Volume 34 Issue 8
Aug.  2019
Turn off MathJax
Article Contents
Effect of discharge resistor on performance of plasma synthetic jet actuator[J]. Journal of Aerospace Power, 2019, 34(8): 1724-1730. doi: 10.13224/j.cnki.jasp.2019.08.011
Citation: Effect of discharge resistor on performance of plasma synthetic jet actuator[J]. Journal of Aerospace Power, 2019, 34(8): 1724-1730. doi: 10.13224/j.cnki.jasp.2019.08.011

Effect of discharge resistor on performance of plasma synthetic jet actuator

doi: 10.13224/j.cnki.jasp.2019.08.011
  • Received Date: 2019-01-14
  • Publish Date: 2019-08-28
  • A plasma synthetic jet actuator (PSJA) with normal orifice was designed to study the effect of discharge resistor. The discharge characteristics and transient flow-field characteristics of actuator with 100,200,300 Ω were researched by electric parameter measurement system and high-speed schlieren technology. Results showed that the discharge process can be divided into two stages due to the existence of current limiting resistance, rapid discharge stage and slow discharge stage.This mode can continuously provide energy to the actuator while satisfying the higher initial energy injection, and effectively improve the stability of the actuator.At the same time, the smaller discharge resistance can obtain greater jet velocity, enhancing the jet flow control capability.The smaller discharge resistance led to the increase of discharge current, unstable velocity and worsening of working stability.In practical application, it was necessary to consider and determine the final resistance value comprehensively to ensure the rational distribution of energy in the two discharge stages.

     

  • loading
  • [1]
    KRAL L D.Active flow control technology[R].[S.l.]:ASME Fluids Engineering Division,2000.
    [2]
    GADELHAK M.Flowcontrol:the future[J].Journal of Aircraft,2001,38(3):402-418.
    [3]
    吴云,李应红.等离子体流动控制与点火助燃研究进展[J].高电压技术,2014,40(7):2024-2038.WU Yun,LI Yinghong.Progress in research of plasma-assisted flow control,ignition and combustion[J].High Voltage Engineering,2014,40(7):2024-2038.(in Chinese)
    [4]
    GROSSMAN K R,CYBYK B Z,VANWIE D M.Sparkjet actuators for flow control[R].AIAA-2003-0057,2003.
    [5]
    李应红.航空等离子体动力学与技术的发展[J].航空工程进展,2011,2(2):127-132.LI Yinghong.Development of aero-plasma dynamics and technology[J].Advances in Aeronauticai Science and Engineering,2011,2(2):127-132.(in Chinese)
    [6]
    CYBYK B Z,GROSSMAN K R,WILKERSON J T,et al.Single-pulse performance of the sparkjet flow control actuator[R].AIAA-2005-0401,2005.
    [7]
    CYBYK B Z,WILKERSON J T,GROSSMAN K R.Performance characteristics of the sparkjet flow control actuator[R].AIAA-2004-2131,2004.
    [8]
    CYBYK B Z,SIMON D H,LAND H,et al.Experimental characterization of a supersonic flow control actuator[R].AIAA-2006-0478,2006.
    [9]
    BELINGER A,HARDY P,BARRICAU P,et al.Influence of the energy dissipation rate in the discharge of a plasma synthetic jet actuator[J].Journal of Physics:D Applied Physics,2011,44(36):365201.1-365201.12.
    [10]
    NARAYANASWAMY V,RAJA L L,CLEMENS N T.Control of a shock/boundary-layer interaction by using a pulsed-plasma jet actuator[J].AIAA Journal,2012,50(1):246-249.
    [11]
    NARAYANASWAMY V,RAJA L L,CLEMENS N T.Control of unsteadiness of a shock wave/turbulent boundary layer inter-action by using a pulsed-plasma-jet actuator[J].Physics of Fluids,2012,24(7):076101.1-076101.23.
    [12]
    WU Y,LI Y H,LIANG H,et al.Nanosecond pulsed discharge plasma actuation:characteristics and flow control performance[R].Atlanta:the 45th AIAA Plasmadynamics and Lasers Conference,2014.
    [13]
    梁华,李应红,吴云,等.等离子体气动激励的数值仿真[J].高电压技术,2009,35(9):1071-1076.LIANG Hua,LI Yinghong,WU Yun,et al.Numerical simulation of plasma aerodynamic actuation[J].High Voltage Engineering,2009,35(9):1071-1076.(in Chinese)
    [14]
    孙权,崔巍,程邦勤,等.等离子体气动激励控制超声速边界层分离的实验研究[J].航空学报,2015,36(2):501-509.SUN Quan,CUI Wei,CHENG Bangqin,et al.Experimental investigation on supersonic boundary layer separation by plasma aerodynamic actuation[J].Acta Aeronautica et Astronautica Sinica,2015,36(2):501-509.(in Chinese)
    [15]
    宋慧敏,李应红,魏沣亭,等.等离子体电流体动力激励器的建模与仿真[J].高电压技术,2006,32(3):72-74.SONG Huimin,LI Yinghong,WEI Fengting,et al.Modeling and simulation of plasma electrohydrodynamic actuator[J].High Voltage Engineering,2006,32(3):72-74.(in Chinese)
    [16]
    JIN D,CUI W,LI Y,et al.Characteristics of pulsed plasma synthetic jet and its control effect on supersonic flow[J].Chinese Journal of Aeronautics,2015,28(1):66-76.
    [17]
    ZONG H,CUI W,WU Y,et al.Influence of capacitor energy on performance of a three-electrode plasma synthetic jet actuator[J].Sensors and Actuators:A Physical,2015,222:114-121.
    [18]
    宗豪华,宋慧敏,梁华,等.纳秒脉冲等离子体合成射流特性实验研究[J].推进技术,2015,36(10):1474-1478.ZONG Haohua,SONG Huimin,LIANG Hua,et al.Experimental study on characteristic of nanosecond pulsed plasma synthetic jet[J].Journal of Propulsion Technology,2015,36(10):1474-1478.(in Chinese)
    [19]
    王林,罗振兵,夏智勋,等.等离子体合成射流能量效率及工作特性研究[J].物理学报,2013,62(12):125207.1-125207.10.WANG Lin,LUO Zhenbing,XIA Zhixun,et al.Energy efficiency and performance characteristics of plasma synthetic jet[J].Acta Physica Sinica,2013,62(12):125207.1-125207.10.(in Chinese)
    [20]
    HUANG H X,TAN H J,SUN S,et al.Letter:transient interaction between plasma jet and supersonic compression ramp flow[J].Physics of Fluids,2018,30(4):041703.1-041703.4.
    [21]
    程林,孙姝,谭慧俊,等.斜孔式等离子体合成射流激励器静特性的实验[J].航空动力学报,2017(11):231-237.CHENG Lin,SUN Shu,TAN Huijun,et al.Experiment on static characteristics of plasma synthetic jet actuator with oblique orifice[J].Journal of Aerospace Power,2017,32(11):2784-2790.(in Chinese)
    [22]
    张宇超,谭慧俊,程林,等.低气压条件下多缝式等离子体合成射流激励器特性实验[J].航空动力学报,2018,33(3):711-716.ZHANG Yuchao,TAN Huijun,CHENG Lin,et al.Experiment on characteristics of plasma synthetic jet actuator with multiple slots under low pressure condition[J].Journal of Aerospace Power,2018,33(3):711-716.(in Chinese)
    [23]
    ZHANG Y,TAN H,HUANG H,et al.Transient flow patterns of multiple plasma synthetic jets under different ambient pressures[J].Flow Turbulence and Combustion,2018,101(3):741-757.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (654) PDF downloads(367) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return