The influence of fibre bridging on delamination failure in multidirectional composite laminates with different thickness scales is characterized, and the dependence of fibre bridging significance on laminate thickness as well as loading regime is investigated in this paper. Both quasi-static and fatigue resistance curves (R-curve) are experimentally determined to quantify the significance of fibre bridging in delamination growth. The results clearly demonstrate that thickness has effect on the amount of fibre bridging in quasi-static delamination. And the significance of fibre bridging decreases with the increase in laminate thickness. However, the situation for fatigue delamination growth (FDG) is much more complicated. The difference in f...
The delamination growth represents one of the main phenomena involved in the fatigue damage evolutio...
The introduction, originally in 2009, by the FAA of a ‘slow growth’ approach to the certification of...
Recently, advances have been made in the design, manufacture and application of composite materials....
The influence of fibre bridging on delamination failure in multidirectional composite laminates with...
Fatigue delamination in multidirectional composite laminates was experimentally investigated in pres...
This paper provides an investigation on thickness effects on fibre-bridged fatigue delamination grow...
Advanced composite materials have been commonly used in aerospace engineering, because of their good...
Fibre bridging can significantly enhance delamination resistance making the use of a single Paris re...
This paper aims to investigate stress ratio effect on fibre bridging significance in mode I fatigue ...
The objective of this paper is to investigate the contribution/role of the crack closure and the fib...
A fiber bridging model has been created to examine the effects of bridging on Mode I delamination fa...
This paper proposes a straightforward methodology to generate fatigue delamination curves without th...
Composite materials have multiple failure modes. Most of these failure modes are dedicated to the di...
Fatigue delamination growth in composite laminates is strongly influenced by mean loads or load rati...
The layers of a composite material may tend to debond under the influence of different static and/or...
The delamination growth represents one of the main phenomena involved in the fatigue damage evolutio...
The introduction, originally in 2009, by the FAA of a ‘slow growth’ approach to the certification of...
Recently, advances have been made in the design, manufacture and application of composite materials....
The influence of fibre bridging on delamination failure in multidirectional composite laminates with...
Fatigue delamination in multidirectional composite laminates was experimentally investigated in pres...
This paper provides an investigation on thickness effects on fibre-bridged fatigue delamination grow...
Advanced composite materials have been commonly used in aerospace engineering, because of their good...
Fibre bridging can significantly enhance delamination resistance making the use of a single Paris re...
This paper aims to investigate stress ratio effect on fibre bridging significance in mode I fatigue ...
The objective of this paper is to investigate the contribution/role of the crack closure and the fib...
A fiber bridging model has been created to examine the effects of bridging on Mode I delamination fa...
This paper proposes a straightforward methodology to generate fatigue delamination curves without th...
Composite materials have multiple failure modes. Most of these failure modes are dedicated to the di...
Fatigue delamination growth in composite laminates is strongly influenced by mean loads or load rati...
The layers of a composite material may tend to debond under the influence of different static and/or...
The delamination growth represents one of the main phenomena involved in the fatigue damage evolutio...
The introduction, originally in 2009, by the FAA of a ‘slow growth’ approach to the certification of...
Recently, advances have been made in the design, manufacture and application of composite materials....