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	Numerical simulation of heat transfer of n-decane under supercritical pressure in horizontal rectangular cooling channels [超临界压力下正癸烷在水平矩形冷却通道内的流动传热数值模拟]
	Zhang, Z.; Huang, S.; Gao, X.
刊名	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
	2018
卷号	39
关键词	Buoyancy Computational fluid dynamics Cooling Engines Heat flux Location Numerical models Paraffins Ramjet engines, Active cooling Distribution of temperature Heat Transfer enhancement Heat transfer predictions Hydrocarbon fuel Rectangular cooling channels Simulation of heat transfer Super-critical pressures, Heat transfer performance
ISSN号	10006893
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/3249359
专题	大连理工大学
作者单位	School of Aeronautics and Astronautics, Dalian University of Technology, Dalian, 116024, China
推荐引用方式 GB/T 7714	Zhang, Z.,Huang, S.,Gao, X.. Numerical simulation of heat transfer of n-decane under supercritical pressure in horizontal rectangular cooling channels [超临界压力下正癸烷在水平矩形冷却通道内的流动传热数值模拟][J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2018,39.
APA	Zhang, Z.,Huang, S.,&Gao, X..(2018).Numerical simulation of heat transfer of n-decane under supercritical pressure in horizontal rectangular cooling channels [超临界压力下正癸烷在水平矩形冷却通道内的流动传热数值模拟].Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,39.
MLA	Zhang, Z.,et al."Numerical simulation of heat transfer of n-decane under supercritical pressure in horizontal rectangular cooling channels [超临界压力下正癸烷在水平矩形冷却通道内的流动传热数值模拟]".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 39(2018).

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