Swirling flow field reconstruction and cooling performance analysis based on experimental observations using physics-informed neural networks

IF 1.1 Q4 ENGINEERING, MECHANICAL Journal of the Global Power and Propulsion Society Pub Date : 2024-05-08 DOI:10.33737/jgpps/185745
Weichen Huang, Xu Zhang, Hongyi Shao, Wenbin Chen, Yihong He, Wenwu Zhou, Yingzheng Liu
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Abstract

The design of thermal protection modules (such as film cooling) for combustion chambers requires a high-fidelity swirling flow field. Although numerical methods provide insights into three-dimensional mechanisms of swirling flow, their predictions of key features such as recirculation zones and swirling jets are often unsatisfactory due to inherent anisotropy and the isotropic nature of the Boussinesq hypothesis. Experimental methods, such as hot wire, laser Doppler velocimetry, and planar particle image velocimetry (PIV), offer more accurate reference data but are limited by sparse or planar observations. In this study, considering the outperformed capability of solving inverse problems, physics-informed neural network (PINN) was adopted to reconstruct the mean swirling flow field based on limited experimental observations from two-dimensional and two-component (2D2C) results. It was found that adding partial information characterizing the swirling flow, such as the swirling jet, could significantly improve the reconstruction of flow field. In addition, film cooling effectiveness was the key variable to evaluate the film cooling performance, which was relatively measurable in the scalar field. To further improve the accuracy of the reconstruction, the multi-source strategy was adopted into the neural network, where the film cooling effectiveness (FCE) of the effusion plate was imported as the scalar source. It was found that the prediction of the flow field near the target plate was improved, where the highest error reduction could reach 76.5%. Finally, through the reconstructed three-dimensional vortex distribution, it was found that swirling flow vortex structures near the swirler exit had a significant impact on cooling effectiveness, causing a non-uniform cooling distribution. This study aims to diagnose the three-dimensional swirling flow field with deep learning by leveraging limited experimental data and deepen the understanding of effusion cooling under swirling flow condition so that obtains a more accurate reference in the design of thermal protection modules.
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利用物理信息神经网络根据实验观测结果重建漩涡流场并分析冷却性能
燃烧室热保护模块(如薄膜冷却)的设计需要高保真的漩涡流场。虽然数值方法可以深入了解漩涡流的三维机制,但由于固有的各向异性和布森斯克假设的各向同性,它们对再循环区和漩涡射流等关键特征的预测往往不能令人满意。热丝、激光多普勒测速仪和平面粒子图像测速仪(PIV)等实验方法可提供更精确的参考数据,但受到观测数据稀少或平面观测的限制。在本研究中,考虑到物理信息神经网络(PINN)在解决逆问题方面的优越性能,采用物理信息神经网络(PINN)根据有限的二维和双分量(2D2C)实验观测结果重建平均漩涡流场。研究发现,添加漩涡射流等表征漩涡流的部分信息可显著改善流场重建效果。此外,薄膜冷却效果是评价薄膜冷却性能的关键变量,这在标量场中是相对可测量的。为了进一步提高重建的准确性,神经网络采用了多源策略,其中导入了流出板的薄膜冷却效果(FCE)作为标量源。结果发现,对目标板附近流场的预测得到了改善,其中误差降低率最高可达 76.5%。最后,通过重建的三维漩涡分布发现,漩涡出口附近的漩涡结构对冷却效果有显著影响,导致冷却分布不均匀。本研究旨在利用有限的实验数据,通过深度学习诊断三维漩涡流场,加深对漩涡流条件下喷流冷却的理解,从而为热保护模块的设计提供更准确的参考。
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来源期刊
Journal of the Global Power and Propulsion Society
Journal of the Global Power and Propulsion Society Engineering-Industrial and Manufacturing Engineering
CiteScore
2.10
自引率
0.00%
发文量
21
审稿时长
8 weeks
期刊最新文献
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