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富氢/富氧燃气气-气多喷嘴正交优化设计与分析

陈涛 李茂 金平 蔡国飙

陈涛, 李茂, 金平, 蔡国飙. 富氢/富氧燃气气-气多喷嘴正交优化设计与分析[J]. 航空动力学报, 2011, 26(9): 2002-2008.
引用本文: 陈涛, 李茂, 金平, 蔡国飙. 富氢/富氧燃气气-气多喷嘴正交优化设计与分析[J]. 航空动力学报, 2011, 26(9): 2002-2008.
CHEN Tao, LI Mao, JIN Ping, CAI Guo-biao. Design and analysis of GH2/GO2 fired gas multi-injectors orthogonal optimization[J]. Journal of Aerospace Power, 2011, 26(9): 2002-2008.
Citation: CHEN Tao, LI Mao, JIN Ping, CAI Guo-biao. Design and analysis of GH2/GO2 fired gas multi-injectors orthogonal optimization[J]. Journal of Aerospace Power, 2011, 26(9): 2002-2008.

富氢/富氧燃气气-气多喷嘴正交优化设计与分析

基金项目: 国家高技术研究发展计划

Design and analysis of GH2/GO2 fired gas multi-injectors orthogonal optimization

  • 摘要: 基于正交设计研究了各设计参数对富氢/富氧燃气气-气多喷嘴推力室燃烧位置、壁面温度及喷注面板温度的影响趋势和影响程度.方差分析和极差分析结果表明:燃氧速度比是影响燃烧长度和壁面温度的主要因素,较小的氧喷嘴出口厚度有利于降低喷注面板温度,但各因素的交互作用对不同设计目标影响程度差异较大;多目标响应面分析表明:低的氧喷嘴压降,高的燃氧速度比和适当的氧喷嘴厚度能使发动机达到更好的均衡性能.

     

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出版历程
  • 收稿日期:  2010-10-23
  • 修回日期:  2010-12-24
  • 刊出日期:  2011-09-28

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