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    Titel :

    Plasma-Actuated Flow Control of Hypersonic Crossflow-Induced Boundary-Layer Transition in a Mach-6 Quiet Tunnel (AIAA 2018-1076)


    Beteiligte:

    Kongress:

    Aerospace sciences meeting ; 2018 ; Kissimmee, FL



    Erscheinungsdatum :

    2018-01-01


    Format / Umfang :

    23 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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    Measurements in the Boeing/AFOSR Mach-6 Quiet Tunnel on Hypersonic Boundary-Layer Transition (AIAA 2017-3632)

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