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Comparative Analysis of Methods for Heat Losses in Physically-Derived Reduced-Order Manifolds

机译:物理衍生数歧管中热损失方法的比较分析

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Heat loss substantially modifies turbulent combustion processes, especially the formation of pollutants such as nitrogen oxides, which are strongly temperature sensitive. To account for the effects of heat loss in Large Eddy Simulation (LES) using a reduced-order manifold approach, thermochemical states are computed via a priori 1-D premixed flame calculations over a range of reduced enthalpy states. Two basic approaches are explored for generating these reduced enthalpy states, which are compared to assess any effects on turbulent flame structure and emissions. In the first approach, a variable heat loss source term is introduced into the 1-D flame solutions by mimicking a real heat loss to reduce the post-flame enthalpy. In the second approach, fuel and oxidizer are converted to products in the unburned gases at a constant temperature to produce reduced enthalpy in the entire 1-D flame solution. The two approaches are compared in methane-air piloted turbulent premixed planar jet flames that maintain a constant adiabatic flame temperature but experience differing radiation heat losses. The results indicate that the manner in which the heat loss is accounted for in the manifold is of secondary importance compared to other model uncertainties such as the chemical mechanism.
机译:热损失基本上改变湍流燃烧过程,尤其是污染物如氮氧化物的形成,这是强烈的敏感性。为了考虑使用阶数歧管方法的大涡模拟(LES)在大涡流模拟(LES)的影响下,通过先验的1-D预混火焰计算来计算热化学状态在一系列减少的焓状态。探索了两种基本方法,用于产生这些减少的焓状态,以评估对湍流火焰结构和排放的任何影响。在第一方法中,通过模拟真正的热量损失以减少火焰焓,将可变热损失源术语引入1-D火焰溶液中。在第二种方法中,燃料和氧化剂在恒定温度下在未燃烧的气体中转化为产物,以在整个1-D火焰溶液中产生降低的焓。两种方法在甲烷 - 空中比较的湍流湍流预混合平面喷射火焰中,保持恒定的绝热火焰温度,但经历不同的辐射热损失。结果表明,与其他模型不确定性(如化学机制)相比,歧管中占歧管的热量损失的方式是次要的。

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