论文标题
应用物理信息增强的超分辨率生成对抗网络以有限速率 - 化学流量并预测瘦的预混合燃气轮机燃烧器
Applying Physics-Informed Enhanced Super-Resolution Generative Adversarial Networks to Finite-Rate-Chemistry Flows and Predicting Lean Premixed Gas Turbine Combustors
论文作者
论文摘要
在解决不足的流中,准确预测小尺度仍然是复杂配置预测模拟的主要挑战之一。在过去的几年中,数据驱动的建模在许多领域都变得很流行,因为现在可以使用大型,广泛标记的数据集,并且在图形处理单元(GPU)上,对大型神经网络的培训变得可能会大大加快学习过程。实际上,在流体动力学(例如解决不足的反应流动)中成功应用深度神经网络仍然具有挑战性。这项工作将最近引入的Piesrgan推进了反应性有限速率化学化学流。但是,由于燃烧化学通常作用于最小的尺度,因此需要扩展原始方法。因此,对Piesrgan的建模方法进行了修改,以准确地说明层流有限速率化学流动的挑战。基于Piesrgan的修改模型在先验的层次倾斜预燃烧设置中提供了良好的一致性和后验测试。此外,提出了一个减少的基于Piesrgan的模型,该模型仅解决重建场上的主要物种,并使用Piersgan查找其余物种,并利用及时的及时使用。显示了歧视者支持的训练的优势,并在模型燃气轮机燃烧器的背景下展示了新模型的可用性。
The accurate prediction of small scales in underresolved flows is still one of the main challenges in predictive simulations of complex configurations. Over the last few years, data-driven modeling has become popular in many fields as large, often extensively labeled datasets are now available and training of large neural networks has become possible on graphics processing units (GPUs) that speed up the learning process tremendously. In fact, the successful application of deep neural networks in fluid dynamics, such as for underresolved reactive flows, is still challenging. This work advances the recently introduced PIESRGAN to reactive finite-rate-chemistry flows. However, since combustion chemistry typically acts on the smallest scales, the original approach needs to be extended. Therefore, the modeling approach of PIESRGAN is modified to accurately account for the challenges in the context of laminar finite-rate-chemistry flows. The modified PIESRGAN-based model gives good agreement in a priori and a posteriori tests in a laminar lean premixed combustion setup. Furthermore, a reduced PIESRGAN-based model is presented that solves only the major species on a reconstructed field and employs PIERSGAN lookup for the remaining species, utilizing staggering in time. The advantages of the discriminator-supported training are shown, and the usability of the new model demonstrated in the context of a model gas turbine combustor.