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Aerodynamic control of NACA 0021 airfoil model with spark discharge plasma synthetic jets[J]. LIU RuBing,NIU ZhongGuo,WANG MengMeng,HAO Ming,LIN Qi.Science China(Technological Sciences). 2015(11)
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Effect of pressure on the performance of plasma synthetic jet actuator[J]. WANG Lin,XIA ZhiXun,LUO ZhenBing,ZHANG Yu.Science China(Physics,Mechanics & Astronomy). 2014(12)
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Shock wave-boundary layer interactions control by plasma aerodynamic actuation[J]. SUN Quan,LI YingHong,CUI Wei,CHENG BangQin,LI Jun,DAI Hui.Science China(Technological Sciences). 2014(07)
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Computational and experimental analysis of Mach 2 air flow over a blunt body with plasma aerodynamic actuation[J]. SUN Quan,CHENG BangQin,LI YingHong,KONG WeiSong,LI Jun,ZHU YiFei,JIN Di.Science China(Technological Sciences). 2013(04)
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Actuators for Active Flow Control[J] . Louis N. Cattafesta,Mark Sheplak.Annual Review of Fluid Mechanics . 2011
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Plasma mitigation of shock wave: experiments and theory[J] . Spencer P. Kuo.Shock Waves . 2007 (4)
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SHOCK WAVE DRAG REDUCTION*[J] . Dennis M. Bushnell.Annual Review of Fluid Mechanics . 2004
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Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control .2 Narayanaswamy,Venkateswaran,Raja,Laxminarayan L,Clemens,Noel T. AIAA Journal . 2010