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    Title :

    Pressure Sensitive Paint Application to a Wing-Body Model in a Hypersonic Shock Tunnel


    Contributors:

    Conference:

    22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ; 2002 ; St. Louis , Missouri



    Publication date :

    2002-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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