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Development of a Damage Analysis Method in Laminated Composites Using Finite Fracture Toughness of Single Lamina

โœ Scribed by Farrokhabadi, Amin; Hosseini-Toudeshky, Hossein; Mohammadi, Bijan


Book ID
127328856
Publisher
Taylor and Francis Group
Year
2013
Tongue
English
Weight
740 KB
Volume
20
Category
Article
ISSN
1537-6494

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An assumed hybrid-stress finite element model incorporating two types of modified composite multilayer elements (MLTUP and MLTPH) is developed to investigate the free vibration of doubly and singly patched cracked laminates. Three-dimensional stresses of the laminated panel, patch and adhesive are a