FATIGUE CRACK CLOSURE MEASUREMENTS ON 2024-T3 SHEET SPECIMENS
β Scribed by W. Yisheng; J. Schijve
- Book ID
- 118712483
- Publisher
- John Wiley and Sons
- Year
- 2007
- Tongue
- English
- Weight
- 315 KB
- Volume
- 18
- Category
- Article
- ISSN
- 8756-758X
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π SIMILAR VOLUMES
Variable-amplitude fat@ue studies of 2024-13 ab&num alloy were performed to examine the effect of sheet thickness on fatigue crack growth rate retardation. Results indicated tbat the amouot of retardation increased with decreasing specimen thickness. This phenomenon was attrii to enhanced plastic st
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
## 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