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	Numerical study on boundary layer suction at throat of a CARET inlet [一种CARET进气道喉部附面层抽吸数值研究]
	He, T.; Wang, Q.
刊名	Hangkong Dongli Xuebao/Journal of Aerospace Power
	2018
卷号	33页码:2278-2284
关键词	Computational fluid dynamics Flow control Flow fields Flow separation Recovery Boundary layer interaction Boundary layer suction CARET inlet Inlet performance Throat section Total pressure distortion Total pressure recovery Total pressure recovery coefficient Boundary layers
ISSN号	10008055
DOI	10.13224/j.cnki.jasp.2018.09.026
URL标识	查看原文
收录类别	CSCD
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5929605
专题	北京航空航天大学
推荐引用方式 GB/T 7714	He, T.,Wang, Q.. Numerical study on boundary layer suction at throat of a CARET inlet [一种CARET进气道喉部附面层抽吸数值研究][J]. Hangkong Dongli Xuebao/Journal of Aerospace Power,2018,33:2278-2284.
APA	He, T.,&Wang, Q..(2018).Numerical study on boundary layer suction at throat of a CARET inlet [一种CARET进气道喉部附面层抽吸数值研究].Hangkong Dongli Xuebao/Journal of Aerospace Power,33,2278-2284.
MLA	He, T.,et al."Numerical study on boundary layer suction at throat of a CARET inlet [一种CARET进气道喉部附面层抽吸数值研究]".Hangkong Dongli Xuebao/Journal of Aerospace Power 33(2018):2278-2284.

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