The simulation by using commercial software FLUENT is carried out to explore the mechanism of the heat transfer and gas flow of combined cooling on the leading edge of the blade.
采用FLUENT软件数值模拟了涡轮叶片前缘复合冷却的流动和传热特性。
参考来源 - 涡轮叶片前缘复合冷却研究·2,447,543篇论文数据，部分数据来源于NoteExpress
按照涡轮叶片复合冷却的全过程，本文由三部分组成。
In view of the whole process of composite cooling on a turbine blade, this paper is composed of three parts.
结果表明，复合冷却壁附近炉气温度是影响其传热行为和渣皮厚度的主要因素。
The result shows that gas temperature near the stave is the main factor that affects heat transfer and slag skull thickness.
燃烧室迷宫复合冷却结构是一种集冲击、对流换热和近似发散冷却于一身，结构合理，冷却效率高，具有创新性的新型冷却结构。
A combustors maze composite cooling structure is an innovative and highly efficient cooling structure that integrates impingement, convection heat exchange and approximate perspection cooling.
应用推荐