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    Titel :

    Numerical Investigations of Flow Separation on the AVT-183 53 Degree Swept Diamond Wing Configuration (AIAA 2015-0066)


    Beteiligte:

    Kongress:

    Aerospace sciences meeting



    Erscheinungsdatum :

    2015-01-01


    Format / Umfang :

    25 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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    Control of Separation on a Swept Wing using Fluidic Oscillators (AIAA 2015-0783)

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