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《Journal of Experiments in Fluid Mechanics》 2007-02
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Experimental study on the separation control by plasma actuator in subsonic flow

ZHANG Pan-feng1,WANG Jin-jun1,SHI Wei-yi1,WU Zhe2(1.Institute of Fluid Mechanics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China;2.Department of Flight Design,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)  
The smoke flow visualization was carried out in wind tunnel to investigate the flow separation control around the inclined flat plate by plasma actuator in subsonic flow.The plasma actuator mounted at the leading edge of the flat plate can prevent the flow separation and make the flow fully attach to the upside surface at the angles of attack near the stall point,and can decrease the width of the recirculation flow region at large angles of attack.The experiments with five different arranged electrodes indicated that it is more efficient to control the flow separation with larger negative electrode width and spacing between the adjacent edges of the electrodes,if the voltage and frequency of the input power source are constants.Finally,the suction and acceleration effects of the plasma actuator on the surrounding air were confirmed by flow visualization,and the mechanism of flow separation control by plasma actuator was discussed.
【Fund】: “十一五”国防预研资助项目;; 中国博士后科学基金资助项目(2005037035);; 航空科学基金资助项目(2006ZA51013)
【CateGory Index】: O539
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