This paper introduces the cooling effectiveness experiment research on a compound air-cooledturbine vane.
介绍了复合式气冷涡轮导叶的冷却效果试验研究。
2
Considering the geometric features of the aircooledturbine blades of the aircraft engines, the methods to sort the features in the parametric modeling of the blades were advanced.
针对航空发动机涡轮气冷叶片的结构特点，提出了叶片参数化建模的特征分类形式。
3
A general nonlinear finite element code has been applied to thermoelastic stress analysis of directionally solidified aircooledturbine blades.