Purpose of study is to outline approximate methods that allow prediction of effects of high angle of attack, nonequilibrium flow chemistry, and vapor injection on subsonic flow field of blunt body in hypersonic speed range, to present results in terms of shockwave shape and location, stagnation-point location, and surface pressure for equilibrium flow, and in terms of shock-wave shape and location for nonequilibrium flow, and flow with vapor injection, and to compare, where possible, these results with available experiment or more exact theory.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Inviscid hypersonic flow around blunt bodies


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Katzen, E.D. (Autor:in) / Kaattari, G.E. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 7


    Erscheinungsdatum :

    1965


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Inviscid hypersonic flow around blunt bodies

    KAATTARI, G. E. / KATZEN, E. D. | AIAA | 1965


    Inviscid hypersonic flow around blunt bodies.

    Kaattari, G. E. / Katzen, E. D. | NTRS | 1965