Add to ORKGDelamination initiation and propagation of aeronautic composites is an active field of research. In this paper we present a methodology for critical energy release rate correlation of numerical simulation and experimental data. Experiments of mode I critical energy release rate were carried out at quasi static and pseudo dynamic loading rates. Cohesive finite elements are used to predict the propagation of delamination in a carbon fiber and epoxy resin composite material. A bilinear material model is implemented via user defined cohesive material subroutine in LS-DYNA. The influence of mode I energy release rate in mixed mode loading, due to a low velocity impact, is also investigate
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The diffusion of composite laminates in aerospace industry has been slowed down by complexity in the...
International audienceDelamination initiation and propagation of aeronautic composites is an active ...
Cohesive finite elements are used to model impact induced delamination prediction of T800/21M unidir...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
The simulation of delamination using the Finite Element Method (FEM) is a useful tool to analyze fra...
The reliability of composite structures depends, among other damage mechanisms, on their ability to ...
The reliability of composite structures depends, among other damage mechanisms, on their ability to ...
International audienceIn this paper we present a methodology for the prediction of impact induced da...
Low-velocity impacts (LVIs) can seriously harm composite laminates by causing both intralaminar (fib...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
AbstractThis paper presents detailed experimental information on mode-II delamination development in...
This paper discusses in detail the use of cohesive interface elements for simulation of delamination...
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The diffusion of composite laminates in aerospace industry has been slowed down by complexity in the...
International audienceDelamination initiation and propagation of aeronautic composites is an active ...
Cohesive finite elements are used to model impact induced delamination prediction of T800/21M unidir...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
The simulation of delamination using the Finite Element Method (FEM) is a useful tool to analyze fra...
The reliability of composite structures depends, among other damage mechanisms, on their ability to ...
The reliability of composite structures depends, among other damage mechanisms, on their ability to ...
International audienceIn this paper we present a methodology for the prediction of impact induced da...
Low-velocity impacts (LVIs) can seriously harm composite laminates by causing both intralaminar (fib...
In this paper we present a methodology for the prediction of impact induced damage in aeronautical c...
AbstractThis paper presents detailed experimental information on mode-II delamination development in...
This paper discusses in detail the use of cohesive interface elements for simulation of delamination...
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The mechanism of damage initiation and growth in layered composites subjected to low- velocity impac...
The diffusion of composite laminates in aerospace industry has been slowed down by complexity in the...