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
β¦ LIBER β¦
PREDICTION OF FATIGUE CRACK GROWTH UNDER SINGLE OVERLOAD APPLICATION IN Ti-6Al-4V
β Scribed by H. Ghonem; M. Zeng
- Book ID
- 109012345
- Publisher
- John Wiley and Sons
- Year
- 1991
- Tongue
- English
- Weight
- 601 KB
- Volume
- 14
- Category
- Article
- ISSN
- 8756-758X
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