国家自然科学基金(Project50806073)

作品数:2被引量:13H指数:2
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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动力工程及工程热物理更多>>
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Numerical Investigation of the Unsteady Tip Leakage Flow and Rotating Stall Inception in a Transonic Compressor被引量:6
《Journal of Thermal Science》2010年第4期310-317,共8页Yanfeng Zhang Xingen Lu Wuli Chu Junqiang Zhu 
National Natural Science Foundation of China(Project No:50806073)
It is well known that tip leakage flow has a strong effect on the compressor performance and stability. This paper reports on a numerical investigation of detailed flow structures in an isolated transonic compressor r...
关键词:transonic axial-flow compressor tip clearance flow stall inception UNSTEADINESS 
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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