4.7 Article

A von Karman-type model for two-layer laminated glass plates, with applications to buckling and free vibration under in-plane edge loads

Journal

COMPOSITE STRUCTURES
Volume 322, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2023.117287

Keywords

Laminated glass; Two-layer plates; Partial shear interaction; vonK'arm'an plate theory; Mindlin plate theory; Flexural buckling and vibration

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This article presents a geometrically nonlinear two-dimensional model for the undamped dynamical response of thin two-layer plates with partial shear interaction. The model is tailored for analyzing laminated glass plates commonly used in building structures. The model is used to study the flexural buckling and free vibration of two-layer plates under in-plane edge loads, and analytical solutions are obtained for different boundary conditions. A conforming rectangular finite element method is also proposed and shown to be effective for approximation.
This article presents a layerwise geometrically nonlinear two-dimensional model for the undamped dynamical response of thin two-layer plates with partial shear interaction. The model is tailored for the analysis of lami-nated glass plates of the type most commonly used in building structures (two glass layers bonded by a polymeric interlayer). The geometrical nonlinearities are introduced via the so-called von K'arm'an strains. The process of dimensional reduction is based on Podio-Guidugli's method of internal constraints. An unconventional choice of generalised displacements highlights several direct similarities with the single-layer plate theories of von K'arm'an and Mindlin. The model is used to study the flexural buckling and free vibration of two-layer plates under in-plane edge loads. Analytical solutions are obtained for rectangular plates with (i) all edges simply supported without shear restraint and (ii) a two-parameter system of uniform in-plane normal edge loads. These solutions degenerate into those of single-layer von K'arm'an plates in the two limiting cases of zero and full shear interaction. A conforming rectangular finite element is formulated and shown to perform effectively. When using uniform meshes, the observed asymptotic rate of convergence for the finite element approximation of the lowest buckling load and vibration frequency is quadratic.

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