| Titre : |
JOINING OF COMPOSITE MATERIALS |
| Type de document : |
texte imprimé |
| Auteurs : |
K.T.Kedward, Auteur |
| Editeur : |
ASTM |
| Importance : |
187p |
| Présentation : |
ill., |
| Format : |
16cmx24cm |
| Langues : |
Français (fre) Langues originales : Anglais (eng) |
| Catégories : |
Généralité:08.Colloque et Conférence
|
| Mots-clés : |
Composite materials Adhesive bonding Mechanical fastening Joint design Stress concentration Delamination . |
| Résumé : |
As advanced composite materials increasingly replace traditional metals in aerospace, automotive, marine, and civil engineering, the technology of joining distinct structural components safely and efficiently remains a critical design challenge. Because composites are inherently anisotropic and lack significant plastic deformation capability to relieve localized stresses, traditional joining techniques often introduce severe stress concentrations and failure initiation sites. This comprehensive overview addresses the fundamental principles, failure mechanisms, and design methodologies associated with primary joining strategies: mechanical fastening, adhesive bonding, and emerging thermal/fusion welding methods. Special emphasis is placed on surface preparation, stress distribution analysis, environmental durability, non-destructive evaluation, and the mechanical behavior of hybrid joints connecting composites to metals or other dissimilar materials. |
JOINING OF COMPOSITE MATERIALS [texte imprimé] / K.T.Kedward, Auteur . - ASTM, [s.d.] . - 187p : ill., ; 16cmx24cm. Langues : Français ( fre) Langues originales : Anglais ( eng)
| Catégories : |
Généralité:08.Colloque et Conférence
|
| Mots-clés : |
Composite materials Adhesive bonding Mechanical fastening Joint design Stress concentration Delamination . |
| Résumé : |
As advanced composite materials increasingly replace traditional metals in aerospace, automotive, marine, and civil engineering, the technology of joining distinct structural components safely and efficiently remains a critical design challenge. Because composites are inherently anisotropic and lack significant plastic deformation capability to relieve localized stresses, traditional joining techniques often introduce severe stress concentrations and failure initiation sites. This comprehensive overview addresses the fundamental principles, failure mechanisms, and design methodologies associated with primary joining strategies: mechanical fastening, adhesive bonding, and emerging thermal/fusion welding methods. Special emphasis is placed on surface preparation, stress distribution analysis, environmental durability, non-destructive evaluation, and the mechanical behavior of hybrid joints connecting composites to metals or other dissimilar materials. |
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