An analytical method based on the energy balance and wave propagation approach was developed for a sandwich panel\ud subjected to a ballistic impact. Possible energy absorbing mechanisms in the complete perforation of a sandwich panel\ud involve tensile fiber stretching and damage, matrix delamination and fracture, core compression and crushing, plugging, delamination between the core and bottom face sheet and friction. The complete perforation of the sandwich panel was modeled as 3-stage process that describes perforation of the top face sheet, complete densification of foam core, and perforation of the bottom face sheet sequentially. An experimental study was carried out to compare ballistic impact performance of foam core sandwich panel ...
The main objective of this thesis is to conduct a numerical study of aluminium foam core sacrificial...
Analytical solutions were derived for the transient response and damage initiation of a foam-core co...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd
A theoretical energy-based model to capture the ballistic response of sandwich structures made of co...
Metallic sandwich structures with aluminium foam core are good energy absorbers for impact protectio...
7 pages, 9 figuresIn this study the perforation of composite sandwich structures subjected to high-v...
Composite sandwich panels are well known for their relatively high stiffness over weight ratio and ...
This work evaluates the behavior of sandwich and spaced plates subjected to high-velocity impacts. T...
15th International Conference on Composite Structures (ICCS/15), University of Porto, Porto, Portuga...
Composite sandwich structures find wide application in the aerospace sector thanks to their lightwei...
This paper studies the high velocity impact response of sandwich plates, with E glass fibre/polyeste...
In this study, the low-velocity impact response of sandwich composites consisting of different foam ...
AbstractShock tube experiments were performed to study the dynamic response of sandwich panels with ...
This dissertation presents the experimental, numerical and analytical investigations on the impact b...
Impact resistance and energy absorbing capability are of great interest in the design of composite s...
The main objective of this thesis is to conduct a numerical study of aluminium foam core sacrificial...
Analytical solutions were derived for the transient response and damage initiation of a foam-core co...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd
A theoretical energy-based model to capture the ballistic response of sandwich structures made of co...
Metallic sandwich structures with aluminium foam core are good energy absorbers for impact protectio...
7 pages, 9 figuresIn this study the perforation of composite sandwich structures subjected to high-v...
Composite sandwich panels are well known for their relatively high stiffness over weight ratio and ...
This work evaluates the behavior of sandwich and spaced plates subjected to high-velocity impacts. T...
15th International Conference on Composite Structures (ICCS/15), University of Porto, Porto, Portuga...
Composite sandwich structures find wide application in the aerospace sector thanks to their lightwei...
This paper studies the high velocity impact response of sandwich plates, with E glass fibre/polyeste...
In this study, the low-velocity impact response of sandwich composites consisting of different foam ...
AbstractShock tube experiments were performed to study the dynamic response of sandwich panels with ...
This dissertation presents the experimental, numerical and analytical investigations on the impact b...
Impact resistance and energy absorbing capability are of great interest in the design of composite s...
The main objective of this thesis is to conduct a numerical study of aluminium foam core sacrificial...
Analytical solutions were derived for the transient response and damage initiation of a foam-core co...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd