期刊文献+

等离子体诱导圆锥前体流场的PIV测量 被引量:1

PIV study of induced flowfield on steady and periodic-pulsed dielectric-barrier-discharges
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摘要 在封闭光学玻璃箱体内,应用介质阻挡放电等离子体对20°顶角圆锥附近的静止大气进行了定常和脉冲循环控制,对等离子体诱导的圆锥截面绕流速度场进行了二维PIV测量,在定常控制和脉冲循环控制下,比较分析了最大绕流速度及最大轴向涡量,研究了脉冲频率和电压对上述参数的影响。实验结果表明:存在一个交流电压阈值(Vp-p≈14.0 kV),当电压高于这个阈值后,相对于定常控制模式,脉冲循环控制下沿90°方位角径向线上分布的时间平均切向速度和轴向涡量迅速增加;在脉冲循环控制控制下,动量传递主要表现为分离涡的形成而不是气流的加速。 A two-dimensional particle image velocimetry is used to measure cross flow velocity field around a 20° conical cone in atmospheric air in a closed tank which is made of optical glass.The time-averaged spatial and temporal distributions of induced maximum cross flow velocity and maximum magnitude of axial-vorticity in the neighborhood of the body are investigated.The test results show that there exists a threshold of the ac voltage(Vp?p≈14.0 kV),over the threshold voltage,the ensemble-averaged tangential velocity and axial vorticity along a radial line perpendicular to the body symmetry plane induced by steady actuation are increased sharply;The main mechanism of momentum transfer under periodic-pulsed actuation is the formation of discrete vortices,rather than the gas acceleration.
出处 《应用力学学报》 CAS CSCD 北大核心 2011年第3期308-312,329-330,共5页 Chinese Journal of Applied Mechanics
基金 西北工业大学基础研究基金(JC200901) 高等学校博士学科点专项科研基金(2010610211000220096102120001) 中国博士后科学基金(20100471000) 国防预研重点实验室基金(9140C42010209019140C42020210ZS51)
关键词 粒子图像测速 圆锥体 等离子体主动流动控制 脉冲循环 流场测量 Particle Image Velocimetry conical cone plasma active flow control periodic-pulsed flow field measurements.
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参考文献7

  • 1Ericsson L. Sources of high alpha vortex asymmetry at zero sideslip[J]. JournalofAircraft, 1992, 29(6): 1086-1090.
  • 2Lowson M, Ponton A. Symmetry breaking in vortex flows on conicalbodies[J]. AIAA J, 1992, 30.. 1576-1583.
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二级参考文献13

  • 1顾蕴松,明晓.大迎角细长体侧向力的比例控制[J].航空学报,2006,27(5):746-750. 被引量:17
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  • 4Zilliae G G, Degani D, Tobak M. Asymmetric vortices on a slender body of revolution[J]. AIAA Journal, 1991, 29 (5): 667-675.
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  • 8Post M, Corke T C. Separation control on high angle of attack airfoil using plasma actuators[J]. AIAA Journal, 2004, 42(11): 2177-2184.
  • 9Liu F, Luo S J, Gao C, et al. Flow control over a conical forebody using duty-cycled plasma actuators[J]. AIAA Journal, 2008, 46(11): 2969-2973.
  • 10Liu F, Luo S J, Gao C, et al. Mechanisms for conical forebody flow control using plasma actuators[R]. AIAA- 2009-4284, 2009.

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