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    Titel :

    Numerical Study of Shockwave Induced Boundary Layer Separation Control using Plasma Actuators



    Kongress:

    46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV



    Erscheinungsdatum :

    01.01.2008


    Format / Umfang :

    12 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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