动静干涉下高压涡轮外环非定常气膜冷却性能分析 / Unsteady Film Cooling Performance Analysis of High-pressure Turbine Shroud under Rotor-stator Interaction
- Resource Type
- Academic Journal
- Source
- 航空发动机 / Aeroengine. 49(4):9-15
- Subject
高压涡轮外环 非定常气膜冷却 叶顶间隙 泄漏流 泄漏涡 动静干涉 航空发动机 turbine shroud unsteady film cooling blade tip clearance leakage flow leakage vortex rotor-stator Interaction aeroengine - Language
- Chinese
- ISSN
- 1672-3147