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    Titel :

    The Effects of a Leading Edge Rotating Cylinder on the Performance of a NACA 0015 Airfoil at High Angles of Attack (AIAA 2014-0540)



    Kongress:

    Conference, AIAA atmospheric flight mechanics ; 2014 ; National Harbor, MD



    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    14 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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