利用基于机器学习的算法加强有限元分析的风洞计算模拟

Luttfi A. Al-Haddad, Alaa Jaber, Latif Ibraheem, Sinan Al-Haddad, Naseem Ibrahim, Fawaz Abdulwahed
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引用次数: 0

摘要

风洞对于检查飞机模型空气动力学、精确模拟真实世界条件以及加强设计和性能评估至关重要。本研究介绍了一种新技术,用于提高风洞模拟中应力分布预测的时间和准确性。该方法将有限元分析(FEA)与两种回归模型相结合:支持向量机 (SVM) 和 k - 最近邻 (kNN)。研究首先对 ANSYS 流体数据进行全面分析,揭示风洞内错综复杂的流体动力学细节。应力预测的比较分析,辅以均方根误差 (RMSE) 指标,证明了所提出方法的可行性。基于 SVM 的模型的 RMSE 为 2.1%,超过了 kNN 模型 5.6% 的 RMSE,证明了该模型的高准确性。值得注意的是,应力分布计算在 ANSYS 中需要近 2 个小时,相比之下,在 SVM 中只需要 10 秒,在 kNN 中只需要 3 秒。此外,SVM 和 kNN 模型的计算效率也得到了强调,突出了它们在应力分析中的灵活性。这种综合方法为工程模拟带来了巨大的潜力,可产生精确的应力分布预测,有望推动飞机设计方法和风洞评估的发展。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Enhancing Wind Tunnel Computational Simulations of Finite Element Analysis Using Machine Learning-Based Algorithms
Wind tunnels are essential for examining aircraft model aerodynamics, accurately simulating real-world conditions, and enhancing design and performance evaluations. This study introduces a novel technique to improve the time and accuracy of stress distribution forecasts in wind tunnel simulations. This method combines Finite Element Analysis (FEA) with two regression models: Support Vector Machine (SVM) and k - Nearest Neighbors (kNN). T he investigation begins with a thorough analysis of ANSYS fluent flow data, which reveals intricate fluid dynamics details within the wind tunnel. A comparative analysis of stress projections, supplemented by Root Mean Square Error (RMSE) metric, demonstrates the proposed methodology’s viability. High accuracy is noted in the SVM-based model, as evidenced by its 2.1% RMSE, which surpasses the kNN model's 5.6% RMSE. Notably, the stress distribution calculation took almost 2 hours in ANSYS.In contrast, it required only 10 seconds in SVM and 3 seconds in kNN, showcasing the time-efficient attributes of these models where they solely depend on the trained data. Moreover, the computational efficacy of the SVM and kNN models is highlighted, emphasizing their flexibility in stress analysis. This integrative approach introduces a promising potential in engineering simulations, yielding precise stress distribution forecasts that have the potential to advance aircraft design methodologies and wind tunnel evaluations.
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