Lift performance is improved on a 60 degrees swept Gothic wing. Vortex lift at moderate to high angles of attack on highly swept wings used to improve takeoff performance and maneuverability. New design proposed in which suction of propulsion system augments vortex. Turbofan placed at down stream end of leading-edge vortex system induces vortex to flow into inlet which delays onset of vortex breakdown.


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    Title :

    Vortex Lift Augmentation by Suction


    Contributors:

    Published in:

    Publication date :

    1983-08-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Vortex lift augmentation by suction on a 60 deg swept Gothic wing

    Taylor, A. H. / Jackson, L. R. / Huffman, J. K. | NTRS | 1982


    Vortex lift augmentation by suction on a 60 deg swept Gothic wing

    TAYLOR, A. / JACKSON, L. / HUFFMAN, J. | AIAA | 1982




    Lift Augmentation

    Swatton, P. J. | Wiley | 2010