The paper reviews the experimental data on the incipient separation characteristics of planar delta wings of 75 degree sharp leading edges, with full-span trailing edge flap deflected into the windward flow. The local Reynolds number range for these investigations covered laminar, transitional and turbulent conditions. It is shown that, while turbulent boundary layer data correlates with two dimensional results, in the laminar and transitional cases, there is a nearly parallel shift to higher flap angles for incipient separation.


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    Titel :

    Hypersonic incipient separation on delta wing with trailing-edge flap


    Beteiligte:
    Rao, D. M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1975-10-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Hypersonic incipient separation on delta wing with trailing-edge flap

    RAO, D. M. / NASA, Langley Research Center / Hampton, Va. | AIAA | 1975


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