高负荷涡轮叶栅气动性能试验汽轮机静叶栅变冲角性能的实验研究不同冲角下有叶顶间隙的涡轮叶栅拓扑与旋涡结构迷宫和薄叶汽封结构与气动特性的对比分析采用流体网络与气热耦合方法的涡轮叶片复合冷却结构改型设计两级轴流压气机流场内流动分离及旋涡运动薄叶式气封在透平级中应用的数值研究Design Optimization of Transonic Compressor Stage Using CFD and Response Surface Model 跨音压气机转子多目标气动优化设计Numerical study of improving aerodynamic performance of low solidity LPT cascade through increasing trailing edge thicknessUse Deflected Trailing Edge to Improve the Aerodynamic Performance and Develop Low Solidity LPT CascadeNumerical Study of Combining Steady Vortex Generator Jets and Deflected Trailing Edge to Reduce the Blade Numbers of Low Pressure Turbine Stage
