In this paper we present an overview of experimental and modelling studies of fatigue crack growth rates in aerospace titanium alloy Ti-6Al-4V. We review work done on the subject since the 1980s to the present day, identifying test programmes and procedures and their results, as well as predictive a
✦ LIBER ✦
Prediction of elevated temperature fatigue crack growth rates in TI-6AL-4V alloy – neural network approach
✍ Scribed by A Fotovati; T Goswami
- Publisher
- Elsevier Science
- Year
- 2004
- Weight
- 382 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0261-3069
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