Fatigue crack growth retardation assessment of 2024-T3 and 6061-T6 aluminium specimens
โ Scribed by Sp.G. Pantelakis; Th.B. Kermanidis; D.G. Pavlou
- Book ID
- 107919630
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 413 KB
- Volume
- 22
- Category
- Article
- ISSN
- 0167-8442
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๐ SIMILAR VOLUMES
## Experimental investigations have been carried out to study the effect of specimen configuration and loading history on the crack growth behaviour of 2024-T3 aluminium alloy at room temperature. It has been observed that fatigue crack growth rate in specimens loaded symmetrically is higher than
The purpose of this research was to compare the resistance to the onset of multi-site damage in thin 2024-T3 and 2524-T3 sheet. Aluminum alloy 2524-T3 is a relatively new fuselage skin sheet material that may offer improved performance with respect to the onset of multi-site damage. The alloys were