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Tabulation of combustion chemistry via Artificial Neural Networks (ANNs): Methodology and application to LES-PDF simulation of Sydney flame L

机译:通过人工神经网络(ANN)进行燃烧化学制表:方法论及其在悉尼火焰L的LES-PDF模拟中的应用

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In this work, a methodology for the tabulation of combustion mechanisms via Artificial Neural Networks (ANNs) is presented. The objective of the methodology is to train the ANN using samples generated via an abstract problem, such that they span the composition space of a family of combustion problems. The abstract problem in this case is an ensemble of laminar flamelets with an artificial pilot in mixture fraction space to emulate ignition, of varying strain rate up to well into the extinction range. The composition space thus covered anticipates the regions visited in a typical simulation of a non-premixed flame. The ANN training consists of two-stage process: clustering of the composition space into subdomains using the Self-Organising Map (SOM) and regression within each subdomain via the multilayer Perceptron (MLP). The approach is then employed to tabulate a mechanism of CH4-air combustion, based on GRI 1.2 and reduced via Rate-Controlled Constrained Equilibrium (RCCE) and Computational Singular Perturbation (CSP). The mechanism is then applied to simulate the Sydney flame L, a turbulent non-premixed flame that features significant levels of local extinction and re-ignition. The flow field is resolved through Large Eddy Simulation (LES), while the transported probability density function (PDF) approach is employed for modelling the turbulence-chemistry interaction and solved numerically via the stochastic fields method. Results demonstrate reasonable agreement with experiments, indicating that the SOM-MLP approach provides a good representation of the composition space, while the great savings in CPU time allow for a simulation to be performed with a comprehensive combustion model, such as the LES-PDF, with modest CPU resources such as a workstation. (C) 2017 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:在这项工作中,提出了一种通过人工神经网络(ANN)编制燃烧机制表的方法。该方法的目标是使用通过抽象问题生成的样本来训练ANN,以使它们跨越一系列燃烧问题的组成空间。这种情况下的抽象问题是层流小火焰的集合,在混合物分数空间中有一个人工引燃器来模拟着火,其应变率一直变化到熄灭范围。这样覆盖的成分空间可以在非预混火焰的典型模拟中预测访问的区域。 ANN训练包括两个阶段的过程:使用自组织映射(SOM)将合成空间聚类为子域,并通过多层感知器(MLP)在每个子域内进行回归。然后,该方法基于GRI 1.2并通过速率控制约束平衡(RCCE)和计算奇异摄动(CSP)来简化CH4-空气燃烧的机制。然后将该机制应用于模拟悉尼火焰L,这是一种湍流的非预混火焰,具有明显的局部熄灭和重燃特性。流场通过大涡模拟(LES)求解,而运移概率密度函数(PDF)方法用于湍流-化学相互作用的建模,并通过随机场方法进行数值求解。结果表明与实验具有合理的一致性,表明SOM-MLP方法可以很好地表示成分空间,而CPU时间的大量节省使您可以使用综合燃烧模型(例如LES-PDF,具有适度的CPU资源(例如工作站)。 (C)2017燃烧研究所。由Elsevier Inc.出版。保留所有权利。

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