On modem military air vehicles, high lift systems are used to improve takeoff and landing performance. For naval air vehicles, an improvement in the lift coefficient of a landing or approach configuration allows for arrested landings at reduced speeds or the ability to carry more weight back to the ship. For conventional takeoff or landing (CTOL), improved lift to drag ratios allow for shorter takeoff runs or greater payload capacity.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Low-Speed Wind Tunnel Tests on a Diamond Wing High Lift Configuration


    Contributors:
    T. A. Ghee (author) / N. J. Taylor (author)

    Publication date :

    2000


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    AIAA-2004-4843 Low-Speed Wind Tunnel Tests on a Lambda Wing High-Lift Configuration

    Ghee, T. / Taylor, N. | British Library Conference Proceedings | 2004


    Wind-tunnel tests of hall high-lift wing

    Weick, F.E. / Sanders, R. | Engineering Index Backfile | 1932


    Wind tunnel tests of a hall high lift wing

    Weick, Fred E. ;Sanders, Robert | SLUB | 1932