Aircraft for sustained supersonic flight usually feature low aspect ratio wings with varying (reducing) leading edge sweep over the outer portion to achieve an adequate low-speed performance. A high-speed 'cruise' wing then becomes subject to mixed flows at low-speeds including strong Vortical flows.


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    Title :

    Vortex Flow Dilemmas and Control on Wing Planforms on High Speed


    Contributors:
    R. K. Nangia (author) / A. Miller (author)

    Publication date :

    2003


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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