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	Understanding better 'artificial total pressure loss' in multi-stage axial-flow compressor
	Gao, Limin; Liu, Haihu; Liu, Bo; Chen, Yunyong
刊名	Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
	2008
卷号	26期号:1页码:1-5
关键词	Artificial total pressure loss Axial flow compressors Blade rows Central difference scheme Mixing plane approach Time marching method
ISSN号	1000-2758
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/4847385
专题	西安交通大学
推荐引用方式 GB/T 7714	Gao, Limin,Liu, Haihu,Liu, Bo,et al. Understanding better 'artificial total pressure loss' in multi-stage axial-flow compressor[J]. Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University,2008,26(1):1-5.
APA	Gao, Limin,Liu, Haihu,Liu, Bo,&Chen, Yunyong.(2008).Understanding better 'artificial total pressure loss' in multi-stage axial-flow compressor.Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University,26(1),1-5.
MLA	Gao, Limin,et al."Understanding better 'artificial total pressure loss' in multi-stage axial-flow compressor".Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 26.1(2008):1-5.

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