Advanced Search+
LI Feng(李峰), GAO Chao(高超), ZHENG Borui(郑博睿), WANG Yushuai(王玉帅). Research on the Peristaltic Flow Acceleration Performance of Asynchronous and Duty Cycle Pulsed DBD Plasma Actuation[J]. Plasma Science and Technology, 2014, 16(9): 861-866. DOI: 10.1088/1009-0630/16/9/10
Citation: LI Feng(李峰), GAO Chao(高超), ZHENG Borui(郑博睿), WANG Yushuai(王玉帅). Research on the Peristaltic Flow Acceleration Performance of Asynchronous and Duty Cycle Pulsed DBD Plasma Actuation[J]. Plasma Science and Technology, 2014, 16(9): 861-866. DOI: 10.1088/1009-0630/16/9/10

Research on the Peristaltic Flow Acceleration Performance of Asynchronous and Duty Cycle Pulsed DBD Plasma Actuation

Funds: supported by National Natural Science Foundation of China (No. 51107101) and the Foundation for Fundamental Research of the Northwestern Polytechnical University of China (JC201103)
More Information
  • Received Date: January 17, 2013
  • Using a plexiglas plate model, the performance of peristaltic flow acceleration in- duced by multiple DBD (dielectric barrier discharge) plasma actuators was studied based on PIV (particle image velocimetry). The asynchronous and the duty cycle pulsed actuation modes were proposed and tested. The velocity fields induced by multiple DBD plasma actuators with different phase angles and duty cycle ratios were acquired and the momentum transfer characteristics of the flow field were discussed. Consequently, the mechanism of the peristalsis-acceleration multi- ple DBD plasma actuation was analyzed. The results show that the peristaltic flow acceleration effect of multiple plasma actuators occurs mainly in paraelectric direction, and the mechanism of peristaltic flow acceleration is ejection pushing effect rather than injection pumping effect. The asynchronous and the duty cycle pulsed actuation modes can, with energy consumption increase of merely 10%, achieve 65% and 42% increase of downstream velocity, and thus are promising in velocity improvement and energy saving.
  • 1 Roth J R, Sherman D M, Wilkinson S P. 1998, Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma. 36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA.
    2 Wilkinson S. 1990, Interactive wall turbulence control viscous drag reduction in boundary layers. AIAA Progress in Astronautics and Aeronautics, Washington, DC
    3 Roth J R. 1997, Method and apparatus for covering bodies with an uniform glow discharge plasma and applications thereof. University of Tennessee Research Corporation. 5669583, Knoxville, USA
    4 Sherman D M, Wilkinson S P, Roth J R. 2000, Paraelectric gas flow accelerator. University of Tennessee Research Corporation. 6200539, Knoxville, USA
    5 Enloe C L, McLaughlin T E, VanDyken R D, et al.2004, AIAA Journal, 42: 589
    6 Enloe C L, McLaughlin T E, Font G I, et al. 2006,AIAA Journal, 44: 1127
    7 Enloe C L, Font G I, McLaughlin T E, et al. 2006,AIAA Journal, 46: 2730
    8 Patel M P, Ng T T, Vasudevan S, et al. 2007, Scaling effects of an aerodynamic plasma actuator. 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA
    9 Zheng Borui, Gao Chao, Li Yibin, et al. 2011, Momentum transfer in millisecond periodic-pulsed dielectric barrier-discharge plasma actuator. AIAA Aeronautics and Astronautics Conference, Reno, USA
    10 Orlov D M, Corke T C. 2005, Numerical simulation of aerodynamic plasma actuator effects. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA
    11 Roth J R, Madhan R C. 2004, Flow field measurements of paraelectric, peristaltic, and combined plasma actuators based on the one atmosphere uniform glow discharge Plasma (OAUGDPTM). 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA
    12 Roth J R, Dai X. 2005, The physics and phenomenology of paraelectric one atmosphere uniform Glow discharge plasma (OAUGDPTM) actuators for aerodynamic flow control. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA
    13 Roth J R. 2003, Physics of Plasmas, 10: 5
    14 Roth J R. 2001, Industrial Plasma Engineering, 18: 6
    15 Whalley R, Choi K S. 2010, Turbulent boundary layer control by DBD plasma: a Spanwise travelling wave.5th AIAA Flow Control Conference, Chicago, USA
    16 Boeuf J P, Pitchford L C. 2005, Journal of Applied Physics, 97: 1033
    17 Mario J. Pinheiro, Alexandre M M. 2010, Journal of Applied Physics, 108: 0333
    18 Zheng Borui, Gao Chao, Li Yibin, et al. 2013, Design and application of multihannel peristaltic acceleration pulsed plasma actuation power supply. 2013 Chinese Aerodynamics Research Society, Jilin, China
    19 Zheng Borui, Gao Chao, Li Yibin, et al. 2012, Plasma Science and Technology, 14: 58
    20 Zheng Borui, Gao Chao, Li Yibin, et al. 2013, Plasma Science and Technology, 15: 350
    21 Wang Yushuai, Zheng Borui, Chao Gao, et al. 2013,Experimental study of DBD plasma actuation body force based on PIV. 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Dallas, USA

Catalog

    Article views (183) PDF downloads (1112) Cited by()

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return