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Experimental and numerical investigations on the impact behaviour of pristine and patch-repaired composite laminates

Liu, H.; Brooks, R. A.; Hall, Z. E.C.; Liu, J.; Crocker, J. W.M.; Joesbury, A. M.; Harper, L. T.; Blackman, B. R.K.; Kinloch, A. J.; Dear, J. P.

Authors

H. Liu

R. A. Brooks

Z. E.C. Hall

J. Liu

J. W.M. Crocker

LEE HARPER LEE.HARPER@NOTTINGHAM.AC.UK
Associate Professor - Composites Manufacturing

B. R.K. Blackman

A. J. Kinloch

J. P. Dear



Abstract

The present paper investigates the impact behaviour of both pristine carbon-fibre-reinforced-plastic (CFRP) composite laminates and repaired CFRP laminates. For the patch-repaired CFRP specimen, the pristine CFRP panel specimen has been damaged by cutting out a central disc of the CFRP material and then repaired using an adhesively bonded patch of CFRP to cover the hole. Drop-weight, impact tests are performed on these two types of specimens and a numerical elastic-plastic, three-dimensional damage model is developed and employed to simulate the impact behaviour of both types of specimen. This numerical model is meso-scale in nature and assumes that cracks initiate in the CFRP at a nano-scale, in the matrix around fibres, and trigger sub-micrometre intralaminar matrix cracks during the impact event. These localized regions of intralaminar cracking then lead to interlaminar, i.e. delamination, cracking between the neighbouring plies which possess different fibre orientations. These meso-scale, intralaminar and interlaminar, damage processes are modelled using the numerical finite-element analysis model with each individual ply treated as a continuum. Good agreement is found between the results from the experimental studies and the predictions from the numerical simulations. This article is part of the theme issue 'Nanocracks in nature and industry'.

Citation

Liu, H., Brooks, R. A., Hall, Z. E., Liu, J., Crocker, J. W., Joesbury, A. M., …Dear, J. P. (2022). Experimental and numerical investigations on the impact behaviour of pristine and patch-repaired composite laminates. Philosophical Transactions A: Mathematical, Physical and Engineering Sciences, 380(2232), Article 20210340. https://doi.org/10.1098/rsta.2021.0340

Journal Article Type Article
Acceptance Date Feb 6, 2022
Online Publication Date Aug 1, 2022
Publication Date Sep 19, 2022
Deposit Date Jan 10, 2023
Publicly Available Date Jan 18, 2023
Journal Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences
Print ISSN 1364-503X
Electronic ISSN 1471-2962
Peer Reviewed Peer Reviewed
Volume 380
Issue 2232
Article Number 20210340
DOI https://doi.org/10.1098/rsta.2021.0340
Keywords General Physics and Astronomy; General Engineering; General Mathematics
Public URL https://nottingham-repository.worktribe.com/output/15929788
Publisher URL https://royalsocietypublishing.org/doi/10.1098/rsta.2021.0340

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