Bonded composite-patch repair has been used to transfer load from cracked structures to the reinforcement such that subsequent crack propagation is reduced. In this study, the mechanical behavior of a single edge v-notch Al7075-T6 plate repaired with 1-ply and 4-ply composite patches was investigate
A Standard Analysis Methodology for the Stress Analysis of Repaired Aircraft Structures with the Method of Composite Patch Repair
โ Scribed by Z. Marioli-Riga; D. Xenos; Chris Vrettos
- Book ID
- 111569844
- Publisher
- Springer Netherlands
- Year
- 2004
- Tongue
- English
- Weight
- 201 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0929-189X
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
In this study the finite element method is used to analyse the effect of the thermal residual stresses resulting from adhesive curing on the performances of the bonded composite repair in aircraft structures. The stress-intensity factor at the crack tip is chosen as fracture criterion in order to es
The finite element method is carried out to analyse the evolution of the stress intensity factor for cracks repaired with bonded hygrothermal aged composite patches. It is well known that the mechanical characteristics of a laminated composite diminish with the conditioning. In this paper, we use an