A two part study was conducted on the effects of hole drilling on the fatigue life of aircraft rivet holes in 2024-T3 aircraft quality aluminum. The first part of the study determined the drilling parameters that had the greatest effect on hole quality. In this, the second part of the study, the fat
Effect of detail design on fatigue performance of fastener hole
β Scribed by J. Liu; H.L. Xu; H.B. Zhai; Z.F. Yue
- Publisher
- Elsevier Science
- Year
- 2010
- Weight
- 606 KB
- Volume
- 31
- Category
- Article
- ISSN
- 0261-3069
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