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    Title :

    EXPERIMENTAL INVESTIGATION OF CORNER FLOWS IN RECTANGULAR SUPERSONIC INLETS WITH 3D SHOCK-BOUNDARY LAYER EFFECTS



    Conference:

    49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL



    Publication date :

    2011-01-01


    Size :

    11 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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