| Titre : |
Numerical simulation of asymmetric composite patch repair for fatigue damaged aluminum plate |
| Type de document : |
texte imprimé |
| Auteurs : |
Belaid Salim, Auteur ; Babaghayou Meriam Imane, Auteur ; Maati Ahmed, Auteur |
| Année de publication : |
2023 |
| Article en page(s) : |
p. 329-338 |
| Note générale : |
Bibliogr. |
| Langues : |
Anglais (eng) |
| Catégories : |
Aluminium -- Alliages
Bore
Colles:Adhésifs
Composites
Eléments finis, Méthode des
Epoxydes
Graphite
Matériaux -- Fatigue
Matériaux -- Fissuration
Patchs de réparation
Rupture (mécanique)
Simulation par ordinateur
|
| Index. décimale : |
668.4 Plastiques, vinyles |
| Résumé : |
Repairing structures damaged by fatigue through the use of composite patch bonding is an efficient and economical process to preserve structures and increase their lifespan. Much work is currently being carried out to improve this technique. In this work, a 3D nonlinear numerical simulation by finite element analysis was carried out to study the behavior of the crack front and determine the evolution of the stress intensity factor and the change of stress with respect to distance from the crack point. for an aluminum alloy plate containing a central crack, repaired asymmetrically with a composite patch. The repair of these plates must be more precise and reinforced around the crack point, therefore the stress are high and the stress integrity factor SIF is more important according to the results of this study. |
| Note de contenu : |
- LITERATURE REVIEW : Structural repair methods, composite patch bonding - Parameter of the break
- METHODOLOGY : Software and simulation steps - Presentation of geometric models - The mesh module
- RESULTS AND DISCUSSION : Crack behavior analysis - Effect of the mechanical properties of the adhesive - Boron/Epoxy patch simulation - Simulations Graphite/Epoxy - Patch results Stress variation during crack propagation
- Table 1 : Dimensions and material properties of the repaired model
- Table 2 : S11 and S-Mises stress along the path in the case of Boron/Epoxy patch
- Table 3 : S11 and S-Mises along the path in the case of Graphite/Epoxy |
| En ligne : |
https://www.iieta.org/download/file/fid/113375 |
| Format de la ressource électronique : |
Pdf |
| Permalink : |
https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=40529 |
in REVUE DES COMPOSITES ET DES MATERIAUX AVANCES > Vol. 33, N° 5 (10/2023) . - p. 329-338
Aller sur edunet
Accueil
Ajouter le résultat dans votre panier Affiner la rechercheNumerical simulation of asymmetric composite patch repair for fatigue damaged aluminum plate / Belaid Salim in REVUE DES COMPOSITES ET DES MATERIAUX AVANCES, Vol. 33, N° 5 (10/2023)
