H. Liu
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
R. A. Brooks
Z. E.C. Hall
J. Liu
J. W.M. Crocker
A. M. Joesbury
Dr 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., Harper, L. T., Blackman, B. R., Kinloch, A. J., & 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 |
Publisher | The Royal Society |
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 |
Files
Final Revised. Clean-Phil Trans 2022-Accepted 6th Feb 2022
(1.1 Mb)
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