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    Title :

    Experimental and Numerical Investigations of a Scramjet Model Tested in the H2K Blow Down Wind Tunnel at Mach 7 Flight Condition


    Contributors:

    Conference:

    19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference



    Publication date :

    2014-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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