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斜孔式等离子体合成射流激励器静特性的实验

程林 孙姝 谭慧俊 何小明 张宇超 张悦

程林, 孙姝, 谭慧俊, 何小明, 张宇超, 张悦. 斜孔式等离子体合成射流激励器静特性的实验[J]. 航空动力学报, 2017, 32(11): 2784-2790. doi: 10.13224/j.cnki.jasp.2017.11.028
引用本文: 程林, 孙姝, 谭慧俊, 何小明, 张宇超, 张悦. 斜孔式等离子体合成射流激励器静特性的实验[J]. 航空动力学报, 2017, 32(11): 2784-2790. doi: 10.13224/j.cnki.jasp.2017.11.028
Experiment on static characteristics of plasma synthetic jet actuator with oblique orifice[J]. Journal of Aerospace Power, 2017, 32(11): 2784-2790. doi: 10.13224/j.cnki.jasp.2017.11.028
Citation: Experiment on static characteristics of plasma synthetic jet actuator with oblique orifice[J]. Journal of Aerospace Power, 2017, 32(11): 2784-2790. doi: 10.13224/j.cnki.jasp.2017.11.028

斜孔式等离子体合成射流激励器静特性的实验

doi: 10.13224/j.cnki.jasp.2017.11.028
基金项目: 国家自然科学基金重点项目(11532007); 江苏高校优势学科建设工程资助项目

Experiment on static characteristics of plasma synthetic jet actuator with oblique orifice

  • 摘要: 设计了斜孔式等离子体合成射流激励器,采用电参数测量和高速纹影技术研究了其放电特性及瞬态流场特性。实验表明:相较直孔式等离子体合成射流激励器,斜孔式等离子体合成射流激励器的射流流动表现出明显的附壁效应和非对称性,这有利于提高射流对流动分离的控制能力。同时,实验中还观察到了浮力对等离子体高温射流流场演化的影响,特别是在射流演化的末期,其诱导的垂向速度分量显著地改变了射流的最终运动方向。

     

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出版历程
  • 收稿日期:  2016-04-22
  • 刊出日期:  2017-11-28

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