Problem of simulating aerodynamic effects of blast on hypersonic vehicle is of current interest; flow behind blast wave, propagating in downstream direction in hypersonic tunnel, is investigated; assuming that tunnel area downstream of throat has power law variation with streamwise distance and that shock is strong, self-similar solutions of L.Sedov and of W.D.Hayes and R.F. Probstein, for blast wave propagation in stationary atmosphere with power law density variation, are directly applicable; expressions given define ideal energy required to generate strong blast of specified strength in given hypersonic tunnel.


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    Titel :

    Aerodynamic blast simulation in hypersonic tunnels


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Mirels, H. (Autor:in) / Mullen, J.F. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 11


    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic blast simulation in hypersonic tunnels.

    MIRELS, H. / MULLEN, J. F. | AIAA | 1965


    Errata: Aerodynamic Blast Simulation in Hypersonic Tunnels

    H. MIRELS AND J.F. MULLEN | AIAA | 1966



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