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冲压发动机气膜冷却分析模型
引用本文:凌文辉,王以飞,裘云,刘凤君,刘松龄. 冲压发动机气膜冷却分析模型[J]. 推进技术, 2011, 32(5): 713-716
作者姓名:凌文辉  王以飞  裘云  刘凤君  刘松龄
作者单位:1. 南京航空航天大学能源与动力学院,江苏南京210016/中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京100074
2. 中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京,100074
3. 西北工业大学动力与能源学院,陕西西安,710072
摘    要:本文建立了冲压发动机燃烧室气膜冷却传热分析程序。根据燃烧室设计的技术要求,从冷却性能角度完成气膜冷却系统的气动性能和传热特性分析,提供冷却结构优化所需的信息。

关 键 词:冲压发动机  燃烧室  气膜冷却  气动特性  传热

A model to analyze the film cooling characteristics of a ramjet combustor
LING Wen-hui,WANG Yi-fei,QIU Yun,LIU Feng-jun and LIU Song-ling. A model to analyze the film cooling characteristics of a ramjet combustor[J]. Journal of Propulsion Technology, 2011, 32(5): 713-716
Authors:LING Wen-hui  WANG Yi-fei  QIU Yun  LIU Feng-jun  LIU Song-ling
Affiliation:LING Wen-hui1,2,WANG Yi-fei2,QIU Yun2,LIU Feng-jun2,LIU Song-ling3(1.School of Energy and Power,Nanjing Univ. of Aeronautics and Astronautics,Nanjing 210016,China,2.Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,3.School of Power and Energy,Northwestern Polytechnic Univ.,Xi' an 710072,China)
Abstract:The heat transfer analysis model for the cooling film of ramjet engine was established in the present paper.In order to meet the combustion chamber design requirement,the heat transfer analysis for a ramjet cooling system was finished,with a focus on the cooling performance.The analysis results can be used to provide useful information for the optimization of a cooling system for ramjet engines.
Keywords:Ramjet engine  Combustion chamber  Film cooling  Aerodynamic characteristic  Heat transfer  
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