Abstract
A new micro-mechanical model is proposed for describing the bridging actions exerted by throughthickness reinforcement on delaminations in prepreg based composite materials, subjected to a mixedmode (I-II) loading regime. The model applies to micro-fasteners in the form of brittle fibrous rods (Z-pins) inserted in the through-thickness direction of composite laminates. These are described as Euler-Bernoulli beams inserted in an elastic foundation that represents the embedding composite laminate. Equilibrium equations that relate the delamination opening/sliding displacements to the bridging forces exerted by the Z-pins on the interlaminar crack edges are derived. The Z-pin failure meso-mechanics is explained in terms of the laminate architecture and the delamination mode. The apparent fracture toughness of Z-pinned laminates is obtained from as energy dissipated by the pull out of the throughthickness reinforcement, normalised with respect to a reference area. The model is validated by means of experimental data obtained for single carbon/BMI Z-pins inserted in a quasi-isotropic laminate. (C) 2014 Elsevier Ltd. All rights reserved.
Original language | English |
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Pages (from-to) | 3314-3332 |
Number of pages | 19 |
Journal | International Journal of Solids and Structures |
Volume | 51 |
Issue number | 19-20 |
DOIs | |
Publication status | Published - 1 Oct 2014 |
Structured keywords
- Composites UTC
Keywords
- Composite materials
- Fibre reinforced
- Delamination
- Toughness
- CARBON-FIBER-EPOXY
- T-JOINTS
- MECHANISMS
- TOUGHNESS
- FRACTURE
- PERFORMANCE
- STRENGTH
- TENSION
- CRACKS
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Professor Giuliano Allegri
- School of Civil, Aerospace and Design Engineering - Professor of Structural Integrity of Composites
- Composites University Technology Centre (UTC)
- Bristol Composites Institute (ACCIS)
Person: Academic