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	Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration
	Zhang, Jing; Kang, Wenwen; Yang, Lingyu
刊名	AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
	2019
卷号	91页码:1285-1294
关键词	Computational fluid dynamics Aerodynamic characteristics Boundary layer ingestion Distributed propulsion configuration
ISSN号	1748-8842
DOI	10.1108/AEAT-06-2018-0174
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000491169100004
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5915985
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Zhang, Jing,Kang, Wenwen,Yang, Lingyu. Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration[J]. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY,2019,91:1285-1294.
APA	Zhang, Jing,Kang, Wenwen,&Yang, Lingyu.(2019).Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration.AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY,91,1285-1294.
MLA	Zhang, Jing,et al."Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration".AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY 91(2019):1285-1294.

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