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燃烧室新型迷宫复合冷却结构冷流入射角对冷却性能影响的数值研究
引用本文:李名魁,何立明,蒋永健,金涛. 燃烧室新型迷宫复合冷却结构冷流入射角对冷却性能影响的数值研究[J]. 机械科学与技术, 2006, 25(5): 539-541
作者姓名:李名魁  何立明  蒋永健  金涛
作者单位:空军工程大学工程学院 西安710038
摘    要:针对燃烧室新型迷宫复合冷却结构,以F luent商业软件为计算平台,采用数值模拟方法研究了该冷却结构外侧壁面上冷却孔开孔角度分别为-60°、-30°、+30°、+60°时内外壁温的分布情况,获得了其壁温及冷却效率的分布规律。研究表明,开孔角度为+30°时冷却效率最高。计算结果对于迷宫复合冷却结构的设计和冷却性能试验研究都具有一定的理论指导意义。

关 键 词:燃烧室  迷宫复合冷却结构  开孔角度  冷却性能  数值模拟
文章编号:1003-8728(2006)05-0539-03
收稿时间:2005-10-20
修稿时间:2005-10-20

Numerical Simulation of Effects of Coolant Air Blowing Incidence on Effusion Cooling Efficiency of Maze Composition Cooling Structures in Combustors
Li Mingkui,He Liming,Jiang Yongjian,Jin Tao. Numerical Simulation of Effects of Coolant Air Blowing Incidence on Effusion Cooling Efficiency of Maze Composition Cooling Structures in Combustors[J]. Mechanical Science and Technology for Aerospace Engineering, 2006, 25(5): 539-541
Authors:Li Mingkui  He Liming  Jiang Yongjian  Jin Tao
Abstract:In order to obtain the wall temperature and cooling efficiency distribution characteristics of maze composition structures in combustors with blowing angles of-60°,-30°,+30°,+60°,0° respectively,the paper uses a two-dimensional numerical simulation method and commercial software of FLUENT.The simulation results provide theoretical basis for the design of maze composition structures and for the experimental investigation of cooling performance,showing that cooling efficiency is the best when the blowing angle is 30°.
Keywords:combustor   maze composition cooling structure   blowing angle   cooling performance   numerical simulation
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