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...

Täydet tiedot

Bibliografiset tiedot
Päätekijät: Korsunsky, A, Song, X, Belnoue, J, Jun, T, Hofmann, F, De Matos, P, Nowell, D, Dini, D, Aparicio-Blanco, O, Walsh, M
Aineistotyyppi: Journal article
Kieli:English
Julkaistu: Elsevier 2009
Aiheet: