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氢/氧气-气喷注器冷流掺混与燃烧比较的仿真研究

汪小卫 金平 杜正刚 蔡国飙

汪小卫, 金平, 杜正刚, 蔡国飙. 氢/氧气-气喷注器冷流掺混与燃烧比较的仿真研究[J]. 航空动力学报, 2008, 23(9): 1737-1742.
引用本文: 汪小卫, 金平, 杜正刚, 蔡国飙. 氢/氧气-气喷注器冷流掺混与燃烧比较的仿真研究[J]. 航空动力学报, 2008, 23(9): 1737-1742.
WANG Xiao-wei, JIN Ping, DU Zheng-gang, CAI Guo-biao. Simulation of cold flow and combustion characteristics of shear-coaxial GH2/GO2 injectors[J]. Journal of Aerospace Power, 2008, 23(9): 1737-1742.
Citation: WANG Xiao-wei, JIN Ping, DU Zheng-gang, CAI Guo-biao. Simulation of cold flow and combustion characteristics of shear-coaxial GH2/GO2 injectors[J]. Journal of Aerospace Power, 2008, 23(9): 1737-1742.

氢/氧气-气喷注器冷流掺混与燃烧比较的仿真研究

基金项目: 国家863项目(2006AA702304)

Simulation of cold flow and combustion characteristics of shear-coaxial GH2/GO2 injectors

  • 摘要: 分别采用无化学反应的和带化学反应的湍流N-S方程描述发动机内流动过程,对气-气同轴剪切式单喷注器进行了冷流掺混和燃烧的仿真.其中化学反应速率由Arrhenius公式计算,采用9步详细反应动力学模型来描述氢氧反应.对典型冷流和燃烧仿真结果进行了比较,结果表明燃烧掺混速率明显小于冷流掺混速率;并对同轴喷注器关键参数对冷流和燃烧掺混的影响进行了仿真和分析比较,得到速度比、缩进量和喷注流量的影响是一致的,而喷注速度的影响是相反的.

     

  • [1] Farhangi S,Yu T,Rojast L,et al.Gas-gas injector technology for full flow stage combustion cycle application[R].AIAA 1999-2757.
    [2] Jones J M,Nichols J T,Boyce W D,et al.Integrated powerhead demonstration:Full flow cycle development[R].Air Force Research Lab 4 DracoEdwards AFB,Aerojet PO Box 13222 Sacramento,William F.Sack,Boeing Defence & Space Group 6633 Canoga Ave Canoga Park,AFRL-PR-ED-TP-1998-003.
    [3] Davis J A,Campbell R L.Advantages of a full-flow staged combustion cycle engine system[R].AIAA 97-3318,1997.
    [4] Calhoon D,ho J,Kors D.Investigation of gaseous propellant combustion and associated injector-chamber design guide-lines[R].Aerojet Liquid Rocket Company,NASA CR-121234,Contract NAS3-13379,July 1973.
    [5] Muss J A,Johnson C W.Numerical cold flow and combustion characterization of swift coaxial injectors[R].AIAA 2003-124.
    [6] Foust M J,Deshpande M,Pal S,et al.Experimental and analytical characterization of a shear coaxial cornbusting GO2/GH2 flowfield[R].AIAA 1996-0646.
    [7] Tucker P K,Klemt M D,Smith T D,et al.Design of efficient GO2/GH2 injectors[R].A NASA,Industry and University Cooperative Effort,AIAA 1997.
    [8] Archambault M R,Talley D.Computational analysis of a single-element,shear-coaxial,GH2/GO2 engine[R].AIAA 2002-1088.
    [9] Marshall W MoPal S,Woodward R D,et al.Benchmark wall heat flux data for a GO2/GH2 single element combustor[R].AIAA-2005-3572.
    [10] Archambault M.Three-dimensional simulation of a gas/ gas,hydrogen/oxygen engine[R].AFRL-PR-ED-AB-2002-276.
    [11] Archamhault M,COhn R,Talley D.Computational analysis of a single-element,shear-coaxial,GH2/GO2 engine[R].AFRL-PR-ED-AB-2001-082.
    [12] Guo Biao,Jin Ping,Yang Lijun,et al.Experimental and numerical investigation of gas-gas injectors for full flow stage combustion cycle engine[R].AIAA-2005-3745.
    [13] 王福军.计算流体动力学分析[M].北京:清华大学出版社,2004.
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出版历程
  • 收稿日期:  2007-08-27
  • 修回日期:  2007-11-23
  • 刊出日期:  2008-09-28

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