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A Thickened Stochastic Fields Approach for Turbulent Combustion Simulation

机译:湍流燃烧模拟的加厚随机场方法

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摘要

The Stochastic Fields approach is an effective way to implement transported Probability Density Function modelling into Large Eddy Simulation of turbulent combustion. In premixed turbulent combustion however, thin flame-like structures arise in the solution of the Stochastic Fields equations that require grid spacing much finer than the filter scale used for the Large Eddy Simulation. The conventional approach of using grid spacing equal to the filter scale yields substantial numerical error, whereas using grid spacing much finer than the filter length scale is computationally-unaffordable for most industrially-relevant combustion systems. A Thickened Stochastic Fields approach is developed in this study in order to provide physically-accurate and numerically-converged solutions of the Stochastic Fields equations with reduced compute time. The Thickened Stochastic Fields formulation bridges between the conventional Stochastic Fields and conventional Thickened-Flame approaches depending on the numerical grid spacing utilised. One-dimensional Stochastic Fields simulations of freely-propagating turbulent premixed flames are used in order to obtain criteria for the thickening factor required, as a function of relevant physical and numerical parameters, and to obtain a model for an efficiency function that accounts for the loss of resolved flame surface area caused by applying the thickening transformation to the Stochastic Fields equations. The Thickened Stochastic Fields formulation is tested by performing LES of a laboratory premixed Bunsen flame. The results demonstrate that the Thickened Stochastic Fields method produces accurate predictions even when using a grid spacing equal to the filter scale. The present development therefore facilitates the accurate application of the Stochastic Fields approach to industrially-relevant combustion systems.
机译:随机场方法是将运输的概率密度函数模型实施到湍流燃烧的大涡模拟中的有效方法。但是,在预混湍流燃烧中,在随机场方程的解中出现了类似火焰的薄结构,该方程组要求的网格间距比大涡流仿真所使用的过滤尺度更精细。使用等于过滤器刻度的栅格间距的常规方法会产生较大的数值误差,而对于大多数与工业相关的燃烧系统,使用比过滤器长度刻度更细的栅格间距在计算上是无法承受的。本研究中开发了一种加厚的随机场方法,目的是在减少计算时间的情况下提供随机场方程的物理精确和数值收敛解。根据所使用的数值网格间距,加厚随机场公式在传统随机场和常规加厚火焰方法之间架起了桥梁。使用自由传播的湍流预混火焰的一维随机场模拟,以获取所需的增稠因子标准(作为相关物理和数值参数的函数),并获得用于计算损失的效率函数的模型对随机场方程应用增稠变换导致的分解火焰表面积的变化。通过执行实验室预混本生火焰的LES测试增稠的随机场配方。结果表明,即使使用等于过滤器刻度的网格间距,“加厚随机场”方法也可以产生准确的预测。因此,当前的发展有助于将随机场方法准确地应用于与工业相关的燃烧系统。

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