1.
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
2.
conduction-cooled turbine blade
(导热)冷却式涡轮叶片
3.
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
4.
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
5.
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
6.
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
7.
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
8.
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
9.
Numerical Investigation of the Flow and Heat Transfer of Steam Cooled Vane;
蒸汽冷却涡轮导向叶片流动与传热的数值模拟和分析
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.
Study on Mechanical Property of Nickel-base Single Crystal Superalloy and Its Application on Cooling Gas Turbine Blade;
镍基单晶合金力学特性及其在冷却涡轮叶片上的应用分析
12.
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
13.
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
14.
Numerical Study of the Augmented Cooling on the Trailing Edge of Turbine Blade;
涡轮叶栅尾缘强化冷却方法的数值研究
15.
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
16.
Clogging up of the cooling air slits in the turbine blades is primarily caused by ultrafine particles with a high specific surface area.
涡轮叶片之间冷却空气缝隙的堵塞主要是因为存在高比表面积的超细粒子。
17.
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
18.
Check no damage for fan blades and turbine blades.
检查风扇叶片和涡轮叶片无损坏迹象。