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- W4211120611 abstract "Externally bonded composite repairs have recently been shown to be an effective technique for repairing a range of structural problems associated with cracked or damaged aircraft components, including multi-site damage in cracked fuselage lap-joints. This paper attempts to further clarify the mechanisms by which these repairs work. The results are presented of a combined numerical and experimental investigation into the use of bonded repairs for a load-bearing hole containing a single “through-thickness” crack. The specimen was repaired with bonded boron/epoxy doublers and a steel sleeve insert. Constant amplitude fatigue tests were performed, on both the repaired and unrepaired specimens, and the resultant fatigue-crack-growth data are presented. This crack-growth data is then correlated with the stress intensity factors obtained from a three-dimensional finite element analysis." @default.
- W4211120611 created "2022-02-13" @default.
- W4211120611 date "1995-04-01" @default.
- W4211120611 modified "2023-09-25" @default.
- W4211120611 title "Thermographic examination of fatigue exercise on high strength pressure vessel Huang, Y., Lin, X.R., Xu, J., Li, S.X. and Li, W. Acta Metall. Sin. (China) (18 May 1994) 30 (5), A2252A231 (in Chinese)" @default.
- W4211120611 doi "https://doi.org/10.1016/0142-1123(95)98958-6" @default.
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