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[1]周 伟.某膨胀循环发动机推力室冷却结构流场仿真分析[J].火箭推进,2015,41(02):63-69.
 ZHOU Wei.Flow field simulation analysis of cooling configuration in thrust chamber of an expander cycle engine[J].Journal of Rocket Propulsion,2015,41(02):63-69.
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某膨胀循环发动机推力室冷却结构流场仿真分析

参考文献/References:

[1]GEORGI S, GORGEN J, HAIDINGER F A. Flow Simul- ations for the design of Vulcain 2 thrust chamber manifolds, 98-3369 [R]. USA: AIAA,1998.
[2]MATTSTEDT T B, HAIDINGER F, LUGER P, et al. Development, manufacturing and test status of the VINCI expander thrust chamber assembly, AIAA 2002-4009 [R]. USA: AIAA, 2002.
[3]HIDEYO N, DAIMON Y, KAWASHIMA, et al. Conjugated combustion and heat transfer modeling for full-scale regeneratively cooled thrust chambers, AIAA 2013-3997 [R]. USA: AIAA, 2013.
[4]李军伟, 刘宇. 一种计算再生冷却推力室温度场的方法[J]. 航空动力学报, 2004, 19(4): 550-556.

[5]吴峰, 王秋旺, 罗来勤, 等. 液体火箭发动机推力室冷却通道流动与传热数值研究[J]. 推进技术, 2005, 10(5): 389- 393.

[6]张宏伟, 陶文铨, 何雅玲, 等. 再生冷却推力室耦合传热数值模拟[J]. 航空动力学报, 2006, 21(5): 930-936.
[7]韩非, 刘宇. 冷却剂不同流动方式对膨胀循环推力室再生冷却换热的影响[J].航空动力学报, 2006, 21(6):1116-1122.
[8]MCCARTY R D. Hydrogen technological survey: thermo- physical properties, NASA SP-3089[R]. USA: NASA, 1975.
[9]刘国球, 任汉芬, 朱宁昌, 等. 液体火箭发动机原理[M]. 北京: 宇航出版社, 1993.
[10]王福军. 计算流体动力学分析-CFD软件原理与应用[M]. 北京: 清华大学出版社, 2004.
[11]KNAB A F. Advanced cooling circuit layout for the VINCI expander cycle thrust chamber, AIAA 2002- 4005 [R]. USA: AIAA, 2002.

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备注/Memo

收稿日期:2014-08-13;修回日期:2014-12-11 作者简介:周伟(1982—),男,高级工程师,研究领域为液体火箭发动机推力室

更新日期/Last Update: 1900-01-01