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纳秒脉冲等离子体气动激励控制平板附面层的研究
引用本文:岳太鹏,李应红,孙冬,崔巍.纳秒脉冲等离子体气动激励控制平板附面层的研究[J].热能动力工程,2011,26(5):528-532.
作者姓名:岳太鹏  李应红  孙冬  崔巍
作者单位:空军工程大学工程学院,陕西西安,710038
基金项目:国家自然科学基金资助项目(50906100)
摘    要:为研究纳秒脉冲等离子体气动激励控制平板附面层的作用机理以及不同参数下的变化规律,利用自行研制的速度测量系统对纳秒脉冲等离子体气动激励诱导的气流速度进行了测量,结果表明:不同的激励组合方式下,等离子体气动激励效果不同,介质阻挡放电产生的效果最好;纳秒脉冲等离子体激励诱导气流加速的效果随激励电压的增大而增强,其作用于低速气...

关 键 词:等离子体气动激励  附面层  诱导  激励组合  介质阻挡放电

Study of the Boundary Layer on a Plate Aerodynamically Excited and Controlled by Using Nanosecond Pulse Plasma
YUE Tai-peng,LI Ying-hong,SUN Dong,CUI Wei.Study of the Boundary Layer on a Plate Aerodynamically Excited and Controlled by Using Nanosecond Pulse Plasma[J].Journal of Engineering for Thermal Energy and Power,2011,26(5):528-532.
Authors:YUE Tai-peng  LI Ying-hong  SUN Dong  CUI Wei
Affiliation:YUE Tai-peng,LI Ying-hong,SUN Dong,CUI Wei(Engineering College,Air Force Engineering University,Xi'an,China,Post Code:710038)
Abstract:To study the working mechanism of the boundary layer on a plate aerodynamically excited and controlled by using nanosecond pulse plasma and the law governing its change under different parameters,the speed of air flow aerodynamically excited and controlled by using the nanosecond pulse plasma was measured by utilizing a self-developed velocity measurement system.The measurement results show that under different combined excitation modes,the aerodynamic excitation effectiveness by using the plasma is varied ...
Keywords:aerodynamic excitation by using plasma  boundary layer  induction  excitation combination  medium barrier discharge  
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