FATIGUE CRACK TIP STRAINS IN 7075-T6 ALUMINUM ALLOY
โ Scribed by Gianni Nicoletto
- Book ID
- 109012132
- Publisher
- John Wiley and Sons
- Year
- 1987
- Tongue
- English
- Weight
- 700 KB
- Volume
- 10
- Category
- Article
- ISSN
- 8756-758X
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
Both standard and non-standard compact specimens were employed to experimentally study the crack growth behavior of 7075-T651 aluminum alloy in ambient air. The effects of the stress ratio (R), overloading, underloading, and high-low sequence loading on fatigue crack growth rate were investigated. S
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