1.
Coupled heat transfer simulations of a transonic vane by taking account of transition flows
考虑转捩的跨声速气冷涡轮叶片气热耦合计算
2.
Research on Conjugate Heat Transfer Simulation of Aero Turbine Engine Air-Cooled Vane
航空发动机气冷涡轮叶片的气热耦合数值模拟研究
3.
conduction-cooled turbine blade
(导热)冷却式涡轮叶片
4.
Influence of Air-film Hole Shapes on Turbine Blade Air-film Cooling Effectiveness
气膜孔形状对涡轮叶片气膜冷却效果的影响
5.
Heat Transfer Investigation of Film Cooling on the Leading Edge of Turbine Blade;
涡轮叶片前缘气膜冷却的传热实验研究
6.
Investigation of Trailing Edge Film Cooling by Jets Ejected from a Slot;
涡轮叶片尾缘半劈缝气膜冷却实验研究
7.
Influence of the film cooling hole on the endurance life of the turbine blade
涡轮叶片持久寿命预测中气膜冷却孔的影响
8.
Recent Advances in the Study of Influence of Air-film Hole Geometrical Structures on Turbine Blade Air-film Cooling
气膜孔几何结构对涡轮叶片气膜冷却影响的研究进展
9.
Research on Fatigue Life of Large Gas Turbine Blades;
大型燃气轮机涡轮叶片疲劳寿命研究
10.
Investigation of the Influence of Density Ratios on Film Cooling on Turbine Blade Surface;
密度比对涡轮叶片气膜冷却特性影响的实验研究
11.
disc ,rotor (with or without fins) for turbojet engines
叶轮（带或不带叶片）,用于涡轮喷气发动机
12.
blade, for gas turbines (excl. turbopropellers)
叶片，用于燃气轮机（不包括涡轮螺旋桨发动机）
13.
Calculate Thermal Field and Analyze Structural Field for Binary Cooling Turbine Blades
双工质冷却涡轮叶片温度场计算与强度分析
14.
Experimental research of turbulated cooling hole machining by ECM
涡轮叶片竹节孔冷却通道电解加工实验研究
15.
Cooling Passage Design Optimization of Turbine Blades Based on Response Surface Methodology
基于响应面的涡轮叶片冷却通道设计优化
16.
Research on the Heat Transfer of the Endwall Film-cooling in Axial Flow Turbine Cascade;
轴流涡轮叶栅端壁气膜冷却的传热研究
17.
Numerical Investigation of Air-cooled Gas Turbine Flow and Thermal Stress Characteristics
气冷涡轮叶栅流动及热应力特性的数值研究
18.
Heat Transfer Experimental Investigation on Full Film Cooling of Turbine Vane Surface
涡轮静叶表面全气膜冷却换热实验研究