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	Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling
	Fan, Xiaojun; Li, Liang; Zou, Jiasheng; Zhou, Yuanyuan
刊名	INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER
	2019
卷号	100页码:133-145
关键词	Impingement cooling Comparative study Double vortex cooling Vortex cooling
ISSN号	0735-1933
URL标识	查看原文
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/2826852
专题	西安交通大学
推荐引用方式 GB/T 7714	Fan, Xiaojun,Li, Liang,Zou, Jiasheng,et al. Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling[J]. INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER,2019,100:133-145.
APA	Fan, Xiaojun,Li, Liang,Zou, Jiasheng,&Zhou, Yuanyuan.(2019).Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling.INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER,100,133-145.
MLA	Fan, Xiaojun,et al."Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling".INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER 100(2019):133-145.

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