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    Titel :

    Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics (AIAA 2016-4321)


    Beteiligte:

    Kongress:

    32nd AIAA aerodynamic measurement technology and ground testing conference 2016 ; 2016 ; Washington D.C



    Erscheinungsdatum :

    01.01.2016


    Format / Umfang :

    21 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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