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Measurement of Plasma Density Produced in Dielectric Barrier Discharge for Active Aerodynamic Control with Interferometer 被引量：1

Measurement of Plasma Density Produced in Dielectric Barrier Discharge for Active Aerodynamic Control with Interferometer
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摘要 We utilize an interferometer to investigate the changes of the refractive index caused by dielectric barrier discharge plasma. The electronic density of the plasma produced is measured and analyzed tentatively. The results show that density of the plasma increases linearly with exciting voltages. We utilize an interferometer to investigate the changes of the refractive index caused by dielectric barrier discharge plasma. The electronic density of the plasma produced is measured and analyzed tentatively. The results show that density of the plasma increases linearly with exciting voltages.
作者 李钢 张翼 徐燕骥 林彬 李玉同 朱俊强
机构地区 Institute of Engineering Thermophysics Laboratory of Optical Physics
出处 《Chinese Physics Letters》 SCIE CAS CSCD 2009年第10期136-139,共4页 中国物理快报（英文版）
基金 Supported by the National Natural Science Foundation of China under Grant No 50776086.
关键词 Fluid dynamics Plasma physics Fluid dynamics Plasma physics
分类号 O461 [理学—电子物理学] X703 [环境科学与工程—环境工程]
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参考文献10

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同被引文献36

  • 1于达仁,武志文,鄂鹏,A.I.Bugrova.稳态等离子体发动机磁场设计的发展及其展望[J].中国工程科学,2005,7(4):22-29. 被引量：4
  • 2营井秀郎.等离子体电子工程学[M].张海波,译.北京:科学出版社,2002.
  • 3Lemire S, Vo H D. Reduction of fan and compressor wake de- fect using plasma actuation for tonal noise reduction[J]. Jour- nal of Turbomachinery, 2011, 133(011017).
  • 4Marks C, Sondergaard R, Wolff M, et al. Experimental corn parison of DBD plasma actuators for low Reynolds number sep aration control[C] ff ASME Conference Proceedings. Vancou ver, Canada: American Society of Mechanical Engineers 2011 :. 581-594.
  • 5Jukes T N, Choi K S. Control of unsteady flow separation over a circular cylinder using dielectric barrier discharge surface plasma[J]. Physics of Fluids, 2009, 21(9): 094106.
  • 6Jukes T N, Choi K S. Flow control around a circular cylinder using pulsed dielectric barrier discharge surface plasma[J]. Physics of Fluids, 2009, 21(8): 084103.
  • 7Enloe C L, McLaughlin T E, VanDyken R D. Plasma struc ture in the aerodynamic plasma actuator[C]//42nd AIAA Aer- ospace Sciences Meeting and Exhibit. Reno, Nevada, USA: AIAA, 2004.
  • 8Enloe C L, McLaughlin T E, VanDyken R D, et al. Mecha- nisms and responses of a single dielectric barrier discharge plas- ma actuator: plasma morphology[J]. AIAA Journal, 2004, 42 (3): 589-594.
  • 9Enloe C L, MeLaughlin T E, VanDyken R D, et al. Mecha- nisms and responses of a single dielectric barrier discharge plas- ma actuator: geometric effects[J]. AIAA Journal, 2004, 42 (3) : 595-604.
  • 10Enloe C L, Mcharg M G, McLaughlin T E. Time-correlated force production measurements of the dielectric harrier dis- charge plasma aerodynamic actuator [J]. Journal of Applied Physics, 2008, 103(7): 1-7.

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Chinese Physics Letters
2009年 第10期

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