Buckling strength improvements for Fibre Metal Laminates using thin-ply tailoring

Mania, R. J. and York, C. B. (2017) Buckling strength improvements for Fibre Metal Laminates using thin-ply tailoring. Composite Structures, 159, pp. 424-432. (doi: 10.1016/j.compstruct.2016.09.097)

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Abstract

The buckling response and load carrying capacity of thin-walled open cross-section profiles made of Fibre Metal Laminates, subjected to static axial compression loading are considered. These include thin-walled Z-shape and channel cross-section profiles adopting a 3/2 FML lay-up design, made of 3 aluminium layers. The objective of the investigation is the comparison of standard thickness Fibre Reinforced Plastic layers versus thin-ply material technology. Whilst thin ply designs differ only by the layer thickness, they offer an exponential increase in stacking sequence design freedoms, allowing detrimental coupling effects to be eliminated. The benefit of different hybrid materials are also considered. The comparisons involve semi-analytical and finite element methods, which are validated against experimental investigations.

Item Type:Articles
Status:Published
Refereed:Yes
Glasgow Author(s) Enlighten ID:York, Dr Christopher
Authors: Mania, R. J., and York, C. B.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
Journal Name:Composite Structures
Publisher:Elsevier
ISSN:0263-8223
ISSN (Online):1879-1085
Published Online:30 September 2016
Copyright Holders:Copyright © 2016 Elsevier
First Published:First published in Composite Structures 159:424-432
Publisher Policy:Reproduced in accordance with the copyright policy of the publisher

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