An investigation of the effect of R-ratio on the mode II fatigue delamination of AS4/3501-6 carbon/epoxy composites has been undertaken. Experiments have been performed on end notched cantilever beam specimens over a wide range of R-ratios (-l ≤R ≤0.50). The measured delamination growth rate data have been correlated with the mode II values of strain energy release rate range ∆G[formula omitted]), maximum strain energy release rate (G[formula omitted]) and stress intensity factor range (∆K[formula omitted]). The growth rate is dependent on the R-ratio over the range tested. For a constant level of ∆G[formula omitted], the crack growth rate decreases with increasing R-ratio. A similar trend is observed when the data is plotted as a function ...
International audienceThe study of fatigue delamination growth in composite materials aims to develo...
© 2017 International Committee on Composite Materials. All rights reserved. Mode I fatigue delaminat...
Delamination growth under fatigue loads in real composite components generally develops in a non-con...
Effect of stress ratio on the Mode I delamination growth behaviour of composite structures under fat...
This paper aims to investigate stress ratio effect on fibre bridging significance in mode I fatigue ...
An experimental investigation aimed at identifying the presence and onset of an asymptotic stable fr...
The available models for the prediction of fatigue crack growth in adhesive bonds rely on the simili...
The objective of this paper is to investigate the contribution/role of the crack closure and the fib...
The strain energy release rate (SERR) is widely used to study delamination growth in composites and ...
Due to the lack of fundamental knowledge of the physics behind delamination growth, certification au...
AbstractThe strain energy release rate (SERR) is widely used to study delamination growth in composi...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
This work aims at studying the loading rate dependency of mode I delamination growth in CFRPs, using...
Fiber reinforced composites are attractive for aerospace applications due to high specific strength ...
Advanced composite materials have been commonly used in aerospace engineering, because of their good...
International audienceThe study of fatigue delamination growth in composite materials aims to develo...
© 2017 International Committee on Composite Materials. All rights reserved. Mode I fatigue delaminat...
Delamination growth under fatigue loads in real composite components generally develops in a non-con...
Effect of stress ratio on the Mode I delamination growth behaviour of composite structures under fat...
This paper aims to investigate stress ratio effect on fibre bridging significance in mode I fatigue ...
An experimental investigation aimed at identifying the presence and onset of an asymptotic stable fr...
The available models for the prediction of fatigue crack growth in adhesive bonds rely on the simili...
The objective of this paper is to investigate the contribution/role of the crack closure and the fib...
The strain energy release rate (SERR) is widely used to study delamination growth in composites and ...
Due to the lack of fundamental knowledge of the physics behind delamination growth, certification au...
AbstractThe strain energy release rate (SERR) is widely used to study delamination growth in composi...
In a context of many studies addressing delamination growth in laminated composites, this thesis pro...
This work aims at studying the loading rate dependency of mode I delamination growth in CFRPs, using...
Fiber reinforced composites are attractive for aerospace applications due to high specific strength ...
Advanced composite materials have been commonly used in aerospace engineering, because of their good...
International audienceThe study of fatigue delamination growth in composite materials aims to develo...
© 2017 International Committee on Composite Materials. All rights reserved. Mode I fatigue delaminat...
Delamination growth under fatigue loads in real composite components generally develops in a non-con...