In this study, finite element method is used to investigate crack propagation of stiffened aluminum panels repaired with composite patches. For this purpose, 3-D crack-front in general mixed-mode conditions is considered for the analyses. The cracks are considered to be near the stiffener around a r
โฆ LIBER โฆ
Fatigue Debonding Analysis of Repaired Aluminium Panels by Composite Patch using Interface Elements
โ Scribed by Hossein Hosseini-Toudeshky; Ali Jasemzadeh; Bijan Mohammadi
- Publisher
- Springer Netherlands
- Year
- 2011
- Tongue
- English
- Weight
- 872 KB
- Volume
- 18
- Category
- Article
- ISSN
- 0929-189X
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In this paper, fatigue crack growth of repaired thick aluminium panels containing a central inclined crack is studied. The cracked panels were repaired on one side with glass/epoxy composite patches. Effects of patch lay-up configuration on starting the crack growth after bonding and crack growth ra