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A machine learning enhanced characteristic length method for failure prediction of open hole tension composites

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Title: A machine learning enhanced characteristic length method for failure prediction of open hole tension composites
Authors: Imran Azeem, OA
Pinho, S
Item Type: Journal Article
Abstract: The characteristic length method is a non-local approach to predicting the failure of open and closed-hole composite features. This method requires the determination of the linear elastic stress field of the composite laminate at its failure load. Typically, this requires computationally expensive progressive damage and linear elastic modelling and simulation with finite element analysis (FEA). In this study, we demonstrate the benefit of machine learning methods to efficiently and accurately predict characteristic lengths of composite laminates with open holes. We find that the prediction of the load-displacement profile usefully informs ultimate failure load prediction. We also find that linear elastic stress fields are more accurately predicted using a long-short term memory neural network rather than a convolutional decoder neural network. We show indirect prediction of characteristic length, via prediction of failure loads and linear elastic stress fields independently, results in more flexible, interpretable and accurate results than direct prediction of characteristic length, given sufficient training data. Our machine learning-assisted characteristic length method shows over five orders of magnitude of time-saving benefit compared to FEA-based methods.
Issue Date: Oct-2024
Date of Acceptance: 5-Oct-2024
URI: http://hdl.handle.net/10044/1/115028
DOI: 10.1016/j.jcomc.2024.100524
ISSN: 2666-6820
Publisher: Elsevier
Journal / Book Title: Composites Part C: Open Access
Volume: 15
Copyright Statement: © 2024 The Author(s). Published by Elsevier B.V. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).
Publication Status: Published
Article Number: 100524
Online Publication Date: 2024-10-10
Appears in Collections:Aeronautics
Faculty of Engineering



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