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    Titel :

    Interaction of an Oblique Shock with a Transitional Mach 5.92 Boundary Layer (AIAA 2016-3647)



    Kongress:

    Fluid dynamics (Conference)



    Erscheinungsdatum :

    01.01.2016


    Format / Umfang :

    14 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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    Interaction of an oblique shock with a transitional Mach 5.92 boundary layer

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    AIAA 2006-1107 Numerical Simulation and Experiment Comparison of Leading-Edge Receptivity of A Mach 5.92 Boundary Layer

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