear focus

    on project management, dissemination and exploitation

    activities within the TELFONA project, a sixth Work Package

    has been dened to contain these activities.

    Project Objectives

    The major objective of TELFONA is the development of the capability to predict the in-ight performance of

    an NLF aircraft using wind tunnel tests and CFD calculations.

    A number of supporting objectives have been dened :

    Transition prediction tool calibration for NLF aircraft

    testing in ETW using a specially designed wind tunnel

    model.

    Improvement of transition receptivity models using wind

    tunnel test data from ETW and small scale facilities to

    better understand how surface quality and atmospheric

    conditions inuence transition mechanisms.

    Development of methods for predicting the in-flight

    performance of an NLF aircraft including understanding

    whether conventional scaling approaches using low

    Reynolds number wind tunnels can be used.

    Validation of the developed methods through the design,

    manufacture and test of an NLF wing designed for high

    performance.

    Development of technology for wind tunnel testing hybridlaminar ow control wings.

    The successful completion of the project will result in

    two wind tunnel model tests and improved transition

    prediction methods. The rst pathnder model will betested in ETW with the results being used to calibrate

    transition prediction methods and to provide insight

    into the receptivity problem. The second performance

    model will be designed using the calibrated methods

    and will be used to demonstrate the potential of a largeNLF aircraft.

    Work Plan

  • 8/8/2019 telfona: testing for laminar flow on new aircraft

    4/4

    Aircraft Manufacturers

    Airbus UK (UK), Airbus E (Spain),

    Airbus D (Germany), Piaggio (Italy)

    Industrial Organisation

    ETW (Germany)

    Research Organisations

    VZLU (Czech Republic),

    ONERA (France), FOI (Sweden),

    CIRA (Italy), DLR (Germany)

    Universities

    Imperial College (UK), IST (Portugal),

    TU-Berlin (Germany), KTH (Sweden)

    Consulting Company

    ALMA Consulting Group (France)

    Project Coordinator:

    Airbus UK : Mr. D. Sawyers, +44 117 936 [email protected]

    With the support of:

    ALMA Consulting Group : A. Hoque, +33 4 72 35 80 [email protected] management is operated on the PRODIGE Internet platform :www.prodige.com

    The TELFONA consortium consists of 15 organisations from 8 different member states. The consortium

    contains 4 aircraft manufacturers, 1 industrial organisation (wind tunnel facility), 5 research organisations

    and 4 universities and 1 consulting company.

    Acknowledgment

    ,

    Consortium

    Supported by the European Commission through the Sixth Framework

    Programme for Research and Development up to 3 025 Keuros (out of

    a total budget of 5 174 Keuros) the TELFONA project address the area

    Strengthening Competitiveness of the Aeronautics and Space thematic

    priority.

    The project has been running since 1st May 2005 and it will last for 42

    months.

    Cration::Comte::047

    8

    39

    56

    13