Crack tip deformation fields and fatigue crack growth rates in Ti-6Al-4V

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...

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Détails bibliographiques
Auteurs principaux: Korsunsky, A, Song, X, Belnoue, J, Jun, T, Hofmann, F, De Matos, P, Nowell, D, Dini, D, Aparicio-Blanco, O, Walsh, M
Format: Journal article
Langue:English
Publié: Elsevier 2009
Sujets: