航空学报 > 2003, Vol. 24 Issue (6): 512-516

有限元传热分析中燃气辐射处理方法及其在飞机结构热分析中的应用

徐让书, 张宝诚, 牛玲, 富丽新   

  1. 沈阳航空工业学院动力工程系 辽宁沈阳 110034
  • 收稿日期:2002-08-17 修回日期:2003-05-12 出版日期:2003-12-25 发布日期:2003-12-25

Approach to the Radiation of Burned Gas in Finite Element Analysis of Heat Transfer and Its Application in the Analysis of Temperature of Aircraft Structure

XU Rang-shu, ZHANG Bao-cheng, NIU Ling, FU Li-xin   

  1. Department of Power Engineering; Shenyang Institute of Aeronautical Engineering; Shenyang 110034; China
  • Received:2002-08-17 Revised:2003-05-12 Online:2003-12-25 Published:2003-12-25

摘要: 研究了有限元传热分析中有吸收-发射性介质( 或称弱吸收性介质, 例如燃气) 参与辐射传热时的处理方法。通过对有、无吸收-发射性介质的封闭包壳的辐射能量交换方程的分析, 提出了用表面边界单元替代其辐射效应的准则; 研究了有吸收-发射性介质参与辐射时表面间辐射角系数计算方法及编制了相应的计算程序。最后, 对某型飞机机尾罩的温度场作了计算并对结果进行了分析。

关键词: 有限元, 传热分析, 燃气辐射, 飞机结构

Abstract: An approach to the thermal radiat ion of absor bing-emitting media, or w eak absor bing media, e. g . burnedg as, in t he finite element analysis ( FEA) of heat transfer is studied in this paper. By means of making a study of ther adiant energ y ex change equat ions of an enclosure w ith and without absorbing-emitting media, a rule of substitutingboundary elements in FEA for the absor bing-emitting media is proposed. The method used in calculating the configuration factor of r adiation between surfaces in occurr ence of absorbing-emitting media in the radiation is representedand corresponding program was developed. Finally, the temperature distribution of t he tail cover of an air craft w ascalculated and analyzed.

Key words: finite element analysis (FEA), heat transfer analysis, radiation of burned gas, aircraft structure

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