Fatigue Life Enhancement of a D16at Aluminum Alloy for Aircraft Components with Fastener Holes
Crossref DOI link: https://doi.org/10.1007/s11223-020-00144-3
Published Online: 2020-04-21
Published Print: 2020-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Duncheva, G. V.
Maximov, J. T.
Ganev, N.
Anchev, A. P.
Text and Data Mining valid from 2020-01-01
Version of Record valid from 2020-01-01
Article History
Received: 18 May 2018
First Online: 21 April 2020