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EnglishThe influence of through-thickness reinforcement on Mode II delamination fracture in composite laminates is investigated. The bridging traction law, which characterizes the toughening mechanisms due to the through-thickness reinforcement, is deduced from crack profile measurements in End Notched Flexure specimens. The problem is solved through an inverse formulation of a bridged-crack model based on bending theory for anisotropic plates.
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| Titolo: | Interlaminar fracture of laminates with through-thickness reinforcement |
| Autori: | |
| Data di pubblicazione: | 1998 |
| Abstract: | The influence of through-thickness reinforcement on Mode II delamination fracture in composite laminates is investigated. The bridging traction law, which characterizes the toughening mechanisms due to the through-thickness reinforcement, is deduced from crack profile measurements in End Notched Flexure specimens. The problem is solved through an inverse formulation of a bridged-crack model based on bending theory for anisotropic plates. |
| Handle: | http://hdl.handle.net/11567/393043 |
| ISBN: | 0792348958 |
| Appare nelle tipologie: | 04.01 - Contributo in atti di convegno |
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http://hdl.handle.net/11567/393043
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