Real air hypersonic flow parameters are presented in tabular and graphical form for flight in earth's atmosphere as function of flight velocity and altitude; thermochemical equilibrium-flow properties are given for inviscid normal shock and stagnation point, and equilibrium and frozenflow parameters, including electron concentration, are listed for far wake of inviscid stagnation streamline.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Huber, P.W. (Autor:in)


    Format / Umfang :

    74 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :