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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(ANNS)的燃烧化学制表:悉尼火焰LES-PDF模拟的方法和应用

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摘要

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.
机译:在这项工作中,提出了通过人工神经网络(ANN)的燃烧机制的制表方法。该方法的目的是使用通过抽象问题产生的样本训练ANN,使得它们跨越一系列燃烧问题的组成空间。在这种情况下的抽象问题是具有混合级分空间中的具有人工飞行员的层流挥发物的集合,以模拟点火,其应变速率变得良好地进入消光范围。由此覆盖的构图空间预期在非预混火焰的典型模拟中访问的区域。 ANN培训由两阶段过程组成:使用自组织地图(SOM)和通过MultiDayer Perceptron(MLP)将构图空间聚类为子域名和回归。然后采用该方法以基于GRI 1.2制表CH4 - 空燃机的机制,并通过速率控制的受限平衡(RCCE)和计算奇异扰动(CSP)降低。然后应用该机制以模拟悉尼火焰L,湍流的未预混火焰,具有显着水平的局部灭绝和重新点火。通过大涡模拟(LES)来解决流场,而运输的概率密度函数(PDF)方法用于将湍流 - 化学相互作用建模并通过随机域法以数值求解。结果表明与实验合理一致,表明SOM-MLP方法提供了组合空间的良好代表,而CPU时间的大量节省允许用综合燃烧模型进行仿真,例如LES-PDF,具有适度的CPU资源,如工作站。

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