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Fatigue crack propagation in Ti–6Al–4V subjected to high strain amplitudes

✍ Scribed by M. ANDERSSON; T. HANSSON; C. PERSSON; S. MELIN

Book ID
109014042
Publisher
John Wiley and Sons
Year
2005
Tongue
English
Weight
144 KB
Volume
28
Category
Article
ISSN
8756-758X

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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