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Posts Tagged ‘JOINTS (Engineering)’

Characteristics of interlaminar stresses for damages in adhesively-bonded composite single lap joints






In this paper three-dimensional non-linear finite element analyses are carried out to evaluate accurately the stresses over the different critical surfaces for adhesion failure, cohesion failure and delamination damages of an adhesively-bonded fibre-reinforced polymer (FRP) composite single lap joint (SLJ) subjected to an in-plane loading. The top and bottom adherends of the SLJ are formed by eight layers of unidirectional graphite FRP composite and the material of the adhesive is epoxy. The out-of-plane stresses and their distribution over the critical surfaces are presented, and conclusions about the damages and failures for the adhesively-bonded composite SLJ are drawn. [ABSTRACT FROM AUTHOR]


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Determination of slip damping in jointed riveted beams

Built-up structures need to possess an energy dissipation mechanism to damp-out vibrations quickly, which can be achieved effectively by providing joints. Damping in joints is due to the frictional effects associated with relative shear displacements at the interfaces of the connections. This paper presents a finite element approach based on Euler-Bernoulli beam theory to evaluate the damping capacities of cantilever beams of unequal thickness with riveted joints under different dynamic conditions. The solution is based on one-dimensional beam elements, with each element consisting of two nodes with two degrees of freedom, ie. transverse displacement and rotation at each node. The experiments are carried out to authenticate the theory and the results establish that the damping capacity of built-up structures with lower beam thickness ratio and higher cantilever length can be improved substantially using larger diameter rivets undergoing vibration at lower amplitude of excitation. [ABSTRACT FROM AUTHOR]

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On the blast resistance of laminated glass

Abstract: Blast resistant glazing systems typically use laminated glass to reduce the risk of flying glass debris in the event of an explosion. Laminated glass has one or more bonded polymer interlayers to retain glass fragments upon fracture. With good design, the flexibility of the interlayer and the adhesion between layers enable laminated glass to continue to resist blast after the glass layers fracture. This gives protection from significantly higher blast loads when compared to a monolithic pane. Full-scale open-air blast tests were performed on laminated glass containing a polyvinyl butyral (PVB) interlayer. Test windows of size 1.5m×1.2m were secured to robust frames using structural silicone sealant. Blast loads were produced using charge masses of 15kg and 30kg (TNT equivalent) at distances of 10–16m. Deflection and shape measurements of deforming laminated glass were obtained using high-speed digital image correlation. Measurements of loading at the joint, between the laminated glass and the frame, were obtained using strain gauges. The main failure mechanisms observed were the cohesive failure of the bonded silicone joint and delamination between the glass and interlayer at the pane edge. A new finite element model of laminated glass is developed and calibrated using laboratory based tests. Predictions from this model are compared against the experimental results. [Copyright &y& Elsevier]

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