Skip to main content

Research Repository

Advanced Search

Using laminate hybridisation (CFRP-GFRP) and shaped CFRP plies to increase plate post-buckling strain to failure under shear loading

Damghani, Mahdi; Wallis, Christopher; Bakunowicz, Jerzy; Murphy, Adrian

Using laminate hybridisation (CFRP-GFRP) and shaped CFRP plies to increase plate post-buckling strain to failure under shear loading Thumbnail


Authors

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

Christopher Wallis

Jerzy Bakunowicz Jerzy.Bakunowicz@uwe.ac.uk
Senior Lecturer in Aerospace Engineering

Adrian Murphy



Contributors

Abstract

Previous works have established the response and failure behaviour of hybrid (CFRP-GFRP) laminates when subjected to a wide range of destabilising loads. However, to date no works have quantified the influence of selective laminate shapes and hybridisation on plate post-buckling strain to failure. Thus, this paper investigates the plate collapse behaviour of a novel X-braced hybrid (CFRP-GFRP) twill woven laminate, subjected to in-plane shear loading. An experimental and numerical investigation is undertaken, including the consideration of a baseline pure CFRP laminate design. The experimental results illustrate that despite having less CFRP material, a hybrid laminate design with shaped CFRP plies can exhibit a greater strain to failure and buckling to failure load ratio, with only a marginally lower initial plate buckling load. Additionally, the experimental and numerical analysis reveals that the failure mechanism of the hybrid laminate is dominated by shear damage and fibre compressive breakage, whereas compressive and tensile fibre breakage dominate the conventional baseline laminate behaviour. Due to the prevalence of the shear damage and hence cracking and plastic deformation of the matrix, the novel hybrid laminate demonstrates a more gradual failure than the standard baseline laminate design, with failure strains significantly higher than that of the baseline laminate design.

Citation

Damghani, M., Wallis, C., Bakunowicz, J., & Murphy, A. (2021). Using laminate hybridisation (CFRP-GFRP) and shaped CFRP plies to increase plate post-buckling strain to failure under shear loading. Thin-Walled Structures, 162, Article 107543. https://doi.org/10.1016/j.tws.2021.107543

Journal Article Type Article
Acceptance Date Feb 3, 2021
Online Publication Date Feb 23, 2021
Publication Date May 1, 2021
Deposit Date Feb 11, 2021
Publicly Available Date Feb 24, 2022
Journal Thin-Walled Structures
Print ISSN 0263-8231
Publisher Elsevier
Peer Reviewed Peer Reviewed
Volume 162
Article Number 107543
DOI https://doi.org/10.1016/j.tws.2021.107543
Keywords shear buckling; Laminated Composites; hybrid composites; post-buckling behaviour; Nonlinear behaviour; failure criterion
Public URL https://uwe-repository.worktribe.com/output/7081799

Files







You might also like



Downloadable Citations