Effect of Localized Corrosion on Fatigue–Crack Growth in 2524-T3 and 2198-T851 Aluminum Alloys Used as Aircraft Materials
Crossref DOI link: https://doi.org/10.1007/s11665-018-3244-7
Published Online: 2018-03-01
Published Print: 2018-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Moreto, J. A.
Broday, E. E.
Rossino, L. S.
Fernandes, J. C. S.
Bose Filho, W. W.
Text and Data Mining valid from 2018-03-01
Article History
Received: 12 September 2017
Revised: 5 December 2017
First Online: 1 March 2018