A plate model for compressive strength prediction of delaminated composites

Journal article


Choudhry, Rizwan Saeed, Rhead, Andrew T., Nielsen, Mark W.D. and Butler, Richard 2018. A plate model for compressive strength prediction of delaminated composites. Composite Structures. https://doi.org/10.1016/j.compstruct.2018.11.066
AuthorsChoudhry, Rizwan Saeed, Rhead, Andrew T., Nielsen, Mark W.D. and Butler, Richard
Abstract

Damage tolerance is of critical importance to laminated composite structures. In this paper, we present a new semi-analytical method for predicting the strain at which delamination propagation will initiate following sublaminate buckling. The method uses a numerical strip model to determine the thin-film buckling strain of an anisotropic sub-laminate created by delamination, before evaluating the strain energy release rate for delamination propagation. The formulation assumes that all energy is available for propagation in a peeling mode (Mode I); avoiding an approximate mixed-mode criterion. Results are compared with twelve experimentally obtained propagations strains, covering a variety of laminates each containing a circular PTFE delamination. Comparison shows agreement to within 12% for balanced sublaminate tests in which delamination propagation occurred before intra-ply cracking. The method can be used to significantly improve the damage tolerance of laminates, opening up new opportunities for structural efficiency using elastic tailoring, non-standard ply angles and material optimisation.

KeywordsDamage tolerance; Delamination; CAI; Modelling; Impact; Buckling
Year2018
JournalComposite Structures
PublisherElsevier
ISSN0263-8223
1879-1085
Digital Object Identifier (DOI)https://doi.org/10.1016/j.compstruct.2018.11.066
Web address (URL)http://hdl.handle.net/10545/623174
hdl:10545/623174
Publication dates24 Nov 2018
Publication process dates
Deposited04 Dec 2018, 15:07
Accepted23 Nov 2018
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ContributorsUniversity of Derby and University of Bath
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