Delamination is a prevalent composite laminate failure mode. It is of particular concern to the aerospace industry where laminated composites have found widespread usage in critical applications. Delamination growth has been widely studied, with Linear Elastic Fracture Mechanics (LEFM) being the most common approach taken to predict delamination behaviour, typically through global parameters such as specimen geometry and applied load measured away from the actual crack tip. However, internal mechanisms, such as fibre bridging, can occur within the structure thus affecting the transfer of the globally applied conditions to the actual crack tip. Thus, measurements made at the actual crack tip, referred to as local measurements, can be...
Delamination is recognised as the most critical damage process in laminated composites: even a simpl...
The mixed mode delamination behavior of through-thickness reinforced carbon\u2013epoxy laminates was...
Delamination growth under fatigue loads in real composite components generally develops in a non-con...
Delamination is a prevalent composite laminate failure mode. It is of particular concern to the aer...
Delamination is an important failure mode for composite laminates. As it affects the mechanical res...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
AbstractA review will be given of the analysis of mixed mode delamination failure in composites and ...
In order to understand the physics of the delamination onset in laminated composites, an experimenta...
One of the major benefits of laminate composites reinforced with long fibers is the ability to orien...
Multidirectional laminates are very often used in advanced structures. However, the existing data in...
Scanning electron microscopy was used to identify fractographic features that are characteristic of ...
This paper demonstrates how the critical strain energy density in the delamination tip vicinity may ...
A wide variety of laboratory tests is currently employed to characterise the delamination toughness ...
A shear deformation model was developed to analyze local delaminations growing from transverse crack...
Delamination is recognised as the most critical damage process in laminated composites: even a simpl...
The mixed mode delamination behavior of through-thickness reinforced carbon\u2013epoxy laminates was...
Delamination growth under fatigue loads in real composite components generally develops in a non-con...
Delamination is a prevalent composite laminate failure mode. It is of particular concern to the aer...
Delamination is an important failure mode for composite laminates. As it affects the mechanical res...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
AbstractA review will be given of the analysis of mixed mode delamination failure in composites and ...
In order to understand the physics of the delamination onset in laminated composites, an experimenta...
One of the major benefits of laminate composites reinforced with long fibers is the ability to orien...
Multidirectional laminates are very often used in advanced structures. However, the existing data in...
Scanning electron microscopy was used to identify fractographic features that are characteristic of ...
This paper demonstrates how the critical strain energy density in the delamination tip vicinity may ...
A wide variety of laboratory tests is currently employed to characterise the delamination toughness ...
A shear deformation model was developed to analyze local delaminations growing from transverse crack...
Delamination is recognised as the most critical damage process in laminated composites: even a simpl...
The mixed mode delamination behavior of through-thickness reinforced carbon\u2013epoxy laminates was...
Delamination growth under fatigue loads in real composite components generally develops in a non-con...