Fiber-reinforced polymer matrix composites are being used increasingly in lightweight applications where high strength and stiffness is required. One of the main challenges with designing components from such materials is to predict the ultimate strength and behaviour of the structure. Furthermore, due to anisotropic material response and a complex micro structure, various interacting failure modes exist. In the present work, the interaction between inter- and intralaminar cracks that causes delamination to migrate from one ply interface to another is simulated for cross-ply laminates. A modeling approach that combines the extended finite element method and a surface-based contact formulation with a cohesive zone model is employed. This ena...
AbstractIn this paper interface element with de-cohesive constitutive law is used to predict the fai...
Based on theories of laminate anisotropic elasticity and interlaminar fracture, the complete solutio...
In this paper, a progressive damage model reflecting the interaction between delamination and intral...
The different failure mechanisms occurring in fibres reinforced polymer matrix composites usually ...
There is no state of the art computational model that is good enough for predictive simulation of th...
In this work, an analysis on the influence of fibre-orientation in the progression of delamination w...
Following the onset of damage caused by an impact load on a composite laminate structure, delaminati...
AbstractThe transition of delamination growth between different ply interfaces in composite tape lam...
The ply delamination which is known as a principle mode of failure of layered composites due to sepa...
The object of this study is the development and implementation of a Cohesive Zone Model (CZM) for in...
In this paper, a damage model using cohesive damage zone for the simulation of progressive delaminat...
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
The use of carbon fibre-epoxy composites in aerospace structures can enable significant weight savin...
The reliability of composite structures depends, among other damage mechanisms, on their ability to ...
Fibre-reinforced laminated composites subjected to quasi-static or low-velocity impact loading usual...
AbstractIn this paper interface element with de-cohesive constitutive law is used to predict the fai...
Based on theories of laminate anisotropic elasticity and interlaminar fracture, the complete solutio...
In this paper, a progressive damage model reflecting the interaction between delamination and intral...
The different failure mechanisms occurring in fibres reinforced polymer matrix composites usually ...
There is no state of the art computational model that is good enough for predictive simulation of th...
In this work, an analysis on the influence of fibre-orientation in the progression of delamination w...
Following the onset of damage caused by an impact load on a composite laminate structure, delaminati...
AbstractThe transition of delamination growth between different ply interfaces in composite tape lam...
The ply delamination which is known as a principle mode of failure of layered composites due to sepa...
The object of this study is the development and implementation of a Cohesive Zone Model (CZM) for in...
In this paper, a damage model using cohesive damage zone for the simulation of progressive delaminat...
Delamination is a common failure mode in composite (fiber reinforced and layered) structures subject...
The use of carbon fibre-epoxy composites in aerospace structures can enable significant weight savin...
The reliability of composite structures depends, among other damage mechanisms, on their ability to ...
Fibre-reinforced laminated composites subjected to quasi-static or low-velocity impact loading usual...
AbstractIn this paper interface element with de-cohesive constitutive law is used to predict the fai...
Based on theories of laminate anisotropic elasticity and interlaminar fracture, the complete solutio...
In this paper, a progressive damage model reflecting the interaction between delamination and intral...