An experimental investigation of separation control using steady and pulsed plasma actuators was carried out on an Eppler E338 airfoil at typical micro air vehicle Reynolds numbers (20,000<=Re<=140,000). Pulsing was achieved by modulating the high frequency plasma excitation voltage. The actuators were calibrated directly using a laser doppler anemometer, with and without free-stream velocity, and this allowed the quantification of both steady and unsteady momentum introduced into the flow. At conventional low Reynolds numbers (Re>100,000) asymmetric single phase plasma actuators can have a detrimental effect on airfoil performance due to the introduction of low momentum fluid into the boundary layer. The effect of modulation, particularly at frequencies corresponding to F+ nearly equal 1, became more effective with decreasing Reynolds number resulting in significant improvements in CL,max. This was attributed to the increasing momentum coefficient, which increased as a consequence of the decreasing free-stream velocities. Particularly low duty cycles of 3% were sufficient for effective separation control, corresponding to power inputs on the order of 5 milliwatts per centimeter.


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    Titel :

    Pulsed plasma actuators for active flow control at MAV Reynolds numbers


    Weitere Titelangaben:

    Gepulste Plasmaaktoren für aktive Strömungsregelung bei Reynolds-Zahlen von Mikroluftfahrzeugen


    Beteiligte:
    Göksel, B. (Autor:in) / Greenblatt, D. (Autor:in) / Rechenberg, I. (Autor:in) / Kastantin, Y. (Autor:in) / Nayeri, C.N. (Autor:in) / Paschereit, C.O. (Autor:in)


    Erscheinungsdatum :

    2007


    Format / Umfang :

    14 Seiten, 13 Bilder, 1 Tabelle, 17 Quellen





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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