This paper presents an experimental investigation of the effect of the dielectric barrier discharge plasma actuators on the leading-edge vortex flow control over a delta wing with a 75 deg swept angle. The Reynolds number based on the delta wing chord is 50,000. The smoke flow visualization and particle image velocimetry experiments in the wind tunnel indicate that the asymmetric control caused by the dielectric barrier discharge plasma actuator can significantly affect the global flow structure over the delta wing: the leading-edge vortex breakdown position on the same side of the actuator is advanced, whereas vortex breakdown on the other side is delayed. This phenomenon is observed for the first time and is only observed in the current full-span delta wing experiment, significantly different from the result of the semispan experiment. The force measurement result shows that the asymmetric control has a limited contribution to lift generation but can induce a relatively large roll moment.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Asymmetric Flow Control on a Delta Wing with Dielectric Barrier Discharge Actuators


    Contributors:
    Shen, Lu (author) / Wen, Chih-yung (author) / Chen, Hsin-An (author)

    Published in:

    AIAA Journal ; 54 , 2 ; 652-658


    Publication date :

    2015-10-06


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Delta Wing Flow Control Using Dielectric Barrier Discharge Actuators

    Greenblatt, David / Kastantin, Yousef / Nayeri, Navid et al. | AIAA | 2007


    Delta Wing Flow Control Using Dielectric Barrier Discharge Actuators

    Greenblatt, D. / Kastantin, Y. / Nayeri, N. et al. | British Library Conference Proceedings | 2007


    Delta-Wing Flow Control Using Dielectric Barrier Discharge Actuators

    Greenblatt, David / Kastantin, Y. / Nayeri, C. N. et al. | AIAA | 2008