The following work focus on the experimental study of low-velocity oblique impact on composite sandwich plates. Several impact angles and impact energies are selected to study their influence on the maximum contact force, maximum contact time, absorbed energy, maximum displacement of the impactor, and damaged area. Peak load and energy absorption rise with increasing impact energy and impact angle, while the contact time remains almost constant. No major differences in the results are shown for impact angles lower than 15 degrees. In addition, a numerical model is developed to reproduce the experimental results and study the evolution of the main impact results for impact angles difficult to perform experimentally (up to 50 degrees). A good...
Given the widespread usage of composite components in critical structures within the aerospace and a...
Low-velocity impact response of composite sandwich panels Shengqing Zhu and Gin Boay Chai In the pre...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd
The following work focus on the experimental study of low-velocity oblique impact on composite sandw...
The low-velocity impact behavior of repaired sandwich structures with woven carbon/epoxy face-sheets...
This paper presents the perforation behaviour of polyethylene terephthalate (PET) foam cored sandwic...
This research project focussed on the low-velocity oblique impact response of glass fibre-reinforced...
This dissertation presents experimental, numerical and analytical investigations of sandwich plates ...
This dissertation presents the experimental, numerical and analytical investigations on the impact b...
The paper reports the results of an experimental and numerical investigation into the effect of the...
Structural response of composite structures subjected to different impact loadings is studied. The l...
In this work the low-velocity impact response of composite sandwich beams was studied by an analytic...
International audienceAn experimental and numerical analysis of the influence of impactor shapes on ...
An experimental and numerical analysis of the influence of impactor shapes on the low velocity impac...
This article is focused on progressive failure analysis of sandwich composite structure subjected to...
Given the widespread usage of composite components in critical structures within the aerospace and a...
Low-velocity impact response of composite sandwich panels Shengqing Zhu and Gin Boay Chai In the pre...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd
The following work focus on the experimental study of low-velocity oblique impact on composite sandw...
The low-velocity impact behavior of repaired sandwich structures with woven carbon/epoxy face-sheets...
This paper presents the perforation behaviour of polyethylene terephthalate (PET) foam cored sandwic...
This research project focussed on the low-velocity oblique impact response of glass fibre-reinforced...
This dissertation presents experimental, numerical and analytical investigations of sandwich plates ...
This dissertation presents the experimental, numerical and analytical investigations on the impact b...
The paper reports the results of an experimental and numerical investigation into the effect of the...
Structural response of composite structures subjected to different impact loadings is studied. The l...
In this work the low-velocity impact response of composite sandwich beams was studied by an analytic...
International audienceAn experimental and numerical analysis of the influence of impactor shapes on ...
An experimental and numerical analysis of the influence of impactor shapes on the low velocity impac...
This article is focused on progressive failure analysis of sandwich composite structure subjected to...
Given the widespread usage of composite components in critical structures within the aerospace and a...
Low-velocity impact response of composite sandwich panels Shengqing Zhu and Gin Boay Chai In the pre...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd