Abstract

Weakly clamped uniformly stretched thin elastic plates can experience edge buckling when subjected to a transverse pressure. This situation is revisited here for a circular plate, under the assumption of finite rotations and negligible bending stiffness in the pre-buckling range. The eigenproblem describing this instability is formulated in terms of two singularly perturbed fourth-order differential equations involving the non-dimensional bending stiffness e>0. By using an extension of the asymptotic reduction technique proposed by Coman and Haughton (Acta Mech 55:179–200, 2006), these equations are formally reduced to a simple second-order ordinary differential equation in the limit e→0+. It is further shown that the predictions of this reduced problem are in excellent agreement with the direct numerical simulations of the original bifurcation equations.

Highlights

  • The presence of localised deformations in thin elastic bodies such as bars, plates and shells, tends to signal the existence of lower-dimensional mathematical structures that can capture the underlying physics of such phenomena

  • By re-visiting the recent study [8] regarding the edge-wrinkling of uniformly stretched thin elastic plates subjected to a transverse pressure, we have extended the asymptotic reduction strategy proposed by

  • The relative errors are illustrated on the right

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Summary

Introduction

The presence of localised deformations in thin elastic bodies such as bars, plates and shells, tends to signal the existence of lower-dimensional mathematical structures that can capture the underlying physics of such phenomena. In the present investigation we are motivated to explore the applicability of the aforementioned asymptotic reduction strategy to a rather different edge-wrinkling situation, recently studied by Coman et al [9, 12] within the context of the Foppl-von Karman (FvK) nonlinear plate theory In this new case, a weakly clamped uniformly stretched circular elastic plate is subjected to a transverse pressure; due to the gradual development of compressive stresses near the edge of the plate, for a critical value of the loading the plate experiences a regular wrinkling pattern confined to that region. The paper concludes with a further discussion of the results reported and some remarks on their possible extension

The bifurcation equations
The asymptotic reduction
Concluding remarks
Findings
A Laplace’s Expansion Theorem
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