Volume 37 Issue 3
Mar.  2011
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Gao Jinhai, Wang Jianjun, Ma Yanhong, et al. Numerical simulation of three dimensional wall temperature of combustor liner based on thermal-fluid-solid coupling method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(3): 300-304. (in Chinese)
Citation: Gao Jinhai, Wang Jianjun, Ma Yanhong, et al. Numerical simulation of three dimensional wall temperature of combustor liner based on thermal-fluid-solid coupling method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(3): 300-304. (in Chinese)

Numerical simulation of three dimensional wall temperature of combustor liner based on thermal-fluid-solid coupling method

  • Received Date: 16 Oct 2009
  • Publish Date: 31 Mar 2011
  • It is the premise and basis of thermal structure analysis to determine the temperature distribution of combustor liner. The three dimensional temperature distribution of a combustor liner was captured by the numerical simulation of an annular return-flow combustion chamber with ANSYS/CFX based on the thermal-fluid-solid coupling finite element method (FEM). The calculation analyzes the effect of heat source and heat radiation, the influence of variable flow field on heat exchange parameter, and the change of the parameters of gas, kerosene, solid with temperature were taken into account. The numerical simulation results demonstrate that the interaction between the flow field and solid wall is more sufficient comparing with traditional methods. The complete feature of flow field and temperature field could be reflected, and the distribution of flow field and temperature field and corresponding flow and heat transfer characteristics could be simulated reasonably. The work is significant on the application of structure design of combustor liner.

     

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  • [1] 杨志民,韩振兴.燃烧室火焰筒壁温三维数值分析[J].航空发动机, 1998(3): 23-27 Yang Zhimin, Han Zhenxing. Numerical simulation of the three dimensional wall temperature of the combustor liner[J]. Aeroengine, 1998(3): 23-27(in Chinese) [2] Strrgess G J. Prediction of adiabatic wall temperatures in film-cooling systems[J].AIAA Journal, 1966, 23(4): 13-18 [3] Pai B R, Whitelaw J. The predications of wall temperature in the presence of film cooling[J]. Heat and Mass Transfer,1971, 21(5): 23-31 [4] 韩振兴,朱谷君.气膜冷却燃烧室火焰筒二维壁温分布计算[J].航空动力学报, 1995, 10(1): 83-86 Han Zhenxing, Zhu Gujun. Calculation of 2D wall temperature distribution for film cooled flame tube of combustion chamber[J].Journal of Aerospace Power, 1995,10(1): 83-86(in Chinese) [5] 记友哲.航空发动机燃烧室数值模拟的现状与发展[J].航空发动机, 2003, 29(4): 25-29 Ji Youzhe. The status and development of the numerical simulations of an areoengine combustion chamber[J].Aeroengine,2003, 29(4): 25-29(in Chinese)
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