| Author | Search for: Li, Chun1; Search for: Teng, Tim1; Search for: Wan, Zhong Yi1; Search for: Young, Neell G.1; Search for: Li, Gang1; Search for: Rans, Calvin; Search for: LaPlante, Gabriel |
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| Affiliation | - National Research Council of Canada. Aerospace
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| Format | Text, Article |
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| Conference | SAMPE Technical Conference, June 2-5, 2014, Seattle, Washington |
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| Subject | 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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| Abstract | 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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| Publication date | 2015-06-05 |
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| In | |
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| Language | English |
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| Peer reviewed | Yes |
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| NPARC number | 21275918 |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | b8c0c947-7081-46c2-a28d-e326c123e266 |
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| Record created | 2015-08-05 |
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| Record modified | 2020-04-22 |
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