Abstract

As at the nanoscale the surface-to-volume ratio may be comparable with any characteristic length, while the material properties may essentially depend on surface/interface energy properties. In order to get effective material properties at the nanoscale, one can use various generalized models of continuum. In particular, within the framework of continuum mechanics, the surface elasticity is applied to the modelling of surface-related phenomena. In this paper, we derive an expression for the effective bending stiffness of a laminate plate, considering the Steigmann–Ogden surface elasticity. To this end, we consider plane bending deformations and utilize the through-the-thickness integration procedure. As a result, the calculated elastic bending stiffness depends on lamina thickness and on bulk and surface elastic moduli. The obtained expression could be useful for the description of the bending of multilayered thin films.

Highlights

  • Nowadays, it is well established that the usual material properties at the nanoscale, such asYoung’s modulus, may significantly differ from what is observed at the macroscale

  • Unlike the Gurtin–Murdoch model, this model explicitly takes into account the surface bending stiffness

  • The derived formula contains various contributions related to the elastic response in the bulk, the influence of the surface Lamé moduli and of the surface bending stiffness moduli

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Summary

Introduction

It is well established that the usual material properties at the nanoscale, such as. In addition to tensional stiffness, there exist various other stiffness parameters such as bending and torsional stiffnesses, known from textbooks on the strength of materials These parameters may characterize the behaviour of thin structures of nanometer size. The aim of this paper is to discuss the bending stiffness of layered nanosized plates. To this end, we consider the classic linear elasticity as a model for material properties in the bulk and the Steigmann–Ogden surface elasticity [9,10] for the modelling of plate faces and interfaces between layers. Let us note tat the surface elasticity models can be treated as a singular case of nonlocality related to the appearance of boundary layers near shell faces.

On the Steigmann–Ogden Surface Elasticity
Laminate Plate
One-Layered Plate with Surface Stresses
Three-Layered Plate with Surface Stresses
N-Layered Plate with Surface Stresses
Discussion and Conclusions
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