论文部分内容阅读
Investigation on corner separation control in a compressor cascade using plasma aerodynamic actuatio
【机 构】
:
Science and Technology on Plasma Dynamics Lab, Air Force Engineering University of China Plasma Dyna
【出 处】
:
第六届亚洲推进与动力国际会议
【发表日期】
:
2012年9期
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