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用温度修正的k-ε模型研究排气系统红外辐射特性

李喜喜 额日其太 朱希娟 吴盟

李喜喜, 额日其太, 朱希娟, 吴盟. 用温度修正的k-ε模型研究排气系统红外辐射特性[J]. 航空动力学报, 2013, 28(9): 1942-1948.
引用本文: 李喜喜, 额日其太, 朱希娟, 吴盟. 用温度修正的k-ε模型研究排气系统红外辐射特性[J]. 航空动力学报, 2013, 28(9): 1942-1948.
LI Xi-xi, Eriqitai, ZHU Xi-juan, WU Meng. Infrared radiation characteristics of exhaust system using temperature corrected k-ε model[J]. Journal of Aerospace Power, 2013, 28(9): 1942-1948.
Citation: LI Xi-xi, Eriqitai, ZHU Xi-juan, WU Meng. Infrared radiation characteristics of exhaust system using temperature corrected k-ε model[J]. Journal of Aerospace Power, 2013, 28(9): 1942-1948.

用温度修正的k-ε模型研究排气系统红外辐射特性

Infrared radiation characteristics of exhaust system using temperature corrected k-ε model

  • 摘要: 为研究温度修正的k-ε湍流模型对排气系统红外辐射特性计算精度的改善程度,计算了某轴对称收敛喷管在3~5μm波段的空腔-喷流组合红外辐射特性,并与试验结果对比.喷管流场及温度场采用有限体积法(FVM)求解Navier-Stokes(N-S)方程得到,湍流模型分别采用标准k-ε模型和温度修正的k-ε模型.红外辐射特性的计算采用有限体积法求解吸收-发射性介质条件下的三维辐射传输方程,并考虑大气衰减作用.计算结果表明:温度修正的k-ε模型可有效预测排气系统热喷流的核心区长度,从而获得与试验结果一致的红外辐射强度.与标准k-ε模型相比,采用温度修正的k-ε模型计算得到的红外辐射强度的最大相对误差由64%降至了4.3%,说明温度修正的k-ε模型适用于精确模拟排气系统的红外辐射特性.

     

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出版历程
  • 收稿日期:  2012-08-07
  • 刊出日期:  2013-09-28

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