Both zero-order and first-order solution presented for 2-dimensional and axisymmetric hypersonic flow where M is free stream Mach number and delta is characteristic slope; solutions are compared with exact numerical integrations of equations of motion, and appear to be accurate particularly when shock is relatively close to body.


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    Titel :

    Approximate analytical solutions for hypersonic flow over slender power law bodies


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Mirels, H. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :