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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

Numerical shape, thickness and stacking sequence optimisation and experimental study of hybrid composite plates under in-plane shear loading Thumbnail


Authors

Mahdi Damghani Mahdi.Damghani@uwe.ac.uk
Senior Lecturer in Aerostructures

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.

Citation

Damghani, M., Matthews, J., Murphy, A., & Featherston, C. (2023). Numerical shape, thickness and stacking sequence optimisation and experimental study of hybrid composite plates under in-plane shear loading. Structures, 51, 372-390. https://doi.org/10.1016/j.istruc.2023.03.066

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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