A cad system for three dimensional electrode of turbo blade mould part is developed in this paper 摘要开发了一个针对涡轮叶片模具活块的电极零件的cad系统。
The surface of a gas turbine blade was cooled by four rows of cylindrical holes in the experiment 实验中对涡轮叶片采用四排气膜孔的冷却方案，气膜孔为圆柱形。
The cooling technology of the turbine blades was very important to improve the efficiency of the aeroengine 涡轮叶片的冷却技术对提高航空发动机性能是至关重要的。
The experimental results showed that the film cooling effectiveness were mainly determined by blowing ratios 该实验结果对涡轮叶片型面气膜冷却的实际工程设计研究有重要意义。
Short pin - fin arrays are often used for the cooling of turbine airfoils , particularly in the trailing edge 短扰流柱排被广泛应用于涡轮叶片的内部冷却结构中，尤其是叶片尾缘区域。
Turbine blades with new , more sophisticated designs have to be finished via machining and preferably by hsm 新型、形状复杂的涡轮叶片必须通过切削来完成加工，最好是用高速切削完成。
To analysis the heat environment in the turbine , it ' s required to couple a flow solver with a conduction heat transfer solver 本文从实验和计算的角度对涡轮叶片中的流场、温度场耦合进行了研究。
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。
A feature information model is proposed to combine the design information and the geometric information of turbine blade in a same model 本文提出了涡轮叶片特征信息模型，将涡轮叶片的设计信息和几何信息有机的统一在了一起。
Two good examples about conjugate heat transfer problem , one with cooling method , the other without cooling inside turbine blade were investigated 最后进一步地讨论了涡轮叶片中无冷却和有简单冷却通道情况下的流/热耦合计算。
