This paper presents a numerical study of the delamination migration in angle-ply laminates observed in experiments reported in the literature, where the delamination originally propagates along the lower, 0∘/60∘ interface and later migrates onto the upper, 60∘/0∘ interface. The recently-developed Floating Node Method (FNM) is used for modelling this problem. The initiation and propagation of both delamination and matrix cracks are modelled within the FNM elements. Experimentally-observed phenomena such as the numerous kinking attempts and the multiple onset locations of migration are successfully predicted. The effect of load offset on the locations of migration is captured. In addition, this work tries to shed light on the proper use of st...
Abstract. Delamination is one of the most important failure mechanisms in laminates. Nor-mally, it i...
The object of this study is the development and implementation of a Cohesive Zone Model (CZM) for in...
This contribution starts with a discussion of various phenomena in laminated composite structures th...
AbstractThe transition of delamination growth between different ply interfaces in composite tape lam...
Predictive models have struggled to accurately simulate progressive delamination growth in composite...
Fiber-reinforced polymer matrix composites are being used increasingly in lightweight applications w...
The use of carbon fibre-epoxy composites in aerospace structures can enable significant weight savin...
The different failure mechanisms occurring in fibres reinforced polymer matrix composites usually ...
A consistent energy-based cohesive zone model to simulate the mode I delamination behaviour of Fully...
Transverse crack propagating towards a cross-ply interface is investigated in this study. The non-un...
In this paper, the recently-developed floating node method is extended for damage analysis of lamina...
In this work, an analysis on the influence of fibre-orientation in the progression of delamination w...
Delamination in composite structures is best modelled at a mesoscopic level. In this approach, the p...
Following the onset of damage caused by an impact load on a composite laminate structure, delaminati...
Abstract. Delamination is one of the most important failure mechanisms in laminates. Nor-mally, it i...
The object of this study is the development and implementation of a Cohesive Zone Model (CZM) for in...
This contribution starts with a discussion of various phenomena in laminated composite structures th...
AbstractThe transition of delamination growth between different ply interfaces in composite tape lam...
Predictive models have struggled to accurately simulate progressive delamination growth in composite...
Fiber-reinforced polymer matrix composites are being used increasingly in lightweight applications w...
The use of carbon fibre-epoxy composites in aerospace structures can enable significant weight savin...
The different failure mechanisms occurring in fibres reinforced polymer matrix composites usually ...
A consistent energy-based cohesive zone model to simulate the mode I delamination behaviour of Fully...
Transverse crack propagating towards a cross-ply interface is investigated in this study. The non-un...
In this paper, the recently-developed floating node method is extended for damage analysis of lamina...
In this work, an analysis on the influence of fibre-orientation in the progression of delamination w...
Delamination in composite structures is best modelled at a mesoscopic level. In this approach, the p...
Following the onset of damage caused by an impact load on a composite laminate structure, delaminati...
Abstract. Delamination is one of the most important failure mechanisms in laminates. Nor-mally, it i...
The object of this study is the development and implementation of a Cohesive Zone Model (CZM) for in...
This contribution starts with a discussion of various phenomena in laminated composite structures th...