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
โฆ LIBER โฆ
Ductile rupture in thin sheets of two grades of 2024 aluminum alloy
โ Scribed by F Bron; J Besson; A Pineau
- Publisher
- Elsevier Science
- Year
- 2004
- Tongue
- English
- Weight
- 536 KB
- Volume
- 380
- Category
- Article
- ISSN
- 0921-5093
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For transport aircraft with long lifetimes, crack growth data to implement the durability life requirements in the low AK range are needed. This is the region comprising most of the lifetime for the cracks of interest, and it is also the region where there is little data available. Crack growth data