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	An investigation for the turbine blade film cooling performance on the suction side tip region under rotating condition
	Wang, H.; Tao, Z.; Zhou, Z.; Zhao, G.; Han, F.; Li, H.
刊名	Applied Thermal Engineering
	2019
卷号	150页码:864-874
关键词	Cooling Numerical models Reynolds number Turbines Turbomachine blades Film cooling performance Film performance K epsilon models Leakage vortex Rotating blades Rotating conditions Rotating turbines Rotation effect Vortex flow
ISSN号	13594311
DOI	10.1016/j.applthermaleng.2018.12.102
URL标识	查看原文
收录类别	EI
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5922356
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Wang, H.,Tao, Z.,Zhou, Z.,et al. An investigation for the turbine blade film cooling performance on the suction side tip region under rotating condition[J]. Applied Thermal Engineering,2019,150:864-874.
APA	Wang, H.,Tao, Z.,Zhou, Z.,Zhao, G.,Han, F.,&Li, H..(2019).An investigation for the turbine blade film cooling performance on the suction side tip region under rotating condition.Applied Thermal Engineering,150,864-874.
MLA	Wang, H.,et al."An investigation for the turbine blade film cooling performance on the suction side tip region under rotating condition".Applied Thermal Engineering 150(2019):864-874.

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