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	Flow control mechanisms of a combined approach using blade slot and vortex generator in compressor cascade
	Hu, Jiaguo; Wang, Rugen; Huang, Danqin
刊名	AEROSPACE SCIENCE AND TECHNOLOGY
	2018
卷号	78页码:320-331
关键词	Fighter aircraft Flow control Vorticity Compressor cascade Control mechanism Corner separation Counter-rotating vortices Numerical results Separation control Suction surfaces Vortex generators Vortex flow
ISSN号	1270-9638
DOI	10.1016/j.ast.2018.04.034
URL标识	查看原文
收录类别	SCIE
WOS记录号	WOS:000436215700028
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5933483
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Hu, Jiaguo,Wang, Rugen,Huang, Danqin. Flow control mechanisms of a combined approach using blade slot and vortex generator in compressor cascade[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2018,78:320-331.
APA	Hu, Jiaguo,Wang, Rugen,&Huang, Danqin.(2018).Flow control mechanisms of a combined approach using blade slot and vortex generator in compressor cascade.AEROSPACE SCIENCE AND TECHNOLOGY,78,320-331.
MLA	Hu, Jiaguo,et al."Flow control mechanisms of a combined approach using blade slot and vortex generator in compressor cascade".AEROSPACE SCIENCE AND TECHNOLOGY 78(2018):320-331.

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