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    Titel :

    Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-Off Distance



    Kongress:

    16th, AIAA International Space Planes and Hypersonic Systems and Technologies Conference ; 2009 ; Bremen, Germany



    Erscheinungsdatum :

    2009-01-01


    Format / Umfang :

    8 pages


    Anmerkungen:

    Includes bibliographic references and index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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