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	An 11-stage axial compressor performance simulation considering the change of tip clearance in different operating conditions
	Yang Dong; Zheng Xinqian; Li Qiushi
刊名	PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY
	2014
卷号	228页码:614-625
关键词	Turbomachinery aerodynamics multistage axial compressor tip clearance
ISSN号	0957-6509
DOI	10.1177/0957650914535389
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000340166200002
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/6560501
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Yang Dong,Zheng Xinqian,Li Qiushi. An 11-stage axial compressor performance simulation considering the change of tip clearance in different operating conditions[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY,2014,228:614-625.
APA	Yang Dong,Zheng Xinqian,&Li Qiushi.(2014).An 11-stage axial compressor performance simulation considering the change of tip clearance in different operating conditions.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY,228,614-625.
MLA	Yang Dong,et al."An 11-stage axial compressor performance simulation considering the change of tip clearance in different operating conditions".PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY 228(2014):614-625.

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