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	Influence of rotor-stator component partition structure on the aerodynamic performance of centrifugal compressors
	Li, Chunyang; Ji, Chunjun; Shi, Mao; Sun, Qi
刊名	ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS
	2019
卷号	13页码:1080-1094
关键词	Multistage centrifugal compressor rotor-stator components partition structure aerodynamic performance loss mechanism
ISSN号	1994-2060
URL标识	查看原文
WOS记录号	[DB:DC_IDENTIFIER_WOSID]
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/3227380
专题	大连理工大学
作者单位	1.Dalian Univ Technol, Sch Energy & Power Engn, Dalian, Peoples R China. 2.Dalian Univ Technol, Sch Energy & Power Engn, Dalian, Peoples R China. 3.Dalian Univ Technol, Minist Educ, Key Lab Ocean Energy Utilizat & Energy Conservat, Dalian, Peoples R China. 4.Dalian Zhongyi Turbin Technol Co Ltd, Dalian, Peoples R China. 5.Chinese Acad Sci, Inst Engn Thermophys, Beijing, Peoples R China.
推荐引用方式 GB/T 7714	Li, Chunyang,Ji, Chunjun,Shi, Mao,et al. Influence of rotor-stator component partition structure on the aerodynamic performance of centrifugal compressors[J]. ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS,2019,13:1080-1094.
APA	Li, Chunyang,Ji, Chunjun,Shi, Mao,&Sun, Qi.(2019).Influence of rotor-stator component partition structure on the aerodynamic performance of centrifugal compressors.ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS,13,1080-1094.
MLA	Li, Chunyang,et al."Influence of rotor-stator component partition structure on the aerodynamic performance of centrifugal compressors".ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS 13(2019):1080-1094.

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