基于深度学习的复合材料微结构-性能的构效关系研究OA
Deep Learning-based Method for Quantitatively Analyzing the Microstructure-property Linkage of Composite Laminates
复合材料的"材料-结构一体化"特点导致细观尺度下的微观结构具有较大的不确定性,无法保证复合材料在航空航天等高安全标准结构上的应用.基于材料信息学方法,本文开发了一种数据驱动的预测模型,旨在预测复合材料细观结构的随机因素对其横向力学性能的影响.首先,在给定的排布空间域内以及给定的纤维体积分数条件下,使用基于分子动力学的随机碰撞算法生成单向碳纤维复合材料的微观结构,并通过基于细观力学的有限元方法计算了相应的弹性模量和剪切模量.然后,利用两点空间相关函数和主成分分析确定微结构的降阶数据表示.最后,基于微结构数字化表达和相应横向力学性能对应的数据库,实现了用机器学习模型得到微结构与横向弹性性能之间潜在的非线性关系,从而可以通过复合材料的微结构快速预测其横向力学性能.通过对微结构数字化表达的特征分析,在纤维体积分数一定的情况下,纤维平均间距是对复合材料力学性能影响较大的定量化微结构特征,对于正向预测复合材料结构的性能和反向的优化设计具有重要意义.
The"material-structure integration"characteristic of composites results in significant uncertainty in their microstructure,posing challenges for their reliable application in high-safety-standard structures such as those in aerospace engineering.Based on material informatics approach,this paper develops a data-driven predictive model.To this end,the microstructure of unidirectional carbon fiber composites is generated using a random collision algorithm,and the corresponding elastic and shear moduli were calculated by the FEM of micromechanics.Then,a reduced-order data representation of the microstructure was determined using two-point spatial correlation functions and principal component analysis.Finally,based on the database of the digital expression of the microstructure and the corresponding transverse mechanical properties,the machine learning model is used to capture the potential nonlinear relationship between the microstructure and the transverse elastic properties,so that the transverse mechanical properties of composites can be quickly predicted through the microstructure.Furthermore,through the characteristic analysis on the digital expression of the microstructure,the quantitative microstructural characteristics that have a great impact on the mechanical properties of composites were obtained.Analysis of digital microstructural representations reveals that,given a fixed fiber volume fraction,the average fiber spacing is a critical quantitative feature affecting the mechanical behavior of composites.It is of great significance for both forward performance prediction and inverse design optimization.
王美蛟;邱诚
中国科学院力学研究所流固耦合系统力学重点实验室,北京 100190||中国科学院大学,北京 100049中国科学院力学研究所流固耦合系统力学重点实验室,北京 100190
航空航天
复合材料细观力学周期性边界条件两点相关函数深度学习
composite laminatesmicromechanicsperiodic boundary conditiontwo-point correlation functiondeep learning
《航空科学技术》 2026 (2)
18-26,9
航空科学基金(2022Z055032001) Aeronautical Science Foundation of China(2022Z055032001)
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