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电流体动力等离子体发生器的能量转化效率分析及其优化设计 被引量:6

Energy Conversion Efficiency Analysis and Optimization Design of Electrohydrodynamic Plasma Actuator
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摘要 为对电流体动力(EHD)等离子体发生器进行性能优化,提高能量转化效率,使用石英和聚四氟乙烯作为介质板,通过实验测量了等离子体发生器的能量消耗和产生的气流速度随背面电极宽度、电极水平间距、电源电压和频率以及放电状态等的变化曲线,用气流速度与单位长度能量消耗的比值对发生器能量转化效率进行衡量。结果表明,等离子体发生器背面电极宽度为2倍正面电极宽度时气流速度最大;无间距等离子体发生器对气流加速效果并非最佳;诱导的气流速度随电压升高先上升后下降,存在气流速度的最大值;当等离子体放电在视觉上比较均匀时放电的能量转换效率最高。实验结果为EHD等离子体发生器提高能量转化效率,进行结构优化提供了参考。 In order to optimize the performance of electrohydrodynamic(EHD) plasma actuator and increase power conversion efficiency,we experimentally researched the effects of plasma actuator back plate electrode width,electrode gaps,voltage and frequency of power and discharge condition on energy consumption and air velocity in Quartz and Teflon plates,and measured the energy conversion efficiency by the ratio of air velocity to energy consumption per unit length.The results show that when the width of back plate electrode is twice of front electrode,air velocity has the maximum value,and the energy conversion efficiency is the highest.Plasma actuator without electrode gaps is not the best condition for airflow acceleration.As the voltage rises,air velocity decreases after an increase and has its maximum value.Energy conversion efficiency is the highest when plasma discharge is visually more homogenous.The results will contribute to the improvement of energy conversion efficiency and structural optimization of plasma actuators.
出处 《高电压技术》 EI CAS CSCD 北大核心 2011年第6期1426-1431,共6页 High Voltage Engineering
基金 国家自然科学基金(51077089) 山东省中青年科学家科研奖励基金(2008BS01020)~~
关键词 电流体动力(EHD) 等离子体发生器 能量转化效率 优化设计 几何参数 气流速度 electrohydrodynamic(EHD) plasma actuator energy conversion efficiency optimization design geometric structure air velocity
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  • 1Rnth J R. Industrial plasma engineering volume 1- principles [M]. Bristol and Philadelphia, U K: Institule of Physics Pub- lishing, 1995. 被引量:1
  • 2Roth J R. Industrial plasma engineering volume 2- applications to non thermal plasma processing[M]. Bristol and Philadelphia, U K: Institute of Physics Publishing, 2001. 被引量:1
  • 3Thomas F O, Kozlov A, Corke T C. Plasma actuators for land- ing gear noise reduction[C]//11th AIAA/CEAS Aeroacoustics Conference, California, USA: AIAA, 2005: 3010-3015. 被引量:1
  • 4Huang Junhui, Corke TC, Thomas F O. Plasma actuators for separation control of low pressure turbine blades[J]. AIAA Journal, 2006, 44(1): 1477- 1487. 被引量:1
  • 5Roth J R, Sherman D M, Wikinson S P. Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma[C] //AIAA Aerospace Sciences Meeting Exhibit. Man- hattan Beach, CA, USA: AIAA, 1998:328- 333. 被引量:1
  • 6Enloe C L, McLaughlin T E, VanDyken R D, et al. Mecha- nisms and responses of a single dielectric barrier plasma actua- tor: geometric effects [ C] //AIAA Aerospace Sciences Meet- ing. Big Sky, MT, USA: AIAA, 2004: 595-605. 被引量:1
  • 7Pons J, Moreau E, Touchard G. Asymmetric surface dielectric barrier discharge in air at atmospheric pressure: electrical prop- erties and induced airflow characteristics[J] . Applied Physics, 2005, 38 (19): 3635- 3642. 被引量:1
  • 8Forte M, Jolibois J, Moreau E, et al. Optimization of a dielec- tric barrier discharge actuator by stationary and in-stationary measurements of the induced flow velocity , application to air flow control [C] //AIAA Aerospace Sciences Meeting. Monter- ey, CA, USA: AIAA, 2006: 2863-2867. 被引量:1
  • 9杨芸,张冠军,杨国清,张源斌,张文元.空气条件下介质阻挡放电影响因素的研究[J].高电压技术,2007,33(2):37-41. 被引量:18
  • 10Porter C O, Baughn J W, McLaughlin T E, et al. Temporal force measurement s on an aerodynamic plasma actuator[C] // AIAA Aerospace Sciences Meeting. Monterey, CA, USA: AIAA, 2006, 9 -12. 被引量:1

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