Influence of applied stress ratio on fatigue crack growth in 6063-T6 aluminium alloy
โ Scribed by Raghuvir Kumar; S.B.L Garg
- Publisher
- Elsevier Science
- Year
- 1985
- Tongue
- English
- Weight
- 721 KB
- Volume
- 20
- Category
- Article
- ISSN
- 0308-0161
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
Crack propagation experiments were performed on a mild steel side edge notched specimen for various load ranges and stress ratios at constant maximum loads. The life of the specimen increased as the load ratio increased. The crack growth data were analysed in terms of AKeff as a function of stress r
The interaction between residual stress and fatigue crack growth rate has been investigated in middle tension and compact tension specimens machined from a variable polarity plasma arc welded aluminium alloy 2024-T351 plate. The specimens were tested at three levels of applied constant stress intens