Article ID Journal Published Year Pages File Type
822270 Composites Science and Technology 2006 10 Pages PDF
Abstract

In this study, the effects of the boundary conditions on the out-of-plane displacements and through-the-thickness strain distribution of symmetric composite laminated plates are reported. The plates are subjected to bending by a central force and supported by two-line or four-point supports. The out-of-plane displacement field is measured using a full field electronic speckle pattern interferometry technique and the through-the-thickness distribution of the deformations by fibre Bragg gratings, embedded at selected locations during preparation of the plates. The experimental data are correlated with the results from elasticity-based 2D and 3D finite element models of the actual experimental configuration. The results clearly exhibit the effects of the boundary conditions on the deformation behaviour of the plates. Non-linear through-the-thickness strain distributions appear in the thick plate range. Aspects such as force and displacement distributions on the contact areas of both loading and supports are also considered.

Related Topics
Physical Sciences and Engineering Engineering Engineering (General)
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