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    Title :

    Control of Separated Flow on a NACA 0015 Airfoil using Three-Dimensional Plasma Actuator (AIAA 2014-2665)


    Contributors:

    Conference:

    Conference; 7th, Flow control; 7th AIAA flow control conference 2014; Atlanta, Georgia, USA, 16-20 June 2014 : held at the AIAA aviation forum 2014 ; 2014 ; Atlanta, GA



    Publication date :

    2014-01-01


    Size :

    10 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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