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首页> 外文期刊>Acta astronautica >Modifying the constant coefficients of Eddy-dissipation concept model in moderate or intense low-oxygen dilution combustion using inverse problem methodology
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Modifying the constant coefficients of Eddy-dissipation concept model in moderate or intense low-oxygen dilution combustion using inverse problem methodology

机译:使用逆问题方法修改中等或强烈低氧稀释燃烧中的涡耗概念模型的常数系数

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There are many differences between combustion modeling of conventional and moderate or intense low oxygen dilution combustion. Among them, turbulent-chemistry interaction modeling is an open field of study. Studies show that the eddy dissipation concept model is very suitable for modeling of moderate or intense low-oxygen dilution combustion but the constants of eddy dissipation concept should be modified for better prediction.In this work, the inverse problem methodology is applied to predict the optimum volume fraction and time scale constants of eddy dissipation concept in order to enhance the accuracy of the numerical prediction of moderate or intense low-oxygen dilution combustion in a jet-in-hot-coflow burner. For this purpose, computational fluid dynamics modeling approach, considering Reynolds-averaged Navier-Stokes equations and detailed reaction mechanism, is used in the openfoam package. The results show that the values of 0.48 and 1.9 are suitable for time scale and volume fraction constants, respectively, as the values leading to the highest results in comparison to experimental data. After validating the numerical results, the effect of sinusoidal variations in the preheated co-flow temperature on the flame characteristics of Methane-Hydrogen blended fuel, to produce more complete moderate or intense low-oxygen dilution combustion regime, was considered. The results show that in moderate or intense low-oxygen dilution combustion regime, the peak temperature under sinusoidal variations in the preheated co-flow temperature is constant as compared to typically moderate or intense low-oxygen dilution combustion; but the amount of CO2 and H2O species, as well as OH and CH2O intermediate species, are increased and CO emission is reduced.
机译:常规燃烧模型与中等或强烈的低氧稀释燃烧模型之间存在许多差异。其中,湍流化学相互作用建模是一个开放的研究领域。研究表明,涡耗散概念模型非常适合于中度或强烈的低氧稀释燃烧的建模,但应修改涡流散逸概念的常数以更好地进行预测。在这项工作中,采用反问题方法来预测最优涡流消散概念的体积分数和时间尺度常数,以提高在热气流射流燃烧器中中等或强烈的低氧稀释燃烧数值预测的准确性。为此,在openfoam软件包中使用考虑了雷诺平均Navier-Stokes方程和详细反应机理的计算流体动力学建模方法。结果表明,0.48和1.9的值分别适合于时间标度和体积分数常数,因为与实验数据相比,该值导致最高的结果。在验证了数值结果之后,考虑了预热共流温度的正弦变化对甲烷-氢混合燃料的火焰特性的影响,以产生更完全的中度或强烈的低氧稀释燃烧方案。结果表明,在中等或强烈的低氧稀释燃烧状态下,与典型的中等或强烈的低氧稀释燃烧相比,在预热同流温度正弦变化下的峰值温度是恒定的。但是增加了CO2和H2O种类以及OH和CH2O中间种类的数量,减少了CO的排放。

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