几何结构对尾缘层板气膜冷却特性的影响 / Investigation on the effects of geometrical structure on film cooling performance of trailing edge lamilloy
- Resource Type
- Academic Journal
- Source
- 固体火箭技术 / Journal of Solid Rocket Technology. 41(1):112-134
- Subject
层板冷却 尾缘劈缝 几何结构 气膜冷却 数值计算 - Language
- Chinese
- ISSN
- 1006-2793