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架空钢板对火箭发动机试车中地面热载的影响 被引量:8

Effects of Aerial Steel Plate on the Ground Heat Load in Rocket Engine Test Runs
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摘要 采用三维模型对发动机尾流流场进行数值模拟,获得氢氧火箭发动机水平试车和摇摆试车的尾流流场,以及在摇摆试车工况下,架空钢板的铺设高度、铺设宽度和起始铺设位置对地面热载的影响。计算中,采用氢氧单步燃烧反应模型考虑尾流燃气与空气的燃烧,湍流模型选用了标准k-ε模型。仿真结果表明,合理铺设架空钢板,可以大幅减少试车过程中地面的热载,有效保护地面设施。 The wake's flow fields of the hydrogen-oxygen rocket engine in the level tests and the swing tests were simulated numerically with the 3-D model. The influences of the aerial steel plate's aerial height, aerial width and original paving position on the ground heat load were obtained. The single-step H-O reaction model was used for the reactions between the wake gas and air, and the standard k-~ turbulence model was selected in the simulations. The numerical results showed that by paving the aerial steel plate right, the ground heat load can be reduced remarkably, and the ground facilities can be protected effectively.
出处 《导弹与航天运载技术》 北大核心 2013年第2期41-45,共5页 Missiles and Space Vehicles
关键词 液体火箭发动机试验 仿真 热载 燃气温度 热流密度 Liquid rocket engine test Simulation Heat load Gas temperature Heat flux.
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参考文献8

  • 1郭霄峰.液体火箭发动机试验[M].北京:中国宇航出版社,1990.
  • 2Shang H M, Chen Y S, Liaw P. Investigation of chemical kinetics integration algorithms for reacting flows[R]. AIAA 1995-0806, 1995.
  • 3Lin Z Y, Zhou J, Huang Y H, et al. An innovative conception for computational combustion: multi reaction mechanisms for LRE combustion simulation[R]. AIAA 2005-3591, 2005.
  • 4Negishi H, Kumakawa A, Yamanishi N, el al. Heat transfer simulations in liquid rocket engine subscale thrust chambers[R]. AIAA 2008-5241,2008.
  • 5Sozer E, Vaidyanathan A, Segal C, et al. Computational assessment of gaseous reacting flows in single element injector[R]. AIAA 2009-449, 2009.
  • 6庄逢辰.液体火箭发动机喷雾燃烧的理论、模型及应用[M].长沙:国防科技大学出版社,1995.220-250.
  • 7Lin J, West J S, Williams R W, et al. CFD code validation of wall heat fluxs for a GO2/GH2 single element combustor[R]. AIAA 2005-4524 2005.
  • 8Sozer E, Hassan E A, Yun S, et al. Turbulence-chemistrT interaction and heat transfer modeling of H2/O2 gaseous injector flows[R]. AIAA 2010-1525, 2010.

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