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    Title :

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



    Conference:

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



    Publication date :

    2009-01-01


    Size :

    8 pages


    Remarks:

    Includes bibliographic references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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