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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Funari, Marco Francesco
University of Surrey
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (7/7 displayed)
- 2020An experimental and numerical study to evaluate the crack path under mixed mode loading on pvc foamscitations
- 2020A moving interface finite element formulation to predict dynamic edge debonding in FRP-strengthened concrete beams in service conditionscitations
- 2019A numerical model based on ALE formulation to predict crack propagation in sandwich structurescitations
- 2018An interface approach based on moving mesh and cohesive modeling in Z-pinned composite laminatescitations
- 2017Dynamic debonding in layered structures:A coupled ALE-cohesive approach
- 2017A coupled ALE-Cohesive formulation for layered structural systemscitations
- 2016A moving interface finite element formulation for layered structurescitations
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article
An interface approach based on moving mesh and cohesive modeling in Z-pinned composite laminates
Abstract
An FE approach based Arbitrary Lagrangian-Eulerian (ALE) and cohesive fracture mechanics is implemented to investigate the effects of debonding mechanisms on the behavior of z-pinned composite laminates. The model is based on the combination of moving and discrete cohesive interface elements, which allow the simulation of interfacial damage or strengthening mechanisms produced by debonding phenomena or z-pinned techniques, respectively. Moreover, complex phenomena such as crack initiation, coalescence mechanisms are easily implemented in both static and dynamic frameworks. Despite existing approaches, available from the literature, the computational procedure is able to overcome difficulties concerning mesh dependence of the solution, numerical complexities and costs involved in the solving procedure. The numerical implementation of the model and its capability to predict debonding mechanisms are discussed with respect different laminate configurations and onset conditions. Moreover, comparisons with existing experimental results available from the literature are developed to investigate the relationship between strengthened and unstrengthened composite laminates. © 2017 Elsevier Ltd