Two approaches to calculate turbulent vortical flows over delta wing configurations are illustrated. The first is for a simple delta wing at low speeds using the boundary layer approximation to treat the effects of the secondary separation. The second is for the supersonic case of a generic fighter using the NASA Ames parabolized Navier/Stokes method. Test/theory comparisons are given in both cases.


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    Titel :

    Viscous vortical flow calculations over delta wings


    Beteiligte:
    Blom, G. (Autor:in) / Wai, J. C. (Autor:in) / Yoshihara, H. (Autor:in)


    Erscheinungsdatum :

    01.07.1986


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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