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Large eddy simulation of a turbulent non-premixed flame based on the flamelet-generated manifolds approach and a reduced mechanism verification

机译:基于轰炸机生成的歧管方法的湍流非预混火焰的大型涡流模拟及减少机制验证

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This work presents the design of a large eddy simulation based on the flamelet-generated manifolds (FGM) approach to evaluate a Sandia Flame D, which is a turbulent non-premixed piloted jet flame. The detailed kinetic mechanism of the Gas Research Institute (GRI3.0, which contains 53 species and 325 elementary reactions), as well as a reduced mechanism, are employed to describe combustion. This reduced mechanism, containing 19 species and 68 elementary reactions, is proposed based on the direct relation graphs with error-propagation (DRGEP) method and a species sensitivity analysis from the GRI3.0. Both the two mechanisms are introduced into Fluent to simulate a Sandia Flame D, and the numerical results are in good agreement with the experimental data, which indicates the accurate predictive capability of the LES/FGM method in combustion modeling and that the proposed reduced mechanism can be applied to the numerical simulation in practical engineering problems. (C) 2020 Elsevier Masson SAS. All rights reserved.
机译:这项工作介绍了基于Flamelet生成的歧管(FGM)方法的大型涡流模拟的设计,以评估桑迪亚火焰D,这是一种湍流的非预混射流火焰。气体研究所的详细动力学机制(GRI3.0含有53种和325个基本反应),以及减少的机制来描述燃烧。基于具有误差传播(DRGEP)方法的直接关系图和来自GRI3.0的物种敏感性分析,提出了含有19种和68个基本反应的这种减少的机理。两种机制都是流利的,以模拟桑迪亚火焰D,数值结果与实验数据很好,这表明了LES / FGM方法在燃烧建模中的准确预测能力,并且所提出的减少机制可以应用于实用工程问题的数值模拟。 (c)2020 Elsevier Masson SAS。版权所有。

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