Additive binding layers to suppress free edge delamination in composite laminates under tension
Additive binding layers to suppress free edge delamination in composite laminates under tension
An additive laminate applied to the free-edges of composite laminates is proposed to stop the development of delamination. Numerical analyses were conducted to find the optimum additive binding layup and the experimental results proved that the free-edge delamination was successfully suppressed. When it was used to bind the edges of a [(202/-202)2]s angle-ply laminate, the tensile failure strain and load of the laminate were increased by about 50%, and the failure mode changed from free-edge delamination to in-plane shear. However, it did not change the failure load and final failure mode of a [452/02/-452/902]s quasi-isotropic laminate, as this substrate is less susceptible to free-edge delamination. Thus, this technique is an efficient solution for suppressing free-edge delamination in real structural applications and in the characterisation of coupon tests where damage at the free-edges undermines the real potential of the composite substrate.
angle-ply, failure, finite element analysis (fea), mechanical testing
Ubago Torres, Miguel
1ef92de3-aba7-4302-a684-76908fc865cd
Jalalvand, Meisam
21ef0df8-fc7c-4466-a2fc-ee98ed3408a2
8 March 2022
Ubago Torres, Miguel
1ef92de3-aba7-4302-a684-76908fc865cd
Jalalvand, Meisam
21ef0df8-fc7c-4466-a2fc-ee98ed3408a2
Ubago Torres, Miguel and Jalalvand, Meisam
(2022)
Additive binding layers to suppress free edge delamination in composite laminates under tension.
Composites Part A: Applied Science and Manufacturing, 156, [106902].
(doi:10.1016/j.compositesa.2022.106902).
Abstract
An additive laminate applied to the free-edges of composite laminates is proposed to stop the development of delamination. Numerical analyses were conducted to find the optimum additive binding layup and the experimental results proved that the free-edge delamination was successfully suppressed. When it was used to bind the edges of a [(202/-202)2]s angle-ply laminate, the tensile failure strain and load of the laminate were increased by about 50%, and the failure mode changed from free-edge delamination to in-plane shear. However, it did not change the failure load and final failure mode of a [452/02/-452/902]s quasi-isotropic laminate, as this substrate is less susceptible to free-edge delamination. Thus, this technique is an efficient solution for suppressing free-edge delamination in real structural applications and in the characterisation of coupon tests where damage at the free-edges undermines the real potential of the composite substrate.
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Accepted/In Press date: 25 February 2022
e-pub ahead of print date: 1 March 2022
Published date: 8 March 2022
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© 2022 Elsevier Ltd
Keywords:
angle-ply, failure, finite element analysis (fea), mechanical testing
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Local EPrints ID: 478395
URI: http://eprints.soton.ac.uk/id/eprint/478395
ISSN: 1359-835X
PURE UUID: 55d4ec08-8b8b-470c-9f3f-6ea93ff4b879
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Date deposited: 29 Jun 2023 16:56
Last modified: 17 Mar 2024 04:02
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Author:
Miguel Ubago Torres
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