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Modelisation and numerical simulation on the residual stress induced by cold expansion of fastener holes located in nickel based superalloy aircraft engine disks

Crossref DOI link: https://doi.org/10.1007/s12289-026-01996-x

Published Online: 2026-03-24

Published Print: 2026-06

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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