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    Title :

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



    Conference:

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



    Publication date :

    2014-01-01


    Size :

    14 pages


    Remarks:

    Includes bibliographical references and author index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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