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Papers by Vinod K

Research paper thumbnail of Impact properties of fibre metal laminates

Composites Engineering, 1993

Conventional composites are known for their sensitivity to impact damage. This has slowed their w... more Conventional composites are known for their sensitivity to impact damage. This has slowed their widespread application to thin, damage tolerance-critical primary structures such as fuselage pressure cabin skins. Therefore, impact tests were performed to determine the impact characteristics of Fibre Metal Laminates (GLARE and ARALL). Comparative low and high velocity impact tests were performed on monolithic aluminium, Fibre Metal Laminates, and carbon thermoplastic composites. Additional impact tests were performed on monolithic aluminium and ARALL specimens under tensile loading.

Research paper thumbnail of The high velocity impact response of composite and FML-reinforced sandwich structures

Composites Science and technology, 2004

... Chen and co-workers investigated the plastic collapse of sandwich beams based onaluminium fac... more ... Chen and co-workers investigated the plastic collapse of sandwich beams based onaluminium face sheets bonded to an aluminium foam core [3]. Here, it was found that the thickness of the foam affects the shear strength of the core. ...

Research paper thumbnail of Low-velocity impact failure of aluminium honeycomb sandwich panels

Composite Structures, 2008

In this paper, the failure response of aluminium sandwich panels subjected to low-velocity impact... more In this paper, the failure response of aluminium sandwich panels subjected to low-velocity impact is discussed. A three-dimensional geometrically correct finite element model of the honeycomb sandwich plate and a rigid impactor was developed using the commercial software, ABAQUS. This discrete modelling approach enabled further understanding of the parameters affecting the initiation and propagation of impact damage. Strain-hardening behaviour of the aluminium alloys and the honeycomb core density were shown to affect the impact response. In addition, the impulse-momentum equation was incorporated into the energy-balance model, so that the impact force and deflection histories could be determined as well.

Research paper thumbnail of Impact properties of fibre metal laminates

Composites Engineering, 1993

Conventional composites are known for their sensitivity to impact damage. This has slowed their w... more Conventional composites are known for their sensitivity to impact damage. This has slowed their widespread application to thin, damage tolerance-critical primary structures such as fuselage pressure cabin skins. Therefore, impact tests were performed to determine the impact characteristics of Fibre Metal Laminates (GLARE and ARALL). Comparative low and high velocity impact tests were performed on monolithic aluminium, Fibre Metal Laminates, and carbon thermoplastic composites. Additional impact tests were performed on monolithic aluminium and ARALL specimens under tensile loading.

Research paper thumbnail of The high velocity impact response of composite and FML-reinforced sandwich structures

Composites Science and technology, 2004

... Chen and co-workers investigated the plastic collapse of sandwich beams based onaluminium fac... more ... Chen and co-workers investigated the plastic collapse of sandwich beams based onaluminium face sheets bonded to an aluminium foam core [3]. Here, it was found that the thickness of the foam affects the shear strength of the core. ...

Research paper thumbnail of Low-velocity impact failure of aluminium honeycomb sandwich panels

Composite Structures, 2008

In this paper, the failure response of aluminium sandwich panels subjected to low-velocity impact... more In this paper, the failure response of aluminium sandwich panels subjected to low-velocity impact is discussed. A three-dimensional geometrically correct finite element model of the honeycomb sandwich plate and a rigid impactor was developed using the commercial software, ABAQUS. This discrete modelling approach enabled further understanding of the parameters affecting the initiation and propagation of impact damage. Strain-hardening behaviour of the aluminium alloys and the honeycomb core density were shown to affect the impact response. In addition, the impulse-momentum equation was incorporated into the energy-balance model, so that the impact force and deflection histories could be determined as well.

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