Abstract

This work deals with the modeling of laminated composite and sandwich shells through a variable separation approach based on a Reissner’s Variational Mixed Theorem (RMVT). Both the displacement and transverse stress fields are approximated as a sum of products of separated functions of the in-plane coordinates and the transverse coordinate. This approach yields to a non-linear problem that is solved by an iterative process, in which 2D and 1D problems are separately considered at each iteration. In the thickness direction, a fourth-order expansion in each layer is used. For the in-plane description, classical Finite Element method is used. Numerical examples involving several representative shell configurations (deep/shallow, thick/thin) are addressed to show the accuracy of the present method. It is shown that it can provide quasi-3D results less costly than classical LW computations. In particular, the estimation of the transverse stresses, which are of major importance for damage analysis, is very good.

Highlights

  • Composite shells are widely used in the industrial field due to their excellent mechanical properties, especially their high specific stiffness and strength

  • Application of the proper generalized decomposition to the cylindrical shell we develop the application of the Proper Generalized Decomposition (PGD) for shell analysis with a mixed formulation

  • Few iterations are required to reach the convergence of the fixed point algorithm

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Summary

Introduction

Composite shells are widely used in the industrial field (aerospace, automotive, marine, medical industries...) due to their excellent mechanical properties, especially their high specific stiffness and strength. Some of these works are based on a linear distribution of the in-plane displacements through each layer, without taking into account the transverse normal stress. While the above references propose models still relying on the 2D constitutive law, the papers [35,36] extend the zig–zag approach to include the transverse normal stress.

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