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    Title :

    Experimental Investigation of Corner Flows in Rectangular Supersonic Inlets with 3D Shock-Boundary Layer Effects


    Contributors:

    Conference:

    49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition



    Publication date :

    2011-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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