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Comparative analysis of methods for heat losses in turbulent premixed flames using physically-derived reduced-order manifolds

机译:使用物理衍生的减少歧管湍流预混火焰热损失方法的比较分析

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Heat losses have the potential to substantially modify turbulent combustion processes, especially the formation of pollutants such as nitrogen oxides. The chemistry governing these species is strongly temperature sensitive, making heat losses critical for an accurate prediction. To account for the effects of heat loss in large eddy simulation (LES) using a precomputed reduced-order manifold approach, thermochemical states must be precomputed not only for adiabatic conditions but also over a range of reduced enthalpy states. However, there are a number of methods for producing reduced enthalpy states, which invoke different implicit assumptions. In this work, a set of a priori and a posteriori LES studies have been performed for turbulent premixed flames considering heat losses within a precomputed reduced-order manifold approach to determine the sensitivity to the method by which reduced enthalpy states are generated. Two general approaches are explored for generating these reduced enthalpy states and are compared in detail to assess any effects on turbulent flame structure and emissions. In the first approach, the enthalpy is reduced at the boundary of the one-dimensional (1D) premixed flame solution, resulting in a single enthalpy deficit for a single premixed flame solution. In the second approach, a variable heat loss source term is introduced into the 1D flame solutions by mimicking a real heat loss to reduce the post-flame enthalpy. The two approaches are compared in methane-air piloted turbulent premixed planar jet flames with different diluents that maintain a constant adiabatic flame temperature but experience different radiation heat losses. Both a priori and a posteriori results, as well as a chemical pathway analysis, indicate that the manner by which the heat loss is accounted for in the manifold is of secondary importance compared to other model uncertainties such as the chemical mechanism, except in situations where heat loss is unphysically fast comp
机译:热损失具有基本上改变湍流燃烧过程的潜力,尤其是污染物如氮氧化物的形成。治疗这些物种的化学是强烈的敏感性,对准确预测的热损失是关键的。为了考虑使用预先计算的减少的歧管方法的大涡流模拟(LES)在大型涡流模拟(LES)的影响下,不仅可以预先计算绝热条件,而且必须在一系列减少的焓状态下预先计算。然而,存在许多用于产生减少的焓态的方法,该焓态调用了不同的隐式假设。在这项工作中,已经对考虑预先计算的减少的歧管方法内的热损失进行了湍流预混火焰来执行一组先验和后验,以确定生成减少焓状态的方法的敏感性。探索了两种一般方法,用于产生这些还原焓状态,并详细比较以评估对湍流火焰结构和排放的任何影响。在第一种方法中,焓在一维(1D)预混合火焰溶液的边界处减小,导致单个预混火焰溶液的单个焓缺陷。在第二种方法中,通过模仿真正的热量损失以减少火焰焓,将可变热损耗源术语引入1D火焰溶液中。在甲烷 - 空气中比较这两种方法,其具有不同的稀释剂,其保持恒定的绝热火焰温度,但经历不同的辐射热损失。先验和后验结果以及化学途径分析表明,与诸如化学机制的其他模型不确定性相比,歧管中的热量损失的算法是次要的,除了在其中的情况下热量损失是不血交的

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