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| Élément Dublin Core | Valeur | Langue |
|---|---|---|
| dc.contributor.author | Achache, Habib | - |
| dc.date.accessioned | 2020-01-22T11:42:53Z | - |
| dc.date.available | 2020-01-22T11:42:53Z | - |
| dc.date.issued | 2017 | - |
| dc.identifier.issn | 2367-8992 | - |
| dc.identifier.uri | https://ds.univ-oran2.dz:8443/jspui/handle/123456789/2875 | - |
| dc.description.abstract | Our work aims to analyze using the finite element method the evolution of the stress intensity factor (SIF) parameter K of three laminated folded plates stacks [+ α, -α], made of the same epoxy matrix and different reinforcement fibe rs (boron, graphite and glass). Our results show that the angle of orientation of the boron / epoxy composite has no great influence on the variation of the parameter K KI. Compared to composite graphite / epoxy and glass / epoxy, the laminated composite bor on / epoxy reduces more the SIF K KI in the middle of the plate for angles 0 ° ≤α≤30 °. | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | International Journal of Theoretical and Applied Mechanics | en_US |
| dc.subject | Cracks , delamination, stress intensity factor, fibers orientations, finite element method and laminateslaminates. | en_US |
| dc.title | Delamination of a Composite Laminated under Monotonic Loading | en_US |
| dc.type | Article | en_US |
| dc.number.totalPage | 10 | en_US |
| Collection(s) : | 6.Institut de Maintenance et de Sécurité Industrielle | |
Fichier(s) constituant ce document :
| Fichier | Description | Taille | Format | |
|---|---|---|---|---|
| article Delamination of a Composite Laminated under Monotonic Loading-Habib Achache | 1,91 MB | Unknown | Voir/Ouvrir |
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