Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Acta Aeronautica Et Astronautica Sinica》 2015-02
Add to Favorite Get Latest Update

High altitude plasma flow control simulation through ground experiment

CHE Xueke;NIE Wansheng;HOU Zhiyong;HE Haobo;TIAN Xihui;TIAN Xuemin;Department of Space Equipment,Equipment Academy;  
The method which is used to study the plasma flow control performance at different altitudes by ground experiments is presented.The induced jet Reynolds number is measured in static air under different pressures at first,then the geometrical and electrical parameters of ground plasma model actuator will be obtained according to Reynolds similarity of the plasma induced jet.Secondly,the model actuator is applied to the wind tunnel experiments and the results can be used to estimate the plasma flow control performance at different altitudes.That plasma modifies the flowfield of S1223 airfoil is studied by this method.It is found that when the altitude increases,the maximal velocity of plasma induced jet increases but Reynolds number decreases under the same working conditions.The plasma can induce one high-speed normal jet towards wall above the actuator except the wall tangential jet under low pressure.The S1223 airfoil with Reynolds number 7.1×104 controlled by the Reynolds similarity plasma model actuator is studied.It is found that when the angle of attack is 6°-20°,the lift coefficient increases about 27% to 43% which indicates that the lift performance of near space vehicle can be improved markedly by plasma.
【Fund】: 国家自然科学基金(11205244)~~
【CateGory Index】: V216
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
【Citations】
Chinese Journal Full-text Database 5 Hits
1 LIANG Hua1,LI Ying-hong2,SONG Hui-min2,WU Yun2, JIA Min2,MA Qing-yuan2(1.The Fifth Flight College of the Air Force, The Chinese People's Liberation Army,Wuwei Gansu 733003,China; 2.Laboratory of Aero Plasma Dynamics,The Engineering Institute, Air Force Engineering University,Xi'an 710038,China);Experimental investigation on airfoil stall separation suppression by multiphase plasma aerodynamic actuation[J];Journal of Aerospace Power;2011-04
2 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);Experimental study on the separation control by plasma actuator in subsonic flow[J];Journal of Experiments in Fluid Mechanics;2007-02
3 NIE Wansheng 1, CHENG Yufeng 2 CHE Xueke 1 1 Department of Space Equipment, Academy of Equipment, Beijing 101416, China 2 Department of Postgraduate, Academy of Equipment, Beijing 101416, China;A REVIEW ON DIELECTRIC BARRIER DISCHARGE PLASMA FLOW CONTROL[J];Advances in Mechanics;2012-06
4 WANG Wan-bo1,2,ZHANG Rong-ping1,2,HUANG Zong-bo2,HUANG Yong1,2, WANG Xun-nian1,2,SHEN Zhi-hong2,ZHANG Xin2(1.State Key Laboratory of Aerodynamics,Mianyang Sichuan 621000,China; 2.China Aerodynamics Research and Development Center,Mianyang Sichuan 621000,China);Test research of two-element airfoil lift enhancement by plasma actuator[J];Acta Aerodynamica Sinica;2013-01
5 DU Hai;SHI Zhiwei;NI Fangyuan;CHENG Ruibin;DAI Xinxi;College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics;;Aerodynamic Moment Control of Flying Wing Vehicle Using Plasma Actuators[J];Acta Aeronautica et Astronautica Sinica;2013-09
【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 Zhang Panfeng Liu Aibing Wang Jinjun(School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Numerical simulation on flow induced by plasma actuator based on phenomenological model[J];Journal of Beijing University of Aeronautics and Astronautics;2010-01
2 WU Xuntao1,BAI Wenping1,JIN Kai1,XIE Likuan2(1 No.91550 Unit,Liaoning Dalian 116023,China;2 Military Representative Office of Navy in Forth Academy of CASC,Xi'an 710025,China);Analysis for Effect of Empennage Spread Synchronization on Flight Attitude[J];Journal of Projectiles,Rockets,Missiles and Guidance;2008-01
3 WANG Jian1,SANG Weimin1,DANG Mingli2,JIANG Shengju2(1 School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China; 2 No.203 Research Institute of China Ordnance Industries,Xi'an 710065,China);Investigation on Missile Aerodynamic Characteristic during Stage Separation[J];Journal of Projectiles,Rockets,Missiles and Guidance;2012-05
4 YANG Bo;SUN Min;BAI Mindi;Department of Physics, Dalian Maritime University;;Experimental Investigation of Airfoil Flow Separation Control by Dielectric Barrier Discharge Plasma Actuator[J];High Voltage Engineering;2014-01
5 CHE Xueke;NIE Wansheng;TIAN Xihui;HOU Zhiyong;CHENG Yufeng;ZHOU Penghui;Department of Space Equipment,the Academy of Equipment;Company of Postgraduate Management,the Academy of Equipment;;Momentum Transfer Efficiency of Positive and Negative Ions in SDBD Plasma[J];High Voltage Engineering;2014-04
6 WU Yun;LI Yinghong;Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University;School of Electrical Engineering, Xi'an Jiaotong University;;Progress in Research of Plasma-assisted Flow Control, Ignition and Combustion[J];High Voltage Engineering;2014-07
7 ZHAO Guangyin;LI Yinghong;FANG Haobai;HUA Weizhuo;HAN Menghu;WU Yun;Science and Technology on Plasma Dynamics Laboratory, Aeronautical and Astronautical Engineering College,Air Force Engineering University;;Characteristic of Discharge and Infrared Radiation Temperature of Saw-toothed Plasma Actuators Under Nanosecond-pulse Voltage[J];High Voltage Engineering;2014-07
8 LIU Rubing;SUN Wei;HUANG Yinyang;WANG Mengmeng;NIU Zhongguo;LIN Qi;Fujian Key Laboratory of Plasma and Magnetic Resonance, School of Physics and Mechanical & Electrical Engineering,Xiamen University;Xiamen Airlines;Aerodynamics Research Institute,AVIC;;Experimental Study on Accelerating the Gas Flow Induced by Planar Coil Electromagnetic Coupling Surface DBD Gas Discharge[J];High Voltage Engineering;2014-07
9 HAO Lingyan;LI Qingquan;BI Xiaotian;LIU Bin;Key laboratory of UHV Transmission Technology and the Gas Discharge, School of Electrical Engineering, Shandong University;Laiwu Power Supply Company, Shandong Electrical Power Corporation;;Simulation Calculation of Characteristic Parameters of Surface Dielectric Barrier Discharge[J];High Voltage Engineering;2014-10
10 ZHOU Siyin;CHE Xueke;NIE Wansheng;Department of Space Equipment, Equipment Academy;;Influence of Nanosecond Pulse Dielectric Barrier Discharge Plasma on the Cavity Performance in Scramjet Combustor[J];High Voltage Engineering;2014-10
China Proceedings of conference Full-text Database 2 Hits
1 NIE Wansheng,HOU Zhiyong,LIU Jingwei,HE Haobo (Department of Space Equipment,the Academy of Equipment Command & Technology,Beijing,101416);Experimental investigation on the fan stability of the low turbulence wind tunnel to the fluid field performance[A];[C];2010
2 Liu Weigang;Peng Lihai;Cao Ying;61255 Unit,PLA;;Helicopter Rotor with Electrical Cloud——Application of Plasma on Helicopter Blade Flow Control[A];[C];2014
【Secondary Citations】
Chinese Journal Full-text Database 10 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
2 LIANG Hua,LI Ying-hong,WU Yun,WU Wei,MA Qing-yuan(Department 1,Engineering College,Air Force Engineering University,Xi’an 710038,China);Numerical Simulation of Plasma Aerodynamic Actuation[J];High Voltage Engineering;2009-05
3 TANG Jie,DUAN Yi-xiang,ZHAO Wei,LUO Wen-feng(State Key Laboratory of Transient Optics and Photonics,Xi'an Institute of Optics and Precision Mechanics,Chinese Academy of Sciences,Xi'an 710119,China);Study of Dielectric Barrier Discharge Nonequilibrium Plasma-assisted Combustion for More Efficient Engine[J];High Voltage Engineering;2010-03
4 LI Gang,XU Yan-ji,NIE Chao-qun,ZHU Jun-qiang(Key Laboratory of Advanced Energy and Power,Institute of Engineering Thermophysics, Chinese Academy of Sciences,Beijing 100190,China);Mechanism Analysis of Combustion Control by the Plasma Swirler[J];High Voltage Engineering;2011-06
5 CHENG Yu-feng,NIE Wan-sheng,CHE Xue-ke(Department of Space Equipment,Academy of Equipment Command & Technology,Beijing 101416,China);Numerical Analysis of Dielectric Barrier Discharge Plasma Aerodynamic Actuation in Near Space[J];High Voltage Engineering;2011-06
6 WU Yun1,LI Ying-hong1,ZHU Jun-qiang2,SU Chang-bing1,LIANG Hua1,SONG Huimin1,LI Gang2(1.The Engineering Institute,Air Force Engineering University,Xi'an 710038,China;2.Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100080,China);Experimental investigation of using plasma aerodynamic actuation to extend low-speed axial compressor's stability[J];Journal of Aerospace Power;2007-12
7 WU Yun1,LI Ying-hong1,ZHU Jun-qiang2,ZHOU Min1,JIA Min1,SU Chang-bing1,SONG Hui-min1(1.The Engineering Institute,Air Force Engineering University,Xi'an 710038,China;2.Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China);Computational and experimental investigation of plasma aerodynamic actuation based corner flow separation control in a compressor cascade[J];Journal of Aerospace Power;2009-04
8 WANG Jiang-nan1,2,ZHONG Cheng-wen1,2,GAO Chao1,2,LIU Feng1,3 (1.School of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China;2.National Key Laboratory of Aerodynamic Design and Research,Northwestern Polytechnical University,Xi′an 710072,China; 3.Department of Mechanical and Aerospace Engineering,University of California,Irvine Irvine,CA 92697-3975,USA);Numerical Simulation of Flow Separation Control Using Plasma-based Actuators[J];Aeronautical Computing Technique;2007-02
9 Li Yinghong,Liang Hua,Ma Qingyuan,Wu Yun,Song Huimin,Wu Wei (PLA Key Laboratory of Aircraft Propulsion Systems,Air Force Engineering University,Xi'an 710038,China);Experimental Investigation on Airfoil Suction Side Flow Separation by Pulse Plasma Aerodynamic Actuation[J];Acta Aeronautica Et Astronautica Sinica;2008-06
10 LI Gang1, NIE Chaoqun1, ZHU Junqiang1, LI Hangming2,3, ZHANG Yi2 1. Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100080, China 2. Institute of Physics, Chinese Academy of Sciences, Beijing 100080, China 3. School of Sciences, China University of Mining and Technology,Beijing 100083, China;Development of Flow Control by Dielectric Barrier Discharge Plasma[J];Science & Technology Review;2008-04
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved