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
Modelling fatigue crack propagation of a cracked metallic member reinforced by composite patches
β Scribed by Rong Wang; A. Nussbaumer
- Publisher
- Elsevier Science
- Year
- 2009
- Tongue
- English
- Weight
- 449 KB
- Volume
- 76
- Category
- Article
- ISSN
- 0013-7944
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β¦ Synopsis
The concept of fracture for material elements at front of a crack for fatigue crack propagation was extended to the fatigue crack propagation of a cracked metallic member reinforced with a composite patch in this paper. From static mechanics and linear elastic fracture mechanics, force transfer on a cracked member through a composite patch was analyzed and a formula connecting the stress intensity factor with crack length was obtained. Thereafter, a fracture model for fatigue crack propagation of a repaired cracked metallic member was proposed. A new expression for the fatigue crack propagation rate has thus been derived. The expression was verified objectively by the test data. It is in good agreement with the test results.
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