inner passage

基本解释

The cooling technique of the blade inner passage plays a significant role in the design of blades for gas turbine.
叶片内部通道冷却技术在航空发动机叶片的设计中占有重要的位置。
An inner air passage is created introducing monsoon from the outer openings of the whole building in order to provide natural ventilation.
为了让建筑自然通风，项目设计了一条内部空气通道，将建筑室外的季风导入到内部。
An experimental research was conducted to simulate the effect of trailing edge ejection of turbine blades on heat transfer of the inner cooling passage with staggered pin fin array.
本文用实验的方法模拟研究了涡轮叶片尾缘出流对带叉排扰流柱阵列的内冷通道的对流换热特性的影响。