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Solution of Turbine Blade Cascade Flow Using an Improved Panel Method
Lei, Zong-qi; Liang, Guo-zhu
刊名INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING
2015
卷号2015
关键词Turbine components Turbines Cascade flow Comparison with experiments Compressibility correction Deviation angles Inviscid flows Meshfree Panel methods Turbine blade Turbomachine blades
ISSN号1687-5966
DOI10.1155/2015/312430
URL标识查看原文
收录类别SCIE ; EI
WOS记录号WOS:000366865100001
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/6541879
专题北京航空航天大学
推荐引用方式
GB/T 7714
Lei, Zong-qi,Liang, Guo-zhu. Solution of Turbine Blade Cascade Flow Using an Improved Panel Method[J]. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,2015,2015.
APA Lei, Zong-qi,&Liang, Guo-zhu.(2015).Solution of Turbine Blade Cascade Flow Using an Improved Panel Method.INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,2015.
MLA Lei, Zong-qi,et al."Solution of Turbine Blade Cascade Flow Using an Improved Panel Method".INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 2015(2015).
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