Author:
Jin Donghai,Liu Xiwu,Zhao Weiguang,Gui Xingmin
Funder
National Natural Science Foundation of China
National Basic Research Program of China
Fundamental Research Funds for the Central Universities of China
Subject
Mechanical Engineering,Aerospace Engineering
Reference24 articles.
1. Performance assessment of an annular S-shaped duct;Bailey;J Turbomach,1997
2. Dueñas CO, Miller RJ, Hodson HP, Longley JP. Effect of length on compressor inter-stage duct performance. Proceedings of ASME Turbo Expo 2007: power for land, sea, and air; 2007 May 14–17; Montreal, Canada. New York: ASME; 2007.
3. Integrated outlet guide vane design for an aggressive S-shaped compressor transition duct;Walker;J Turbomach,2013
4. Rose MG. Non-axisymmetric endwall profiling in the HP NGV’s of an axial flow gas turbine. Proceedings of international gas turbine and aeroengine congress and exposition; 1994 Jun 13–18; The Hegue, Netherlands. New York: ASME; 1994.
5. Hartland JC, Gregory-Smith DG, Rose MG. Non-axisymmetric endwall profiling in a turbine rotor blade. Proceedings of international gas turbine and aeroengine congress and exposition; 1998 Jun 2–5; Stockholm, Sweden. New York: ASME; 1998.
Cited by
22 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