Ítem
| Bushpalli, Sindhu | |
| 31 maig 2023 | |
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Highly curved composites such as L-angle composite laminates, used at the junction between two perpendicular panels experience unfolding failure. These laminates are typically used in critical components such as aircraft wing spars, hence understanding of their failure mechanisms becomes
crucial. Unfolding failure is typically associated with the interlaminar stresses, eventually leading to sudden delamination, in the curved sections when they are loaded under an opening bending moment. However, depending on the stacking sequences, failure mechanisms experienced in curved composite
laminates, may have different causes. This study addresses the two prominent failure mechanisms occurring in L-shaped composite beams. 7225.mp4 7225.mp3 9 |
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| http://hdl.handle.net/10256.1/7225 | |
| eng | |
| Universitat de Girona. Grup de Recerca en Anàlisi 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 Plàstics reforçats amb fibra de carboni -- Congressos Carbon fiber-reinforced plastics -- Congresses Mecànica de fractura -- Congressos Fracture mechanics -- Congresses Materials compostos -- Fractura -- Congressos Composite materials -- Fracture -- Congresses Materials laminats -- Congressos Laminated materials -- Congresses |
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| Investigation of failure mechanisms in L-angle composite laminates | |
| info:eu-repo/semantics/lecture | |
| DUGiMedia |
