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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    Title :

    Viscous vortical flow calculations over delta wings


    Contributors:
    Blom, G. (author) / Wai, J. C. (author) / Yoshihara, H. (author)


    Publication date :

    1986-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


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