2003
DOI: 10.1016/s1359-835x(03)00252-5
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Effects of inter-fibre spacing and matrix cracks on stress amplification factors in carbon-fibre/epoxy matrix composites. Part I: planar array of fibres

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Cited by 15 publications
(11 citation statements)
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“…effect of matrix cracking on the stress redistribution by introducing a conical-shaped matrix crack initiated from the fiber fracture into the FE model during an additional load step. [6] A numerical model of composite with matrix defects of three different shapes, including square, circular and hexagonal, were investigated by Li et al [7] Fiedler et al studied stress amplification in multi-fiber model composites by using a fiber with a pre-existing crack in their model; [8] However, the presence of matrix cracks in this composite model was neglected, as in the study done by Van den Heuvel et al [9] Analysis of the initial interface debonding which occurs around fiber breaks during tensile load was investigated by Zhou et al, based on an energy balance model. [10] From an overview of the literature regarding the fibrous composites damage research, it appears that the present numerical studies have mostly been performed only on one special damage mode, namely the local load transfer at the interface between fiber and matrix and the local stress concentration due to fiber break or matrix crack, [11][12][13][14][15][16][17] while few studies have yet been performed on the propagation of cracks towards the interface.…”
Section: Full Papermentioning
confidence: 99%
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“…effect of matrix cracking on the stress redistribution by introducing a conical-shaped matrix crack initiated from the fiber fracture into the FE model during an additional load step. [6] A numerical model of composite with matrix defects of three different shapes, including square, circular and hexagonal, were investigated by Li et al [7] Fiedler et al studied stress amplification in multi-fiber model composites by using a fiber with a pre-existing crack in their model; [8] However, the presence of matrix cracks in this composite model was neglected, as in the study done by Van den Heuvel et al [9] Analysis of the initial interface debonding which occurs around fiber breaks during tensile load was investigated by Zhou et al, based on an energy balance model. [10] From an overview of the literature regarding the fibrous composites damage research, it appears that the present numerical studies have mostly been performed only on one special damage mode, namely the local load transfer at the interface between fiber and matrix and the local stress concentration due to fiber break or matrix crack, [11][12][13][14][15][16][17] while few studies have yet been performed on the propagation of cracks towards the interface.…”
Section: Full Papermentioning
confidence: 99%
“…Crack propagation was simulated by deactivating the contact elements along the crack path during the final load steps. [6] But this model is far more intricate.…”
Section: Full Papermentioning
confidence: 99%
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“…[4][5][6] Some experimental data has been obtained by Raman spectroscopy, 7,8 including attempts to measure strains in the interior of composites by embedding optic probe fibres, used to transmit Raman spectra. 7 However as pointed out by Surgeon and Wevers, 9 the presence of larger diameter fibres affects the surrounding stress field and reduces the value of the measurements.…”
Section: Introductionmentioning
confidence: 99%
“…A special challenge is detection and localization of hidden defects, which can have many forms depending on the scale of the problem, eg. dislocations, voids or inclusions in microscale [43,49,44,3] to macroscopic defects, such as delamination in laminated composites [31] or welds in metallic materials [53,50]. The current work is focused on testing the applicability of dynamic vibration-based, as well as the space analysis methods to defect detection and localization in 1D (beam) structures.…”
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confidence: 99%