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激光能量主动控制高超声速进气道研究现状 被引量:2

Development of laser energy controlling flow field of hypersonic inlet
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摘要 以注入激光能量的方式对高超声速进气道进行主动流动控制是提高超燃冲压发动机性能的一种重要方法。回顾了国际学者针对斜激波相互作用、Edney IV型激波相互作用和来流捕获这3项内容的控制方法和结果,为国内主动控制高超声速流场的研究提供了有益参考。 Laser energy deposition is an efficient way in promoting the performance of the engine by controlling the hypersonic inlet flow filed. Methods and results in control of the interaction of oblique shock, Edney IV interaction and capture of mass flow are reviewed in this work. Useful references in research of the active control of the hypersonic flow filed are provided.
出处 《激光杂志》 CAS CSCD 北大核心 2012年第5期1-2,共2页 Laser Journal
关键词 激光能量沉积 流动控制 高超声速 进气道 laser energy deposition flow control hypersonic inlet
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参考文献17

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