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.
Related Topics
Physical Sciences and Engineering
Materials Science
Ceramics and Composites
Authors
Gergely Czél, Tamas Rev, Meisam Jalalvand, Mohamad Fotouhi, Marco L. Longana, Oliver J. Nixon-Pearson, Michael R. Wisnom,