Volume 28 Issue 12
Dec.  2013
Turn off MathJax
Article Contents
ZHOU Peng-hui, TIAN Xi-hui, CHE Xue-ke, NIE Wan-sheng, HOU Zhi-yong. Experiment of airflow induced by microsecond pulse surface dielectric barrier discharge under pressure influences[J]. Journal of Aerospace Power, 2013, 28(12): 2691-2697.
Citation: ZHOU Peng-hui, TIAN Xi-hui, CHE Xue-ke, NIE Wan-sheng, HOU Zhi-yong. Experiment of airflow induced by microsecond pulse surface dielectric barrier discharge under pressure influences[J]. Journal of Aerospace Power, 2013, 28(12): 2691-2697.

Experiment of airflow induced by microsecond pulse surface dielectric barrier discharge under pressure influences

  • Received Date: 2013-04-24
  • Publish Date: 2013-12-28
  • Particle image velocimetry (PIV) technology was applied to obtain the evolution of the flow field induced by microsecond pulse plasma aerodynamic actuation, while the starting vortex, flow filed and wall jet were analyzed at different air pressures. Thrust created by the actuator was calculated and analyzed based on the experimental data. Experiment results showed that one starting vortex was found at the ground pressure and the pressure of 5500Pa, while two starting vortices were found at the pressure of 19000Pa and 11700Pa. The steady configuration of the flow field was complex, and evolved towards L, ∽ and V structure as the pressure decreased. The reaction time of the flow field and the tangential distance of the wall jet induced by plasma aerodynamic actuation decreased as the pressure decreased, while the normal distance of the wall jet increased. The maximum thrust also decreased as the pressure decreased, and its x coordinate became closer to the actuator.

     

  • loading
  • [1]
    Roth J R, Madhan R C M, Yadav M, et al.Flow field measurements of paraelectric, peristaltic, and combined plasma actuators based on the one atmosphere uniform glow discharge plasma (OAUGDPTM)[R].AIAA-2004-0845, 2004.
    [2]
    Gaitonde D V, Visbal M T, Roy S.Control of flow past a wing section with plasma-based body forces[R].AIAA-2005-5302, 2005.
    [3]
    Corke T C, Mertz B, Patel M P.Plasma flow control optimized airfoil[R].AIAA-2006-1208, 2006.
    [4]
    Roupassov D, Zavialov I, Starikovskii A, et al.Boundarylayer separation plasma control using low-temperature non-equilibrium plasma of gas discharge[R].AIAA-2006-0373, 2006.
    [5]
    Porter C O, Baughn J W, Mclaughlin T E, et al.Plasma ac-tuator force measurements[J].AIAA Journal, 2007, 45(7):1562-1570.
    [6]
    Estevadeordal J, Gogineni S.Low-speed flow control using dielectric barrier discharge (DBD).AFRL-VA-WP-TR-2006-3211, 2006.
    [7]
    梁华, 李应红, 宋慧敏, 等.等离子体气动激励诱导空气流动的PIV研究[J].实验流体力学, 2011, 25(4):22-26. LIANG Hua, LI Yinghong, SONG Huimin, et al.PIV investigation on flow induced by plasma aerodynamic actuation[J].Journal of Experiments in Fluid Mechanics, 2011, 25(4):22-26.(in Chinese)
    [8]
    赵小虎, 李应红, 李益文, 等.等离子体气动激励诱导气流加速的实验[J].航空动力学报, 2009, 24(11):2436-2442. ZHAO Xiaohu, LI Yinghong, LI Yiwen, et al.Experiment on the induced airflow acceleration by plasma aerodynamic actuation[J].Journal of Aerospace Power, 2009, 24(11):2436-2442.(in Chinese)
    [9]
    Roupassov D V, Nikipelov A A, Nudnova M M, et al.Flow separation control by plasma actuator with nanosecond pulse periodicdischarge[R].AIAA-2008-1367, 2008.
    [10]
    王万波, 黄勇, 黄宗波, 等.介质阻挡放电等离子体对NACA0015翼型流动控制的PIV实验研究[J].实验流体力学, 2012, 26(2):1-5. WANG Wanbo, HUANG Yong, HUANG Zongbo, et al.PIV measurement of dielectric barrier discharge plasma flow control on NACA0015 airfoil[J].Journal of Experiments in Fluid Mechanics, 2012, 26(2):1-5.(in Chinese)
    [11]
    梁华, 李应红, 宋慧敏, 等.多相等离子体气动激励抑制翼型失速分离的实验[J].航空动力学报, 2011, 26(4):867-873. LIANG Hua, LI Yinghong, SONG Huimin, et al.Experiment investigation on airfoil stall separation suppression by multiphase plasma aerodynamic actuation[J].Journal of Aerospace Power, 2011, 26(4):867-873.(in Chinese)
    [12]
    Abe T, Takagaki M.Momentum coupling and flow induc tion in a DBD plasma actuator[R].AIAA-2009-4068, 2009.
    [13]
    Valerioti J A, Corke T C.Pressure dependence of dielectric barrier discharge plasma flow actuators[J].AIAA Journal, 2012, 50(7):1490-1501.
    [14]
    WU Yun, LI Yinghong, JIA Min, et al.Influence of operating pressure on surface dielectric barrier discharge plasma aerodynamic actuation characteristics.[EB/OL].http://dx.doi.org/+10.1063/1.2964193.
    [15]
    CHE Xueke, SHAO Tao, NIE Wansheng, et al.Numerical simulation on a nanosecond-pulse surface dielectric barrier discharge actuator in near space.[EB/OL].http://dx.doi.org/10.1088/0022-3727/45144/145201.
    [16]
    Thomas F O, Corke T C, Iqbal M, et al.Optimization of dielectric barrier discharge plasma actuators for active aerodynamic flow control[J].AIAA Journal, 2009, 47(9):2169-2178.
  • 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 (1517) PDF downloads(982) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return