WOSInternational audienceThis paper presents a multiscale hybrid approach for predicting damage and failure of laminated composite structures based on the thermo-mechanical properties (stress/strain behaviour and strength) of the unidirectional plies. This kind of approach is thus predictive for different stacking sequences. The approach introduces viscosity of the matrix in order to obtain an accurate description of the mesoscopic behaviour, especially the non-linearity under shear loading. The failure criterion used is based on physical principles and introduces micromechanical aspects (such as the effect of the local debonding on the non-linear failure behaviour) at the mesoscopic scale. The main improvements, over those proposed in the ...
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
The evolution of damage in laminated fiber reinforced composites is a complex phenomenon, which invo...
A failure-mechanism-based micromechanical theory has been proposed for the development of a failure ...
This paper proposes a multi-scale analysis technique based on the micromechanics of failure (MMF) to...
A micromechanics-based constituent progressive damage model was proposed in this study to predict ma...
A new damage model based on a micromechanical analysis of cracked [+/-0deg/90deg(sub n)]s laminates ...
This paper is concerned with a progressive failure analysis methodology for fiber reinforced composi...
There is no state of the art computational model that is good enough for predictive simulation of th...
ABSTRACT: A micromechanics-based constituent progressive damage model was proposed in this study to ...
Microscale damage mechanism of the multi-layer composite laminates is one of the active areas of res...
A failure-mechanism-based micromechanical theory has been proposed for the development of a failure ...
There is no state of the art computational model that is good enough for predictive simulation of th...
The failure of carbon fiber reinforced composite laminates is studied using a multiscale method. ...
A comprehensive, novel and computationally low cost multiscale model based on finite element analysi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77029/1/AIAA-2009-2545-493.pd
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
The evolution of damage in laminated fiber reinforced composites is a complex phenomenon, which invo...
A failure-mechanism-based micromechanical theory has been proposed for the development of a failure ...
This paper proposes a multi-scale analysis technique based on the micromechanics of failure (MMF) to...
A micromechanics-based constituent progressive damage model was proposed in this study to predict ma...
A new damage model based on a micromechanical analysis of cracked [+/-0deg/90deg(sub n)]s laminates ...
This paper is concerned with a progressive failure analysis methodology for fiber reinforced composi...
There is no state of the art computational model that is good enough for predictive simulation of th...
ABSTRACT: A micromechanics-based constituent progressive damage model was proposed in this study to ...
Microscale damage mechanism of the multi-layer composite laminates is one of the active areas of res...
A failure-mechanism-based micromechanical theory has been proposed for the development of a failure ...
There is no state of the art computational model that is good enough for predictive simulation of th...
The failure of carbon fiber reinforced composite laminates is studied using a multiscale method. ...
A comprehensive, novel and computationally low cost multiscale model based on finite element analysi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77029/1/AIAA-2009-2545-493.pd
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
The evolution of damage in laminated fiber reinforced composites is a complex phenomenon, which invo...
A failure-mechanism-based micromechanical theory has been proposed for the development of a failure ...