2018
DOI: 10.1007/s40430-018-1056-1
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Mixed mode cohesive zone modelling and analysis of adhesively bonded composite T-joint under pull-out load

Abstract: The failure behaviour of three different configurations of adhesively bonded carbon fibre composite T-joints subjected to pull-out load is investigated. Finite element analysis is carried out on the carbon fibre composite T-joint models. A nonlinear, contact target-based cohesive zone model with appropriate traction separation law is selected to simulate the pullout test condition in FE package ANSYS Ò. The FE analysis results are in close agreement with available experimental results.

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Cited by 28 publications
(7 citation statements)
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“…Under pure-mode loading, damage onset occurs when the cohesive strength in tension or shear (t n 0 or t s 0 , respectively) is attained, i.e., the material's elastic ceases to exist and degradation begin (Sane et al 2018). Moreover, the crack proliferates up to the adjacent pair of nodes when the values of current tensile or shear cohesive stresses (t n or t s , respectively) become null.…”
Section: Czm Theorymentioning
confidence: 99%
“…Under pure-mode loading, damage onset occurs when the cohesive strength in tension or shear (t n 0 or t s 0 , respectively) is attained, i.e., the material's elastic ceases to exist and degradation begin (Sane et al 2018). Moreover, the crack proliferates up to the adjacent pair of nodes when the values of current tensile or shear cohesive stresses (t n or t s , respectively) become null.…”
Section: Czm Theorymentioning
confidence: 99%
“…To corroborate these assumptions, accurate predictions in SLJ were found for the three adhesives. For this model, under pure-mode loading, damage initiation occurs when t n 0 or t s 0 are attained, i.e., the material's elastic behaviour is cancelled and degradation starts. 38 Furthermore, the crack propagates up to the adjacent pair of nodes when t n or t s become null. Under mixed-mode loading, stress and/or energetic criteria are often used to combine the pure-mode laws, and damage begins when the mixed mode cohesive strength ( t m 0 ) is reached.…”
Section: Experimental and Numerical Conditionsmentioning
confidence: 99%
“…Under pure-mode loading, damage initiation occurs when the cohesive strength in tension or shear ( t n 0 or t s 0 , respectively) is attained. 38 Furthermore, the crack propagates up to the adjacent pair of nodes when the values of current tensile or shear cohesive stresses ( t n or t s , respectively) become nil. Under mixed-mode loading, stress and/or energetic criteria are often used to combine the pure-mode laws, and damage begins when the mixed mode cohesive strength ( t m 0 ) is reached.…”
Section: Numerical Workmentioning
confidence: 99%