| Auteur | Rechercher : Li, Chun1; Rechercher : Teng, Tim1; Rechercher : Wan, Zhong Yi1; Rechercher : Young, Neell G.1; Rechercher : Li, Gang1; Rechercher : Rans, Calvin; Rechercher : LaPlante, Gabriel |
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| Affiliation | - Conseil national de recherches du Canada. Aérospatiale
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| Format | Texte, Article |
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| Conférence | SAMPE Technical Conference, June 2-5, 2014, Seattle, Washington |
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| Sujet | aircraft manufacture; airframes; failure modes; fracture toughness; joints (structural components); repair; adhesively bonded composite joints; bonded composite joints; composite aircraft structure; critical fracture toughness; fatigue performance; growth characteristic; loading condition; part manufacturing |
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| Résumé | Adhesive bonding has been increasingly used for part manufacturing and repair of composite aircraft structures. This work focuses on static and fatigue performance of bonded composite joints under mixed mode I/II loading. A series of experiments was performed on bonded composite joint specimens with load mixities (GII/G) of 0, 0.2, 0.4, 0.6 and 0.8. The experimental results show a change in critical fracture toughness and fatigue disbond growth characteristics with load mixity. Failure analysis indicates that these changes are not only attributable to the loading conditions, but they are also affected by failure modes |
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| Date de publication | 2015-06-05 |
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| Dans | |
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| Langue | anglais |
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| Publications évaluées par des pairs | Oui |
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| Numéro NPARC | 21275918 |
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| Exporter la notice | Exporter en format RIS |
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| Signaler une correction | Signaler une correction (s'ouvre dans un nouvel onglet) |
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| Identificateur de l’enregistrement | b8c0c947-7081-46c2-a28d-e326c123e266 |
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| Enregistrement créé | 2015-08-05 |
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| Enregistrement modifié | 2020-04-22 |
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