In this thesis, the low-velocity impact behavior of sandwich structures having aluminum foam core reinforced with aluminum plates was investigated. In this study, the effects of the Al-foam core density and the impact energy on the impact response of sandwich structures were investigated.Sandwich plates were produced by combining of Al-foams with three different densities of 0.37, 0.52, and 0.70 g/cm3, placed between Al-6061-T6 reinforcement plates with epoxy adhesive. Low velocity impact tests were carried out for each sample at 15, 30, 45 and 60J impact energies.The low-velocity impact tests of the prepared samples were carried out with the CEAST Fractovis impact device in the Mechanic Laboratory of the Mechanical Engineering Department o...
In this study, the low-velocity impact response of sandwich composites consisting of different foam ...
High specific strength and stiffness dominate the choice of material selection in the fields of weig...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd
In this study, the low-velocity impact behavior of sandwich structures having aluminum foam core rei...
Relative performance of metal and polymeric foam cored sandwich plates is studied under low velocity...
© 2020 Elsevier Ltd This study aimed to investigate low-velocity impact responses and crashworthines...
International audienceThe sandwich panel structures with aluminum foam core and metal surfaces have ...
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...
ABSTRACT: The energy absorption of an aluminum foam sandwich structure and a conventional polymer fo...
The main objective of this thesis is to conduct a numerical study of aluminium foam core sacrificial...
Sandwich panels with aluminium (Al) foam as the core have been increasingly attracting research inte...
Aluminium (Al) foam sandwich panels are of strong capability to resist impact and absorb energy sinc...
Aluminium foams and aluminium sandwich structures with metal foam cores are novel materials and stru...
Low velocity impact responses of a newly developed sandwich panel with aluminium foam core and fibre...
In this study, the low-velocity impact response of sandwich composites consisting of different foam ...
High specific strength and stiffness dominate the choice of material selection in the fields of weig...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd
In this study, the low-velocity impact behavior of sandwich structures having aluminum foam core rei...
Relative performance of metal and polymeric foam cored sandwich plates is studied under low velocity...
© 2020 Elsevier Ltd This study aimed to investigate low-velocity impact responses and crashworthines...
International audienceThe sandwich panel structures with aluminum foam core and metal surfaces have ...
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...
ABSTRACT: The energy absorption of an aluminum foam sandwich structure and a conventional polymer fo...
The main objective of this thesis is to conduct a numerical study of aluminium foam core sacrificial...
Sandwich panels with aluminium (Al) foam as the core have been increasingly attracting research inte...
Aluminium (Al) foam sandwich panels are of strong capability to resist impact and absorb energy sinc...
Aluminium foams and aluminium sandwich structures with metal foam cores are novel materials and stru...
Low velocity impact responses of a newly developed sandwich panel with aluminium foam core and fibre...
In this study, the low-velocity impact response of sandwich composites consisting of different foam ...
High specific strength and stiffness dominate the choice of material selection in the fields of weig...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97064/1/AIAA2012-1701.pd