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
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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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