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某发动机喷管周围流场研究 被引量:2

Research of flow field around nozzle of an engine
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摘要 运用Fluent流体动力学软件,采用结构化网格和RNG k-ε湍流模型研究了热试车条件下,某带高温隔热屏发动机喷管周围及隔热屏上温度场的分布,计算结果与试验结果吻合较好。研究结果表明:推进系统热试车条件下,高温隔热屏各组成部分温度均在各自耐受温度以内;高温隔热屏能有效地将发动机羽流的对流及辐射进行隔离,避免高温燃气对发动机周围的推进系统组件进行再加热。 The fluid dynamics software Fluent, structured grids and RNG k-ε turbulence model are used in this paper to research the temperature field distribution around the nozzle with high-tem- perature heat shield and on the high-temperature heat shield of an engine under the condition of the ground hot test. The calculation results agree well with the experimental results. The results show that, under the condition of the ground hot test of propulsion system, the temperature of all parts of the high-temperature heat shield is within their heat tolerance, and the high-temperature heat shield can effectively isolate the convection and radiation of engine plume and can avoid the propulsion system components around the engine from heating of high-temperature gas.
出处 《火箭推进》 CAS 2013年第5期41-45,81,共6页 Journal of Rocket Propulsion
基金 中国航天科技集团公司支撑项目(2011JY01)
关键词 高温隔热屏 温度场 推进系统 Fluent软件 high-temperature heat shield temperature field propulsion system Fluent software
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参考文献7

  • 1DETFLEFF G, BOETYCHER R D, DANKERT C, et al. Attitude control thruster plume flow modeling and experiments [J]. Journal of Spacecraft and Rockets, 1986, 23(5): 476-481.
  • 2PENKO P F, BOYD I D, MEISSNER D L, et al. Pressure measurements in a low-density nozzle plume for code veri- fication, AIAA 91-2110[R]. US: AIAA, 1991.
  • 3PENKO P F, BOYD I D, MEISSNIR D L, et al. Measurement and analysis of a small nozzle plume in vacuum, AIAA 92-3108[R]. US: AIAA, 1992.
  • 4BOYD I D, PENKO P F, MEISSNER D L, et al. Experimental and numerical investigations of low density nozzle and plume flows of nitrogen[J]. AIAA Journal, 1992, 30(10): 2453-2461.
  • 5张建华,贺碧蛟,蔡国飙.轴对称羽流流场数值模拟和实验验证[J].北京航空航天大学学报,2011,37(5):524-527. 被引量:3
  • 6张建华,贺碧蛟,蔡国飙,陈爱国,杨彦广,李震乾.卫星姿控发动机喷管羽流撞击效应试验[J].空气动力学学报,2007,25(2):250-255. 被引量:10
  • 7庄逢辰,赵文涛,刘卫东,邹勤,聂万胜.液体火箭发动机燃烧稳定性CFD分析[J].燃烧科学与技术,2001,7(1):16-20. 被引量:14

二级参考文献22

  • 1张建华,贺碧蛟,蔡国飙,陈爱国,杨彦广,李震乾.卫星姿控发动机喷管羽流撞击效应试验[J].空气动力学学报,2007,25(2):250-255. 被引量:10
  • 2Dettleff G. Plume flow and plume impingement in space technology[J]. Progress in Aerospace Science,1991,28(1 ) :1 -71.
  • 3Dettleff G, Boettcher R D, Dankert C, et al. Attitude control thruster plume flow modelling and experiments [ J ]. Journal of Spacecraft and Rockets, 1986,23 (5) :476 - 481.
  • 4Penko P F, Boyd I D, Meissner D L, et al. Pressure measurements in a low-density nozzle plume for code verification [ R ]. AIAA 91-2110,1991.
  • 5Penko P F, Boyd I D, Meissner D L, et al. Measurement and anal- ysis of a small nozzle plume in vacuum[ R]. AIAA 92-3108, 1992.
  • 6Boyd I D,Penko P F,Meissner D L,et al. Experimental and numerical investigations of low-density nozzle and plume flows of nitrogen [J]. AIAA Journal,1992,30(10) :2453 -2461.
  • 7George J D,Boyd 1 D. Simulation of nozzle plume flows using a combined CFD-DSMC approach[ R]. AIAA 99-3454,1999.
  • 8Rosenhauer M, Plahn K, Hannemann K. Comparison of decou- pied hybrid Navier-Stokes:DSMC calculation with experiments in plumes[ C ]//Rarefied Gas Dynamics 21st International Sympo- sium. Toulouse : C6padu6s Edition, 1999:671 - 678.
  • 9Bird G A. Molecular gas dynamics and the direct simulation of gas flows[ M ]. Clarendon Oxford, 1994.
  • 10DETTLEFF G,BOETTCHER R D,DANKERT C,KPPPENWALLNER G,LEGGE H.Attitude control thruster plume flow modelling and experiments[J].Journal of Spacecraft and Rockets,1986,23(5):476-481.

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