The failure and the analysis of composite structures can be various. The failure modes can be investigated separately, but these modes generally arise together (e.g.: matrix cracking and delamination). Due to this experimental observation the main problem is to construct models that can follow more than one of the failure modes. To solve this problem the most proper method is the finite element method (FEM), because of its simplicity. The aim of this paper is to summarize a few publications about the damage and failure of composite materials and structures. The publications were grouped according to the mode of failure, the aim is to give a short description about the finite element modelling of the given failure mode. The models were recon...
The recent decades have seen various attempts at the numerical modelling of fibre-reinforced polymer...
The recent decades have seen various attempts at the numerical modelling of fibre-reinforced polymer...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90654/1/AIAA-2011-1722-752.pd
The failure and the analysis of composite structures can be various. The failure modes can be invest...
The failure and the analysis of composite structures can be various. The failure modes can be inves-...
This chapter is the result of a study of many special disciplines, such as damage of matrix, crackin...
ABSTRACT: Modeling progressive damage in composite materials and structures poses considerable chall...
The present article deals with micromechanical composite modeling. Both, analytical and computationa...
This thesis describes the investigation and development of damage modelling for composites materials...
Considerable effort has been put into the development of models describing damage and failure of fib...
Fiber-reinforced plastics are of increasing relevance in a broad variety of engineering applications...
Fiber-reinforced plastics are of increasing relevance in a broad variety of engineering applications...
A finite element model of the deformation and failure of brittle matrix composites during matrix cra...
Modelling of composite structures is limited by finite element (FE) codes to effectively model certa...
Damage and failure of fiber composites is a complex process the prediction of which requires adequat...
The recent decades have seen various attempts at the numerical modelling of fibre-reinforced polymer...
The recent decades have seen various attempts at the numerical modelling of fibre-reinforced polymer...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90654/1/AIAA-2011-1722-752.pd
The failure and the analysis of composite structures can be various. The failure modes can be invest...
The failure and the analysis of composite structures can be various. The failure modes can be inves-...
This chapter is the result of a study of many special disciplines, such as damage of matrix, crackin...
ABSTRACT: Modeling progressive damage in composite materials and structures poses considerable chall...
The present article deals with micromechanical composite modeling. Both, analytical and computationa...
This thesis describes the investigation and development of damage modelling for composites materials...
Considerable effort has been put into the development of models describing damage and failure of fib...
Fiber-reinforced plastics are of increasing relevance in a broad variety of engineering applications...
Fiber-reinforced plastics are of increasing relevance in a broad variety of engineering applications...
A finite element model of the deformation and failure of brittle matrix composites during matrix cra...
Modelling of composite structures is limited by finite element (FE) codes to effectively model certa...
Damage and failure of fiber composites is a complex process the prediction of which requires adequat...
The recent decades have seen various attempts at the numerical modelling of fibre-reinforced polymer...
The recent decades have seen various attempts at the numerical modelling of fibre-reinforced polymer...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90654/1/AIAA-2011-1722-752.pd