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 ✦
Non-closure of cracks and fatigue crack growth in β heat treated Ti-6A1-4V
✍ Scribed by M. D. Halliday; C. J. Beevers
- Publisher
- Springer Netherlands
- Year
- 1979
- Tongue
- English
- Weight
- 256 KB
- Volume
- 15
- Category
- Article
- ISSN
- 1573-2673
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