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Geometrically nonlinear analysis for some axially compressed laminated cylindrical panels

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Abstract

Mainly, this paper deals with cylindrical laminated panels, axially compressed under the constraint of four simply-supported edges.

By imposing uniform increasing end-shortening to the two opposite circular edges, characteristic equilibrium paths have been obtained in correspondence to numerical evaluations with finite element models subject to geometric non linearity. A peculiar link among different branches of the total path, each of which is connected to a proper deformed configuration, is pointed out in the axial load/end-shortening space.

Convergence problems and mesh sensibility are also examined.

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Calì, C., Esposito, R., Graziano, M. et al. Geometrically nonlinear analysis for some axially compressed laminated cylindrical panels. Appl Compos Mater 1, 301–316 (1994). https://doi.org/10.1007/BF00568286

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  • DOI: https://doi.org/10.1007/BF00568286

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