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...
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 ...