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    Title :

    Experimental and Numerical Investigation of Leading-Edge Bluntness on Shock Boundary layer Interaction Inside a Scramjet Inlet at Mach 6


    Contributors:

    Conference:

    25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference



    Publication date :

    2023-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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