| Article ID | Journal | Published Year | Pages | File Type | 
|---|---|---|---|---|
| 7889980 | Composites Part A: Applied Science and Manufacturing | 2018 | 14 Pages | 
Abstract
												Un-notched and notched tensile response and damage accumulation of quasi-isotropic carbon/epoxy hybrid laminates made of ultra-high modulus and intermediate modulus carbon fibre/epoxy thin-ply prepregs were studied. It was confirmed that the ply fragmentation demonstrated previously in unidirectional hybrids as a successful pseudo-ductility mechanism can be transferred to multi-directional laminates. Furthermore, reduced notch sensitivity was demonstrated in quasi-isotropic specimens for both open holes and sharp notches as a result of local ply fragmentation around the notch.
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													Physical Sciences and Engineering
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											Authors
												Gergely Czél, Tamas Rev, Meisam Jalalvand, Mohamad Fotouhi, Marco L. Longana, Oliver J. Nixon-Pearson, Michael R. Wisnom, 
											