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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    Titel :

    Vortex Flow Dilemmas and Control on Wing Planforms on High Speed


    Beteiligte:
    R. K. Nangia (Autor:in) / A. Miller (Autor:in)

    Erscheinungsdatum :

    2003


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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