In this paper, a numerical home-made finite element model for the failure analysis of bolted joints between fiber-reinforced composite laminates is presented. The model is based on an incremental displacement basedapproach, it is hinged on the laminate theory and on a progressive material degradation governed by the failure of composite constituents. The model has been applied to a pin-plate system comprising a monodirectional fiber-reinforced laminated plate, and numerical results in terms of the bearing failure load have been successfully compared with available experimental data. Aim of this paper is to evaluate the effectiveness of Rotem’s and Huang’s failure criteria in predicting the pin-bearing failure of bolted joints. The selected ...
The paper deals with the influence of the geometric (joint clearance) and mechanical parameters (bol...
A method is presented for predicting the failure strength and the failure mode of fiber reinforced c...
The use of mechanical fasteners is still main assembling method for CFRP sub-structures in aircrafts...
In this paper, a numerical home-made finite element model for the failure analysis of bolted joints ...
AbstractThis paper aims to model the progressive damage of multi-bolted joints connecting structural...
In this paper, a progressive damage model based on a non-linear finite-element incremental approach ...
This paper presents finite-element predictions for the strength of a pultruded fiber-reinforced poly...
This paper aims to model the progressive damage of multi-bolted joints connecting structural element...
This paper aims to model the progressive damage of multi-bolted joints connecting structural element...
An analytical model to predict bearing failure of pinned-joint composite laminates is proposed. The ...
Finite Element Analysis numerical models were generated to simulate and investigate the pull-throug...
In this paper, the pin-induced progressive damage of fiber-reinforced laminates employed in composit...
A method is presented for predicting the failure strength and failure mode of pin-loaded holes in fi...
This paper considers a computation method in failure analysis of layered composites containing pin-l...
ABSTRACT: The aim of this research is to investigate the pin/hole contact stress of a composite lami...
The paper deals with the influence of the geometric (joint clearance) and mechanical parameters (bol...
A method is presented for predicting the failure strength and the failure mode of fiber reinforced c...
The use of mechanical fasteners is still main assembling method for CFRP sub-structures in aircrafts...
In this paper, a numerical home-made finite element model for the failure analysis of bolted joints ...
AbstractThis paper aims to model the progressive damage of multi-bolted joints connecting structural...
In this paper, a progressive damage model based on a non-linear finite-element incremental approach ...
This paper presents finite-element predictions for the strength of a pultruded fiber-reinforced poly...
This paper aims to model the progressive damage of multi-bolted joints connecting structural element...
This paper aims to model the progressive damage of multi-bolted joints connecting structural element...
An analytical model to predict bearing failure of pinned-joint composite laminates is proposed. The ...
Finite Element Analysis numerical models were generated to simulate and investigate the pull-throug...
In this paper, the pin-induced progressive damage of fiber-reinforced laminates employed in composit...
A method is presented for predicting the failure strength and failure mode of pin-loaded holes in fi...
This paper considers a computation method in failure analysis of layered composites containing pin-l...
ABSTRACT: The aim of this research is to investigate the pin/hole contact stress of a composite lami...
The paper deals with the influence of the geometric (joint clearance) and mechanical parameters (bol...
A method is presented for predicting the failure strength and the failure mode of fiber reinforced c...
The use of mechanical fasteners is still main assembling method for CFRP sub-structures in aircrafts...