Numerical simulation of infrared radiation characteristic of exhaust system using Tam-Ganesan turbulence model
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Numerical simulation of infrared radiation characteristic of exhaust system using Tam-Ganesan turbulence model
Vol. 27, Issue 10, (2012)
作者机构:
北京航空航天大学 能源与动力工程学院,北京,100191
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Published:2012
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LI Xi-xi, Eriqitai. Numerical simulation of infrared radiation characteristic of exhaust system using Tam-Ganesan turbulence model[J]. 2012, 27(10).
DOI:
LI Xi-xi, Eriqitai. Numerical simulation of infrared radiation characteristic of exhaust system using Tam-Ganesan turbulence model[J]. 2012, 27(10).DOI:
Numerical simulation of infrared radiation characteristic of exhaust system using Tam-Ganesan turbulence model
并考虑大气衰减作用.对比了采用标准 k - ε 模型和Tam-Ganesan模型对排气系统核心区长度的影响
以及由此引起的排气系统红外辐射特性的变化.通过与试验数据对比证明了该结果的准确性
结果表明选择合适的湍流模型对计算排气系统红外辐射特性有重要的意义.
Abstract
The infrared signature in 3~5μm band of an axisymmetric nozzle was calculated by a three-dimensional code to investigate the improvement of Tam-Ganesan turbulence model in the infrared radiation (IR) of aircraft exhaust system.The flow fields of nozzle were simulated by the finite volume method (FVM)
coupled with the standard k-ε turbulence model and Tam-Ganesan model respectively.The infrared signature of the exhaust system was calculated by FVM in non-gray absorbing-emitting media coupled with narrow band model (NBM).The final infrared signature has considered the atmosphere effect.A standard k-ε model was also investigated by being compared with the Tam-Ganesan turbulence model.The Tam-Ganesan turbulence model provided improved mean flow and infrared radiation predictions related to the standard model.It is shown the application of the optimal turbulence model is vital to the calculation of infrared radiation characteristics of exhaust system.