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    Title :

    Numerical Study of Hypersonic Leeward Flow over a Blunt Nosed Delta Wing



    Published in:

    Publication date :

    1995



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.60 / 50.93 / 55.50 / 50.93 Weltraumforschung
    Local classification TIB:    770/7040



    Numerical study of hypersonic leeward flow over a blunt nosed delta wing

    Mallett, E. R. / Pullin, D. I. / Macrossan, M. N. | AIAA | 1995


    Numerical study of hypersonic leeward flow over a blunt nosed delta wing

    Mallett, E.R. / Pullin, D.I. / Macrossan, M.N. | Tema Archive | 1995


    Approximate viscous shock-layer method for hypersonic flow over blunt-nosed bodies

    Grantz, A. C. / Dejarnette, F. R. / Thompson, R. A. | NTRS | 1990


    Approximate viscous shock-layer method for hypersonic flow over blunt-nosed bodies

    GRANTZ, A. C. / DEJARNETTE, F. R. / THOMPSON, R. A. | AIAA | 1990