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	Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number
	Lu, Huawei; Yang, Yi; Guo, Shuang; Pang, Wenxuan; Yang, Fan; Zhong, Jingjun
刊名	AEROSPACE SCIENCE AND TECHNOLOGY
	2019
卷号	85页码:48-60
关键词	Highly loaded compressor cascade Dimple Flow loss Variation of inlet Mach number
ISSN号	1270-9638
DOI	10.1016/j.ast.2018.11.054
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000457819900005
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5922784
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Lu, Huawei,Yang, Yi,Guo, Shuang,et al. Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2019,85:48-60.
APA	Lu, Huawei,Yang, Yi,Guo, Shuang,Pang, Wenxuan,Yang, Fan,&Zhong, Jingjun.(2019).Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number.AEROSPACE SCIENCE AND TECHNOLOGY,85,48-60.
MLA	Lu, Huawei,et al."Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number".AEROSPACE SCIENCE AND TECHNOLOGY 85(2019):48-60.

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