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Journal of Sandwich Structures and Materials
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Buckling Load Design of Sandwich Panels Made with Hybrid Laminated Faces and Transversely Flexible Core

Maria Antonieta Aiello

Department of Innovation Engineering, University of Lecce Via per Arnesano, 73100 Lecce, Italy

Luciano Ombres

Department of Structural Engineering, University of Calabria 87036 Arcavacata di Rende, Italy, l.ombres{at}tin.it

This article presents an analytical approach for evaluating the buckling load of sandwich panels made of hybrid laminated faces and a transversely flexible core. Useful design indications are obtained once the influence of main parameters influencing the structural response is examined. The proposed model is based on a priori assumption of the displacement field through the thickness, which is composed of two sets of modal configurations, one symmetric and one antisymmetric, besides a pure compressive mode. An equivalent `single layer approach', considering all displacement components (u, v, w) that linearly vary across the panel thickness, is used. For simply supported flat sandwich panels subjected to in-plane biaxial and shear loads, the Rayleigh—Ritz method is used to evaluate the buckling loads. Predictions of the proposed model are compared with those obtained by other available theoretical models and with experimental results. Finally, the best arrangement of sandwich panels, corresponding to the maximum buckling loads, is investigated by varying the parameters of both the faces and the core material.

Key Words: buckling • composite • hybrid • sandwich • design.

Journal of Sandwich Structures and Materials, Vol. 9, No. 5, 467-485 (2007)
DOI: 10.1177/1099636207070854


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A.V. Lopatin and E.V. Morozov
Symmetrical Facing Wrinkling of Composite Sandwich Panels
Journal of Sandwich Structures and Materials, November 1, 2008; 10(6): 475 - 497.
[Abstract] [PDF]