2019
DOI: 10.1177/1464420719871390
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Numerical study of mode I fracture toughness of carbon-fibre-reinforced plastic under an impact load

Abstract: The main objective of this work is, by using cohesive zone modelling, to compute the fracture toughness behaviour in mode I of unidirectional carbon-fibre-reinforced plastic subjected to an impact load at 4.7 m/s. To perform this task, double-cantilever beam specimens were simulated, with its opening displacement and crack propagation being assessed, as well as the evolution of strain rate through the test. Therefore, by plotting the crack propagation, it was possible to calculate the fracture toughness in mod… Show more

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Cited by 3 publications
(4 citation statements)
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“…CZM concepts were also employed by Machado et al [190] for the rate-dependent analysis of adhesives. The linear elastic assumption has also been considered in some studies to numerically study the effect of strain rate [191].…”
Section: Strain Rate Effectsmentioning
confidence: 99%
“…CZM concepts were also employed by Machado et al [190] for the rate-dependent analysis of adhesives. The linear elastic assumption has also been considered in some studies to numerically study the effect of strain rate [191].…”
Section: Strain Rate Effectsmentioning
confidence: 99%
“…In the SPR forming process, the rivet needs to pierce the CFRP plate, which inevitably causes CFRP interlaminar damage (delamination) at the connection interface in the area around the rivet. Cohesive behavior is built into ABAQUS/Explicit to simulate delamination, and the model is based on the traction-separation criterion with the following equation 45 :…”
Section: Inter-laminar Damage Modelmentioning
confidence: 99%
“…In the SPR forming process, the rivet needs to pierce the CFRP plate, which inevitably causes CFRP interlaminar damage (delamination) at the connection interface in the area around the rivet. Cohesive behavior is built into ABAQUS/Explicit to simulate delamination, and the model is based on the traction-separation criterion with the following equation 45 : where t n, t s, t t represent the stress components in the normal, first, and second directions, respectively. K n, K s, K t represent the initial stiffness in the three directions, respectively.…”
Section: Numerical Modeling Of Cfrp/al Sprmentioning
confidence: 99%
“…On the other hand, the production of such complicated loading systems may have some practical challenges, and therefore, many researchers prefer to do their experiments by simple conventional systems. 1,1416…”
Section: Introductionmentioning
confidence: 99%