Add to ORKGImpact events can hardly be called quasi-static. To test for relevant properties with quasi-static test methods thus seems to make little sense, especially when materials with a rate-sensitivity are the subject of testing. Therefore, a test setup is developed to obtain the trac-tion-separation behaviour and fracture toughness of composites in mode I delamination at impact rates of deformation. An optical technique is applied to obtain the load-deflection curve, allowing for contactless measurements
This research aims at the high speed Mode I delamination characterisation of carbon Non Crimp Fabric...
A thorough experimental procedure is presented in which the mode II delamination resistance of a lam...
As global warming is a prime concern to the wellbeing of the planet, lighter planes are a requirem...
Impact events can hardly be called quasi-static. To test for relevant properties with quasi-static t...
This research investigates dynamic delamination Mode II of carbon Non-Crimp Fabric (NCF) epoxy compo...
A dynamic mode-I energy release rate (ERR) of a double cantilever beam (DCB) under impact from a str...
Through thickness reinforcement (TTR) technologies have been shown to provide effective delamination...
High-performance aerospace laminated composite structures manufactured from carbon-fibre prepreg are...
One of the major benefits of laminate composites reinforced with long fibers is the ability to orien...
Dynamic delamination of thick fiber reinforced polymeric matrix composite laminates is investigated ...
The present experimental study aims to extend the understanding of delamination crack bridging mech...
Delamination initiation and propagation of aeronautic composites is an active field of research. In ...
This thesis focuses on the subject of damage in composite materials and structures, in particular de...
Dynamic impact onto laminated composite structures can lead to large-scale delamination. This can be...
Damage sensitivity of composites under out-of-plane dynamic loading, and its limited detectability o...
This research aims at the high speed Mode I delamination characterisation of carbon Non Crimp Fabric...
A thorough experimental procedure is presented in which the mode II delamination resistance of a lam...
As global warming is a prime concern to the wellbeing of the planet, lighter planes are a requirem...
Impact events can hardly be called quasi-static. To test for relevant properties with quasi-static t...
This research investigates dynamic delamination Mode II of carbon Non-Crimp Fabric (NCF) epoxy compo...
A dynamic mode-I energy release rate (ERR) of a double cantilever beam (DCB) under impact from a str...
Through thickness reinforcement (TTR) technologies have been shown to provide effective delamination...
High-performance aerospace laminated composite structures manufactured from carbon-fibre prepreg are...
One of the major benefits of laminate composites reinforced with long fibers is the ability to orien...
Dynamic delamination of thick fiber reinforced polymeric matrix composite laminates is investigated ...
The present experimental study aims to extend the understanding of delamination crack bridging mech...
Delamination initiation and propagation of aeronautic composites is an active field of research. In ...
This thesis focuses on the subject of damage in composite materials and structures, in particular de...
Dynamic impact onto laminated composite structures can lead to large-scale delamination. This can be...
Damage sensitivity of composites under out-of-plane dynamic loading, and its limited detectability o...
This research aims at the high speed Mode I delamination characterisation of carbon Non Crimp Fabric...
A thorough experimental procedure is presented in which the mode II delamination resistance of a lam...
As global warming is a prime concern to the wellbeing of the planet, lighter planes are a requirem...