中国博士后科学基金(Project20070420068)

作品数：1被引量：7H指数：1
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相关期刊：《Journal of Thermal Science》更多>>
相关主题：NUMERICAL_INVESTIGATIONHIGH-NON-AXISYMMETRICAXIAL-FLOWSUBSONIC更多>>
相关领域：航空宇航科学技术机械工程更多>>
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Numerical Investigation of a High-subsonic Axial-flow Compressor Rotor with Non-axisymmetric Hub Endwall被引量：7
《Journal of Thermal Science》2010年第1期14-20,共7页Shuzhen Hu Xingen Lu Hongwu Zhang Junqiang Zhu Qiang Xu 
Financial supports for the work presented are provided by National Natural Science Foundation of China (Project No: 50806073);China Postdoctoral Science Foundation (Project No: 20070420068);K C Wong Education Foundation, these supports are greatly appreciated
The major source of loss in modem compressors is the secondary loss. Non-axisymmetric endwall profile contouring is now a well established design methodology in axial flow turbines. However, flow development in axial ...
关键词：axial-flow compressor non-axisymmetric hub endwali and numerical investigation 
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