Mahdi Damghani Mahdi.Damghani@uwe.ac.uk
Senior Lecturer in Aerostructures
Numerical shape, thickness and stacking sequence optimisation and experimental study of hybrid composite plates under in-plane shear loading
Damghani, Mahdi; Matthews, Jason; Murphy, Adrian; Featherston, Carol
Authors
Dr Jason Matthews Jason.Matthews@uwe.ac.uk
Senior Lecturer in Automotive Manufacturing
Adrian Murphy
Carol Featherston
Abstract
Shape, thickness and stacking sequence optimisation of a damage tolerant hybrid (GFRP-CFRP) composite laminate is performed using the commercial Optistruct solver. The results of the optimisation study are compared to both a benchmark non-damage tolerant CFRP laminate (without protective surface GFRP plies known as type 1 laminate) and a damage tolerant traditionally optimised hybrid CFRP-GFRP laminate (having X shape CFRP plies known as type 2 laminate), designed and tested in a previous study. The optimised laminate is manufactured using three different manufacturing techniques. The experimental buckling and post-buckling performance of the manufactured laminates are investigated. The optimised hybrid laminate is approximately 8% heavier than the type 1 but 17% lighter than type 2, but with the benefit of protective surface GFRP plies in favour of a damage tolerant design as shown in a previous study. Both numerical and experimental buckling and post-buckling performance studies show that the optimised laminates demonstrate higher pre-buckling stiffness compared to the type 1 design. However, the experimental buckling and failure/collapse loads, unlike the numerically predicted loads, are 24.31% and 26.70% lower, respectively. This is due to the significant number of ply drop-offs in the hybrid laminate design, and hence geometric imperfections and stress concentration effects at these locations leading to early buckling and failure in the post-buckling region.
Journal Article Type | Article |
---|---|
Acceptance Date | Mar 13, 2023 |
Online Publication Date | Mar 20, 2023 |
Publication Date | May 1, 2023 |
Deposit Date | Mar 15, 2023 |
Publicly Available Date | Mar 22, 2023 |
Journal | Structures |
Electronic ISSN | 2352-0124 |
Publisher | Elsevier |
Peer Reviewed | Peer Reviewed |
Volume | 51 |
Pages | 372-390 |
DOI | https://doi.org/10.1016/j.istruc.2023.03.066 |
Keywords | Free size optimisation; hybrid composites; Buckling; Post-buckling; shear loading |
Public URL | https://uwe-repository.worktribe.com/output/10553082 |
Publisher URL | https://www.sciencedirect.com/science/article/pii/S2352012423003521 |
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Numerical shape, thickness and stacking sequence optimisation and experimental study of hybrid composite plates under in-plane shear loading
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Licence
http://creativecommons.org/licenses/by/4.0/
Publisher Licence URL
http://creativecommons.org/licenses/by/4.0/
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