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再生冷却超燃冲压发动机整机稳态热分析
引用本文:蒋劲,张若凌,乐嘉陵.再生冷却超燃冲压发动机整机稳态热分析[J].航空动力学报,2009,24(12):2649-2654.
作者姓名:蒋劲  张若凌  乐嘉陵
作者单位:1.西北工业大学动力与能源学院, 西安 710072
摘    要:为了对再生冷却超燃冲压发动机进行热分析,结合三维燃气流场计算软件平台、国内航空煤油物性计算程序,发展了三维热分析计算程序.在Ma=4.9和5.86两种工作状态下,对再生冷却超燃发动机整机进行了三维热分析,得到了发动机局部高温区位置,并研究了冷却剂流量分配对发动机冷却的影响. 

关 键 词:超燃冲压发动机    再生冷却    稳态热分析
收稿时间:2008/11/21 0:00:00
修稿时间:5/5/2009 12:00:00 AM

Steady thermal analysis of regeneratively cooled scramjet
JIANG Jin,ZHANG Ruo-ling and LE Jia-ling.Steady thermal analysis of regeneratively cooled scramjet[J].Journal of Aerospace Power,2009,24(12):2649-2654.
Authors:JIANG Jin  ZHANG Ruo-ling and LE Jia-ling
Institution:1.School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China2.Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
Abstract:In order to analyze the heat transfer in the regeneratively cooled scramjet, three-dimensional internal CFD platform and the computational program of domestic aviation kerosene properties are used together to develop three-dimensional thermal evaluation code .The code was used for Ma=4.9 operating condition as well as Ma=5.86,numerical results show the local high temperature areas in scramjet.The code was also used to study the effects of coolant distribution on the scramjet cooling.
Keywords:scramjet  regenerative cooling  steady thermal analysis
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