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    Title :

    Experimental Analysis of Burst Actuation for Separation Control around a Pitching NACA0015 Airfoil Using a DBD Plasma Actuator at low Reynolds number


    Contributors:

    Conference:

    2018 AIAA Aerospace Sciences Meeting



    Publication date :

    2018-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English