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    Title :

    Shock-Boundary Layer Interaction due to a Sharp Unswept Fin in a Mach 2 Flow (AIAA 2015-1517)


    Contributors:

    Conference:

    Aerospace sciences meeting



    Publication date :

    2015-01-01


    Size :

    12 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



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