[3] Kumar,Haribalan, Roy, et al. Hydrodynamic Model of Plasma-Sheath for RF Discharges with and without Collision. AIAA 2005-948

　　[4] Junhui Huang, etal, Plasma Actuators for Separatio Flow Controlof Low Pressure Turbine Blands. AIAA2003- 1027

　　[5] Thomas C.,etal,Applicationof Weakly-ionized Plasma as WingFlow-control Deverces.AIAA2002-0350

　　[6] 李应红,吴云. 大气压等离子体流动控制实验[ J ]. 空军工程大学学报(自然科学版) 2006, 7(3) : 1- 3.

　　LI Yinghong, WU Yun.Preliminary Experimental Investigation of Atmosphere Plasma Flow Control Technoloy. Journal of Air Force Engineering University (Natural science Edition), 2006, 7(3):1-3.(in Chinese)

　　[7] 刘万刚,李一滨. 应用等离子体实现主动流动控制的实验研究[ J ]. 弹箭与制导学报, 2006, 26: 110 - 111.

　　LIU WanGang, LI YiBin. Experimental Study of Using Plasma to Induce Flow in the Quiet Air. Journal of Projectiles, Rockets, Missiles and Guidance, 2006, 26: 110-111(in Chinese)

　　[8] 毛枚良，邓小刚，向大平.辉光放电等离子体对边界层流动控制的机理研究.空气动力学报，2006年9月，第24卷3期，pg269-274

　　MAO Meiliang, DENG XiaoGang,XIANG DaPing. Numerical study for the influence of high-pressure glow discharged-induced plasma on the flow of boundary region. Acta Aerodynamica Sinica,Sep 2006, 24(3):269-274 (in Chinese)

　　[9] Miguel R, Viaval, Datta V, et al. Direct Numerical Simulation of a Forced Transitional Plane Wall Jet[R ]. A IAA 1998: 2643.

　　[10] J Reece Roth, Hojung Sin, Taja , et al. Flow Re-attachment and Acceleration by paraelectric and Peristaltic Electronhydrodynamic(EHD)Effects.AIAA 2003-531

　　[11] Thomas C, Corke, Eric Matlis. Phased Plasma Arrays for Unsteady Flow Control.AIAA2000-2323

　　[12] Corke,T CPost. Separation control on high angle of attack airfoil using plasma actuators.AIAA2003-1024

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