Abstract
Un-notched and notched tensile response and damage accumulation of quasi-isotropic carbon/epoxy hybrid laminates were studied. It was confirmed that ply fragmentation demonstrated previously as a successful ductility mechanism can be transferred to multi-directional laminates. Furthermore, notch-insensitivity was demonstrated by locally active fragmentation in notched quasi-isotropic specimens.
Original language | English |
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Title of host publication | ECCM 2016 - Proceeding of the 17th European Conference on Composite Materials |
ISBN (Electronic) | 9783000533877 |
Publication status | Published - 2016 |
Event | 17th European Conference on Composite Materials, ECCM 2016 - Munich, Germany Duration: 26 Jun 2016 → 30 Jun 2016 |
Conference
Conference | 17th European Conference on Composite Materials, ECCM 2016 |
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Country/Territory | Germany |
City | Munich |
Period | 26/06/16 → 30/06/16 |
Keywords
- carbon/epoxy
- pseudo-ductility
- quasi-isotropic