Influence of fibre misalignment and voids on composite laminate strength

Influence of fibre misalignment and voids on composite laminate strength

This article studies the effects of manufacturing defects of laminate composite materials on the first ply failure load and ultimate strength of the laminate, which are calculated using finite element modelling with Zinoviev’s damage model. The following types of defects are considered for cross-ply...

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Veröffentlicht in:Journal of composite materials 2015-09, Vol.49 (23), p.2887-2896
Hauptverfasser: Fedulov, BN, Antonov, FK, Safonov, AA, Ushakov, AE, Lomov, SV
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container_issue 23
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container_title Journal of composite materials
container_volume 49
creator Fedulov, BN
Antonov, FK
Safonov, AA
Ushakov, AE
Lomov, SV
description This article studies the effects of manufacturing defects of laminate composite materials on the first ply failure load and ultimate strength of the laminate, which are calculated using finite element modelling with Zinoviev’s damage model. The following types of defects are considered for cross-ply and quasi-isotropic layups: in-plane misalignement and out-of-plane waviness of fibres, misorientation of the layers and void content. The list of laminates studied in this article includes cross-ply and quasi-isotropic layups, loaded in tension and compression in 0°, 90°, 45° and 5° directions. The limits of the first ply failure load and strength degradation for a realistic range of the defect intensities are estimated.
doi_str_mv 10.1177/0021998314557533
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title Influence of fibre misalignment and voids on composite laminate strength
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