用深度学习模型实时预测复合材料变形时的应力与损伤演化。
Predicting Stress and Damage in Carbon Fiber-Reinforced Composites Deformation Process using Composite U-Net Surrogate Model
- 基于U-Net架构构建自回归模型,融合宏微观特征捕捉变形全过程。
- 相比IGFEM模拟,预测速度提升60倍以上,精度高且可追踪裂纹萌生与扩展。
- 适合需要快速仿真复合材料性能的航空航天等工程领域研究者。
碳纤维增强复合材料(CFRC)因其优异的力学性能,在航空航天等高端工程中至关重要。准确理解其在载荷下的行为对优化性能至关重要。传统有限元方法(如界面增强广义FEM,IGFEM)虽能提供有效洞见,但计算效率较低。现有数据驱动代理模型可预测损伤传播或应力-应变行为,但难以全面刻画从裂纹萌生到扩展的完整变形过程中的应力与损伤演化。本研究提出一种新型自回归复合U-Net深度学习模型,可同步预测CFRC变形过程中的应力场与损伤场。该模型利用U-Net结构捕获空间特征,并整合宏观与微观现象,克服了先前方法的关键局限。在单向拉伸条件下,模型能高精度预测微结构内应力与损伤分布演化,相比IGFEM计算速度提升超过60倍。
原文摘要 · Abstract (English)
Carbon fiber-reinforced composites (CFRC) are pivotal in advanced engineering applications due to their exceptional mechanical properties. A deep understanding of CFRC behavior under mechanical loading is essential for optimizing performance in demanding applications such as aerospace structures. While traditional Finite Element Method (FEM) simulations, including advanced techniques like Interface-enriched Generalized FEM (IGFEM), offer valuable insights, they can struggle with computational efficiency. Existing data-driven surrogate models partially address these challenges by predicting propagated damage or stress-strain behavior but fail to comprehensively capture the evolution of stress and damage throughout the entire deformation history, including crack initiation and propagation. This study proposes a novel auto-regressive composite U-Net deep learning model to simultaneously predict stress and damage fields during CFRC deformation. By leveraging the U-Net architecture's ability to capture spatial features and integrate macro- and micro-scale phenomena, the proposed model overcomes key limitations of prior approaches. The model achieves high accuracy in predicting evolution of stress and damage distribution within the microstructure of a CFRC under unidirectional strain, offering a speed-up of over 60 times compared to IGFEM.
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