The mixed mode delamination behavior of through-thickness reinforced carbon\u2013epoxy laminates was investigated using two different test specimens, a T-stiffener and a mixed-mode bending (MMB) specimen. Small quantities of titanium or carbon z-fibers (short rods) substantially improve delamination resistance in both types of specimen. Reinforcement raises the ultimate strength of the MMB specimen by a factor of three. However, the failure sequence and therefore the ultimate load in the T-stiffeners depend strongly on the test configuration. No change in ultimate load is seen in some cases but up to 40% improvement is observed in others. Improved delamination resistance results from crack bridging by the z-fibers, which reduces the driving...
Dynamic impact onto laminated composite structures can lead to large-scale delamination. This can be...
The present experimental study aims to extend the understanding of delamination crack bridging mech...
Delamination cracks in composites may interact with misaligned or inclined fibers. Such interactions...
Delamination resistance of composite laminates can be improved with through-thickness reinforcement ...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
AbstractA new micro-mechanical model is proposed for describing the bridging actions exerted by thro...
The paper outlines the current status of mechanical testing, identification of failure mechanisms a...
This paper presents a detailed numerical study of the mode I interlaminar fracture of carbon/epoxy ...
This study investigates the effects of Z-pinning on the delamination performance in opening and shea...
This paper presents an experimental investigation into the mode I interlaminar fracture toughness an...
Delamination is a prevalent composite laminate failure mode. It is of particular concern to the aer...
An experimental investigation is presented into the improvement to the delamination fatigue resistan...
One of the most effective technique, developed over the last decade, to enhance the strength of the ...
The delamination fracture behaviour in static and fatigue loading for T300/914C composite laminate h...
Resistance to impact induced delamination damage is critical to the safety of composite structures, ...
Dynamic impact onto laminated composite structures can lead to large-scale delamination. This can be...
The present experimental study aims to extend the understanding of delamination crack bridging mech...
Delamination cracks in composites may interact with misaligned or inclined fibers. Such interactions...
Delamination resistance of composite laminates can be improved with through-thickness reinforcement ...
Failure of composite laminates involves different damage mechanisms that result in the degradation o...
AbstractA new micro-mechanical model is proposed for describing the bridging actions exerted by thro...
The paper outlines the current status of mechanical testing, identification of failure mechanisms a...
This paper presents a detailed numerical study of the mode I interlaminar fracture of carbon/epoxy ...
This study investigates the effects of Z-pinning on the delamination performance in opening and shea...
This paper presents an experimental investigation into the mode I interlaminar fracture toughness an...
Delamination is a prevalent composite laminate failure mode. It is of particular concern to the aer...
An experimental investigation is presented into the improvement to the delamination fatigue resistan...
One of the most effective technique, developed over the last decade, to enhance the strength of the ...
The delamination fracture behaviour in static and fatigue loading for T300/914C composite laminate h...
Resistance to impact induced delamination damage is critical to the safety of composite structures, ...
Dynamic impact onto laminated composite structures can lead to large-scale delamination. This can be...
The present experimental study aims to extend the understanding of delamination crack bridging mech...
Delamination cracks in composites may interact with misaligned or inclined fibers. Such interactions...