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带有前缘气膜冷却燃气轮机叶片的气热耦合研究(英文) 被引量:2
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作者 董平 王强 +2 位作者 郭兆元 黄洪雁 冯国泰 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2009年第2期145-152,共8页
Conjugate calculation methodology is used to simulate the C3X gas turbine vanes cooled with leading edge films of 'shower- head' type. By comparing calculated results of different turbulence models with the me... Conjugate calculation methodology is used to simulate the C3X gas turbine vanes cooled with leading edge films of 'shower- head' type. By comparing calculated results of different turbulence models with the measured data, it is clear that calculation with the transition model can better simulate the flow and heat transfer in the boundary layers with leading edge film cooling. In the laminar boundary layers, on the upstream suction side, the film cooling flow presents 3D turbulent characteristics before tran... 展开更多
关键词 gas turbine conjugate calculation leading edge film cooling TRANSITION temperature gradient
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