Shock waves generated in air flow over or through hypersonic vehicle cannot be analyzed by well-known perfect gas relations because of vibrational relaxation and chemical dissociation effects on properties behind shock waves; paper presents simple, rapid and informative analysis for equilibrium or nonequilibrium conditions in range of oxygen dissociation; freestream dissociation effects, which may be important in wind-tunnel testing of vehicles, also are considered; relaxation results presented are compared to those given by other investigators.


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    Titel :

    Simplified technique for evaluating vibrational and/or chemical relaxation behind shock waves


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Adams, D.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :