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A four node Marguerre element for non‐linear shell analysis

Philippe Jetteur (IREM, Department of Civil Engineering, Swiss Federal Institute of Technology, CH‐1015 Lausanne, Switzerland)
François Frey (IREM, Department of Civil Engineering, Swiss Federal Institute of Technology, CH‐1015 Lausanne, Switzerland)

Engineering Computations

ISSN: 0264-4401

Article publication date: 1 April 1986

136

Abstract

A non‐linear shallow thin shell element is described. The element is a curved quadrilateral one with corner nodes only. At each node, six degrees of freedom (i.e. three translations and three rotations) make the element easy to connect to space beams, stiffeners or intersecting shells. The curvature is dealt with by Marguerre's theory. Membrane bending coupling is present at the element level and improves the element behaviour, especially in non‐linear analysis. The element converges to the deep shell solution. The sixth degree of freedom is a true one, which can be assimilated to the in‐plane rotation. The present paper describes how overstiffness due to membrane locking on the one hand and to the sixth degree of freedom on the other hand can be corrected without making use of numerical adjusted factors. The behaviour of this new element is analysed in linear and non‐linear static and dynamic tests.

Citation

Jetteur, P. and Frey, F. (1986), "A four node Marguerre element for non‐linear shell analysis", Engineering Computations, Vol. 3 No. 4, pp. 276-282. https://doi.org/10.1108/eb023667

Publisher

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MCB UP Ltd

Copyright © 1986, MCB UP Limited

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