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    Title :

    Experimental Investigation of a Mach 4 Shock-wave Turbulent Boundary Layer Interaction Near an Expansion Corner (AIAA 2015-0112)


    Contributors:

    Conference:

    Aerospace sciences meeting



    Publication date :

    2015-01-01


    Size :

    11 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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