Tunnel developed by General Electric Research Laboratory, Schenectady, NY, consists of driver, diaphragm section, shock tube of constant area and nozzle partly installed in dump tank; instrumentation used; preliminary results in investigation of high temperature gas effects on flow around bodies traveling at hypersonic Mach numbers encountered by intercontinental ballistic missiles and satellites re-entering Earth's atmosphere.


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    Titel :

    Hypersonic shock tunnel


    Weitere Titelangaben:

    ARS -- J


    Beteiligte:
    Nagamatsu, H.T. (Autor:in) / Geiger, R.E. (Autor:in) / Sheer, Jr., R.E. (Autor:in)

    Erschienen in:

    ARS Journal ; 29 , n 5 ; p 332-340


    Erscheinungsdatum :

    1959


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    NOL Hypersonic Shock Tunnel Facilities

    J. W. Watt / P. M. Aronson | NTIS | 1964


    The Boeing Hypersonic Shock Tunnel

    Cassady, P. E. / Institute of Theoretical and Applied Mechanics | British Library Conference Proceedings | 1996


    Triple-diaphragm hypersonic shock tunnel

    Kamimoto, Goro / Hasegawa, T. | TIBKAT | 1962



    Hypersonic Model Testing in a Shock Tunnel

    Olivier, H. | Online Contents | 1995