[2] WU Yun,SONG Hui-min,LI Ying-hong,et al.Experimental Investigation of Plasma Assisted Flow Control on NACA 0015 Airfoil [C]//Xi’an:XVI International Conference on Gas Discharges and their Applications,2006:833-836.
[3] ROTH J R,SHEMAN D M,WILKINSON S P.Boundary Layer Flow Control with a One Atmosphere Uniform Glow Discharge Surface Plasma [R].Reno:American Institute of Aeronautics and Astronautics,1998.
[4] ROTH J R,SIN H,MADHAN R C M,et al. Flow Reattachment and Acceleration by Paraelectric and Peristaltic Electrohydrodynamic(EHD) Effects [R].Reno:American Institute of Aeronautics and Astronautics,2003.
[5] ENLOE C L,MCLAUGHLIN T E,VANDYKEN R D,et al.Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator:Plasma Morphology [J].AIAA Journal,2004,42(3):589-594.
[6] POST M L,CORKE T C.Flow Control with Single Dielectric Barrier Plasma Actuators [R].Toronto:American Institute of Aeronautics and Astronautics,2005. [7] ROUPASSOV D V,ZAVYALOV I N,STARIKOVSKII A Y.Boundary Layer Separation Control by Nanosecond Plasma Actuators [R].Miami:American Institute of Aeronautics and Astronautics,2007.
[8] BOUEF J P,LAGMICH Y,CALLIGARI T,et al.Electrohydrodynamic Force and Flow Acceleration in Surface Discharges [R].San Francisco:American Institute of Aeronautics and Astronautics,2006.