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| Carraro, Paolo Andrea | |
| 2023 May 31 | |
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The fatigue life of multi-directional composite laminates is characterised, in the earlier stages, by the initiation and propagation of multiple off-axis cracks. These cracks involve the entire ply thickness and propagate along the fibre direction. In a schematic geometrical representation, thus, the crack
faces belong to the 1-3 plane, where 1 is the fibre direction and 3 is the through-the-thickness direction. 7244.mp4 7244.mp3 9 |
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| http://hdl.handle.net/10256.1/7244 | |
| eng | |
| Universitat de Girona. Grup de Recerca en Anà lisi i Materials Avançats per al Disseny Estructural (AMADE) | |
| CompTest 2023 | |
| Attribution-NonCommercial-ShareAlike 4.0 International | |
| http://creativecommons.org/licenses/by-nc-sa/4.0/ | |
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Assaigs de materials -- Congressos
Materials -- Testing -- Congresses Resistència de materials -- Congressos Strength of materials -- Congresses Plà stics reforçats amb fibra de carboni -- Congressos Carbon fiber-reinforced plastics -- Congresses Mecà nica de fractura -- Congressos Fracture mechanics -- Congresses Materials compostos -- Fractura -- Congressos Composite materials -- Fracture -- Congresses Materials laminats -- Congressos Laminated materials -- Congresses |
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| Comparison between the inter- and intra-laminar fatigue crack propagation as obtained from DCB and cross-ply specimens | |
| info:eu-repo/semantics/lecture | |
| DUGiMedia |
