Delamination of Z-pinned carbon fibre reinforced laminates

dc.contributor.authorDenis, D. R.-
dc.contributor.authorCartiƩ, Manos Troulis-
dc.contributor.authorPartridge, Ivana K.-
dc.date.accessioned2011-04-14T23:02:03Z
dc.date.available2011-04-14T23:02:03Z
dc.date.issued2005-05-17T00:00:00Z-
dc.description.abstractThe paper outlines the current status of mechanical testing, identification of failure mechanisms and data analysis related to delamination cracking in high performance laminates made via the prepreg/autoclave route, strengthened in the through-thickness direction by Z-pinning. The applied loading cases under consideration are limited to Mode I and Mode II. Sample preparation, test methodologies and applicability of data reduction schemes are considered, with data obtained from within the range of aerospace and Formula 1 grades of carbon fibre / epoxy composites. Micromechanisms of failure in the three dimensional tests specimens are shown to be dependent on the architecture of the fibre reinforcement (i.e. unidirectional versus woven fabric prepregs), particularly in the case of Mode II loading.en_UK
dc.identifier.citationDenis D.R. Cartie, Manos Troulis and Ivana K. Partridge, Delamination of Z-pinned carbon fibre reinforced laminates, Composites Science and Technology, Volume 66, Issue 6, Advances in statics and dynamics of delamination, May 2006, Pages 855-861.en_UK
dc.identifier.issn0266-3538-
dc.identifier.urihttp://dx.doi.org/10.1016/j.compscitech.2004.12.018-
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/851
dc.language.isoen_UKen_UK
dc.publisherElsevier Science B.V., Amsterdam.en_UK
dc.titleDelamination of Z-pinned carbon fibre reinforced laminatesen_UK
dc.typeArticleen_UK

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