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	Airframe/intake-exhaust integration design of flying wing using a multi-bump strategy
	Gan, Wenbiao; Zhou, Zhou; Zhang, Xiaocui
刊名	PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
	2017
卷号	231页码:2396-2407
关键词	Multi-bump design strategy flying wing airframe intake-exhaust transition model flow control optimization
ISSN号	0954-4100
DOI	10.1177/0954410016664925
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000414034400007
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5937803
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Gan, Wenbiao,Zhou, Zhou,Zhang, Xiaocui. Airframe/intake-exhaust integration design of flying wing using a multi-bump strategy[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,2017,231:2396-2407.
APA	Gan, Wenbiao,Zhou, Zhou,&Zhang, Xiaocui.(2017).Airframe/intake-exhaust integration design of flying wing using a multi-bump strategy.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,231,2396-2407.
MLA	Gan, Wenbiao,et al."Airframe/intake-exhaust integration design of flying wing using a multi-bump strategy".PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING 231(2017):2396-2407.

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