Effect of Curing Cycle on Fatigue Life of Cracked AA7075-T6 Aircraft Sheet Repaired with a Boron/Epoxy Composite Patch
Crossref DOI link: https://doi.org/10.1007/s40997-020-00400-6
Published Online: 2020-10-16
Published Print: 2022-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Khodja, Malika
Fekirini, Hamida http://orcid.org/0000-0001-6013-9977
Govender, Gonasagren
Bachir Bouiadjra, Belabbes
Text and Data Mining valid from 2020-10-16
Version of Record valid from 2020-10-16
Article History
Received: 7 February 2020
Accepted: 26 September 2020
First Online: 16 October 2020