Fatigue delamination behaviour of unidirectional carbon fibre/epoxy laminates reinforced by Z-Fiber® pinnin

dc.contributor.authorCartié, Denis D. R.-
dc.contributor.authorLaffaille, J-M-
dc.contributor.authorPartridge, Ivana K.-
dc.contributor.authorBrunner, A. J.-
dc.date.accessioned2011-09-29T17:19:24Z
dc.date.available2011-09-29T17:19:24Z
dc.date.issued2009-12-31T00:00:00Z-
dc.description.abstract-Pin reinforced carbon-fibre epoxy laminates were tested under Mode I and Mode II conditions, both quasi-statically and in fatigue. Test procedures were adapted from existing standard or pre-standard tests. Samples containing 2% and 4% areal densities of carbon-fibre Z-pins (0.28mm diameter) were compared with unpinned laminates. Quasi-static tests under displacement control yielded a dramatic increase of the apparent delamination resistance. Specimens with 2% pin density failed in Mode I at loads 170N, equivalent to an apparent GIC of 2kJ/m2. Fatigue testing under load control showed that the presence of the through- thickness reinforcement slowed down fatigue delamination propagation.en_UK
dc.identifier.issn0013-7944-
dc.identifier.urihttp://dx.doi.org/10.1016/j.engfracmech.2009.07.018-
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/5642
dc.publisherElsevier Science B.V., Amsterdam.en_UK
dc.titleFatigue delamination behaviour of unidirectional carbon fibre/epoxy laminates reinforced by Z-Fiber® pinninen_UK
dc.typeArticle-

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