Abstract

This paper deals with the local loss of stability (wrinkling) problem of a thin facing of a sandwich panel. Classical solutions to the problem of a facing instability resting on a homogeneous and isotropic substructure (a core) are compared. The relations between strain energy components associated with different forms of core deformations are discussed. Next, a new solution for the orthotropic core is presented in detail, which is consistent with the classic solution for the isotropic core. Selected numerical examples confirm the correctness of the analytical formulas. In the last part, parametric analyses are carried out to illustrate the sensitivity of wrinkling stress to a change in the material parameters of the core. These analyses illustrate the possibility of using the equations derived in the article for the variability of Poisson’s ratio from −1 to 1 and for material parameters strongly deviating from isotropy.

Highlights

  • As a result of these interactions, the facing can be compressed, and because it is connected to a susceptible substructure, it very often experiences local loss of stability

  • The presented solution for an orthotropic core is based on the work of [7], in which sandwich columns under compression were considered, and the solution was presented in the form of hyperbolic functions

  • We present some relations between the classical solutions to the analyzed problem of wrinkling

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Summary

Introduction

The presented solution for an orthotropic core is based on the work of [7], in which sandwich columns under compression were considered, and the solution was presented in the form of hyperbolic functions. We present some relations between the classical solutions to the analyzed problem of wrinkling We believe that they will shed a slightly different light on known solutions. A parametric analysis of the solution for the orthotropic core is presented, illustrating the sensitivity of the solution (especially the wrinkling stress) to a change in some material parameters. In our opinion, this is essential for the optimal design of layered structures. By assuming certain constraints on material parameters, we can specify a solution with the maximum value or the minimum sensitivity

Formulation of the Problem
Classical Solutions of the Wrinkling Problem
Energy Method—Linear h h l
Differential Equation Method
Comparison
Assumptions and Strain Energy Considerations
16 EC l 2
Differential Equation
Solution of the Differential Equation
Analytical Solutions
Numerical Solutions
Parametric Analysis
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