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Plasma flow is a hot topic of aerodynamics in recent years. Papers on plasma flow are also fast rising in China. The characteristics of plasma aerodynamic actuation generated by dielectric barrier discharge, arc discharge and sliding discharge were studied widely. Separation on airfoil, compressor cascade, bluff body and slender conical forebody using plasma aerodynamic actuation was investigated mostly. Shock wave and compressor stability extension using plasma aerodynamic actuation were also performed. In order to improve the separation authority, a new principle of plasma-shock-based flow control was put forward.
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Li et al. (2012) studied this question.
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