Funder
National Natural Science Foundation of China
National Key Technology Research and Development Program of China
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference31 articles.
1. Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor;Suder;ASME J. TurboMach.,1996
2. The exploitation of three-dimensional flow in turbomachinery design;Denton;Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci.,1999
3. Shock/boundary-layer/tip-clearance interaction in a transonic rotor blade;Biollo;AIAA J. Propul. Power,2009
4. W. Hofmann, J. Ballmann, Tip Clearance Vortex Development and Shock-Vortex-Interaction in a Transonic Axial Compressor Rotor, AIAA 2002-0083, 2002.
5. C. Hah, D.C. Rabe, A.R. Wadia, Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor, ASME Paper GT2004-53867.
Cited by
27 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献