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《Nuclear Fusion and Plasma Physics》 2009-01
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Simulation investigation on boundary layer of a plate flow control by plasma aerodynamic actuation

LIANG Hua,LI Ying-hong,WU Yun,MA Qing-yuan,WU Wei(Engineering College,Air Force Engineering University,Xi’an 710038)  
Simulation investigation on boundary layer flow controlled by plasma aerodynamic actuation is performed,in which the influences of the plasma actuation on the boundary layer are regarded as added momentum and thermal energy.The body force of the plasma actuation is obtained by solving a two-dimensional fluid model of the surface discharge;from the body force the momentum and thermal energy acting on the boundary layer are induced,and then introduced into the Navier-Stokes equation as the source term.The influence of the intensity of the plasma aerodynamic actuation,the electrode number and position,as well as the thermal energy is investigated,the results agree with experiments.
【Fund】: 国家863计划(2005AA753031);; 教育部优秀人才支持计划;; 空军工程大学工程学院优秀博士学位论文创新基金(BC07001)
【CateGory Index】: O539
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【Citations】
Chinese Journal Full-text Database 3 Hits
1 SONG Huimin,LI Yinghong,WEI Fengting,ZHANG Pu(Engineering Institute,Air Force Engineering University,Xi'an 710038,China);Modeling and Simulation of Plasma Electrohydrodynamic Actuator[J];High Voltage Engineering;2006-03
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【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 FU Xin,ZHANG Wen-xuan,LI Bao-ming(National Key Laboratory of Transient Physics,NUST,Nanjing 210094,China);Experimental Study of Boundary Layer Velocity Profile Induced by Low-temperature Plasma[J];Journal of Ballistics;2008-01
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8 LIANG Hua1,LI Ying-hong2,JIA Min2,BAI Jun-xin1,ZHANG Sheng-zhi 1,BAI Jun-xing1(1.The Fifth Flight College of the Air Force,Wuwei 733003,China;2.PLA Key Laboratory of Aero Plasma Dynamics,Air Force Engineering University,Xi'an 710038,China);Energy Conversion Process Analysis of Plasma Aerodynamic Actuation[J];High Voltage Engineering;2010-12
9 LI Yi-wen1,LI Ying-hong1,WU Yun1,LIANG Hua1,SU Chang-bing1,LIU Li-bin2(1.Engineering College,Air Force Engineering University,Xi’an 710038; 2.Military Representative Department of Xi’an Airplane Company,Yanliang 710032);Impact to discharge characteristic and acceleration effect of plasma aerodynamic actuators configurations[J];Nuclear Fusion and Plasma Physics;2008-02
10 LIANG Hua,LI Ying-hong,CHENG Bang-qin,MA Qing-yuan,WU Wei(The Engineering Institute,Air Force Engineering University,Xi′an 710038,China);Numerical simulation on airfoil stall separation suppression by plasma aerodynamic actuation[J];Journal of Aerospace Power;2008-05
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1 WU Yun, LI Ying-hong, ZHANG Pu, SU Chang-bing, LIANG Hua (PLA Key Laboratory of Aircraft Propulsion System, Air Force Engineering University, Xi'an 710038, China);Experimental Investigation on Atmosphere Plasma Actuation Based Flow Separation Suppression[A];[C];2006
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