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A physics-informed machine learning model for global-local stress prediction of open holes with finite-width effects in composite structures

Title: A physics-informed machine learning model for global-local stress prediction of open holes with finite-width effects in composite structures
Authors: Imran Azeem, OA
Pinho, S
Item Type: Journal Article
Abstract: Fast and accurate methods are required to predict stresses in the vicinity of open and closed holes in composite structures, especially in a global-local modelling context as applied during the design of airframe structures. Fast analytical solutions for infinite-width anisotropic plates with open holes do not consider finite-width effects. Heuristic methods and semi-analytical solutions can be used to towards addressing such effects. To improve the accuracy and speed of these respective methods, we use machine learning (ML) methods trained on high-fidelity finite element analyses (FEA) to make finite-width corrections. However, such methods require large amounts of training data to reduce errors to satisfactory levels. Therefore, in this study, the fusion of analytical solutions with machine learning is performed. We develop an analytical solution-informed ML model that is as fast as an analytical solution and superior in accuracy to analytical solutions with heuristic finite-width scaling. Our informed ML model offers accuracies equal to analytical solutions for the infinite-width case, and it is capable for use in a global-local modelling context, under uniaxial and biaxial loading. Our informed ML model outperforms prediction accuracy across all cases compared to uninformed ML models and requires a significantly lower size training dataset size.
Issue Date: Sep-2024
Date of Acceptance: 16-Aug-2024
URI: http://hdl.handle.net/10044/1/114002
DOI: 10.1177/00219983241281073
ISSN: 0021-9983
Publisher: SAGE Publications
Start Page: 2501
End Page: 2514
Journal / Book Title: Journal of Composite Materials
Volume: 58
Issue: 23
Copyright Statement: © The Author(s) 2024. This article is distributed under the terms of the Creative Commons Attribution 4.0 License (https://creativecommons.org/licenses/by/4.0/) which permits any use, reproduction and distribution of the work without further permission provided the original work is attributed as specified on the SAGE and Open Access page (https://us.sagepub.com/en-us/nam/open-access-at-sage).
Publication Status: Published
Online Publication Date: 2024-09-03
Appears in Collections:Aeronautics
Faculty of Engineering



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