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[1]石晓波,刘占一,郭灿琳.燃气发生器喷注器内氧腔三维流动分析[J].火箭推进,2013,39(02):6-11.
 SHI Xiao-bo,LIU Zhan-yi,GUO Can-lin.Analysis of three-dimensional flow in oxygen chamber in injector of gas generator[J].Journal of Rocket Propulsion,2013,39(02):6-11.
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燃气发生器喷注器内氧腔三维流动分析

参考文献/References:

[1]张贵田, 高压补燃液氧煤油发动机[M]. 北京: 国防工业出版社, 2005, 8.
[2]赵文涛, 聂万胜, 庄逢辰. 有隔板和无隔板的液体火箭发动机冷态全流场数值模拟[J]. 推进技术, 1997, 18(2): 16-20.
[3]李小平, 葛李虎, 吴宝元. 富氧发生器喷注单元二次喷注后的流场研究[J]. 火箭推进, 2002, 28(4): 14-19.
[4]冯喜平, 何洪庆, 葛李虎. 预燃室三维湍流和燃烧过程的数值模拟[J]. 推进技术, 2002, 23(2):121-125.
[5]费继友, 俞炳丰, 张杰, 等. 液体火箭发动机推力室粘性流场数值模拟和实验验证[J]. 推进技术, 2003, 24(4): 292-295.
[6] SALVADOR N M C, MORALES M M, MIGUEIS C E S S, et al. Numerical simulation of a liquid propellant rocket motor [J]. Journal of Thermal Science, 2000, 10(1): 83-86.
[7]杨青真, 王红梅, 张银波. 液态火箭发动机氧腔流动分析及均流板设计研究[J]. 宇航学报, 2005, 6(26): 698-701.
[8] 王晓丽, 燃气发生器氢腔均流改进设计及试验研究[J]. 火箭推进, 2011, 37(2): 38-42.
[9]王福军. 计算流体动力学分析[M]. 北京: 清华大学出版社, 2005.
[10]景思睿, 张鸣远. 流体力学[M]. 西安: 西安交通大学出版社, 2001.

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备注/Memo

收稿日期:2013-01-14;修回日期:2013-02-25
基金项目:国家863项目(2009AA705211)
作者简介:石晓波(1977—),男,高级工程师,研究领域为液体火箭发动机气动传热

更新日期/Last Update: 1900-01-01