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Regeneratively cooled scramjet heat transfer calculation and comparison with experimental data
文献类型:期刊
作者:Jiang, Jin[1]  Zhang, Ruo-Ling[2]  Le, Jia-Ling[3]  Liu, Wei-Xiong[4]  Yang, Yang[5]  Zhang, Lei[6]  Zhao, Guo-Zhu[7]  
机构:[1]Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute of CARDC, Sichuan, Mianyang 621000, China
[2]Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute of CARDC, Sichuan, Mianyang 621000, China
[3]Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute of CARDC, Sichuan, Mianyang 621000, China
[4]Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute of CARDC, Sichuan, Mianyang 621000, China
[5]Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute of CARDC, Sichuan, Mianyang 621000, China
[6]School of Mechanical Engineering, Southwest Jiaotong University, Sichuan, Chengdu, China
[7]School of Power and Energy, Northwestern Polytechnical University, Xi'an, China
通讯作者:Jiang, J (reprint author), Hyperveloc Aerodynam Inst CARDC, Sci & Technol Scramjet Lab, Mianyang 621000, Sichuan, Peoples R China.
年:2014
期刊名称:PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING影响因子和分区
卷:228
期:8
页码范围:1227-1234
增刊:正刊
学科:工程学
收录情况:SCI(E)(WOS:000335722200001)  EI(20142117748633)  
所属部门:动力与能源学院
被引频次:2
人气指数:1589
浏览次数:1560
关键词:Regeneratively cooled scramjet engine; thermal analysis; thermal environment; the heat transfer correlation; test
摘要:
Regeneratively cooled scramjet heat transfer calculation method was developed using three-dimensional calculation for engine solid wall heat conduction. The scramjet thermal environment was determined by engine heat flux measurement and the engine three-dimensional combustion flow calculations. Different heat transfer relationships in the laminar, transition and turbulence fuel flow regions were applied. The cooling fuel flow distribution data inside combustion chamber side panel were obtained b ...More
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