A fibre direction compressive failure criterion for long fibre laminates at ply scale,including stacking sequence and laminate thickness effects |
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Authors: | J-C Grandidier P Casari C Jochum |
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Affiliation: | 1. Département de Physique et Mécanique des Matériaux, Institut P′, UPR 3346, ENSMA, 1 Avenue Clément Ader, F-86961 Chasseneuil, Futuroscope, France;2. Institut de Recherche en Génie Civil et Mécanique (GeM), 58 rue Michel Ange, BP 420, F-44606 Saint Nazaire Cedex, France;3. Centre de Recherche en Mécanique des Structures Navales, Laboratoire LBMS-EA 4325, ENSTA Bretagne, 2 rue François Verny, F-29806 Brest Cedex 9, France |
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Abstract: | Long fibre laminate compressive failure is due to a microbuckling instability which leads to a kink band and a brittle failure of the fibres. This failure mechanism is well known, but more or less pertinently explained in the literature. Some references also showed that local microbuckling instability depends on parameters that belong to the scale of the elementary ply, like thickness and corresponding lay-up. The compressive strength of the unidirectional ply is therefore no more an intrinsic material property, but results from a structural effect of the design. In this paper, the so-called “structure effect” is included in a simple way as an analytical formula in the phenomenological compressive failure criterion which was initially presented by Budiansky and Fleck works. The criterion presented is expressed analytically for unidirectional composite and stands for the local compressive failure strength at ply scale in fibres direction. |
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Keywords: | Laminates Microbuckling Compressive strength Structural effect |
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