Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/117527
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dc.contributorDepartment of Industrial and Systems Engineering-
dc.creatorWang, X-
dc.creatorShi, Z-
dc.creatorLin, J-
dc.date.accessioned2026-02-26T03:46:38Z-
dc.date.available2026-02-26T03:46:38Z-
dc.identifier.issn0921-5093-
dc.identifier.urihttp://hdl.handle.net/10397/117527-
dc.language.isoenen_US
dc.publisherElsevier BVen_US
dc.rights© 2025 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY license ( http://creativecommons.org/licenses/by/4.0/ ).en_US
dc.rightsThe following publication Wang, X., Shi, Z., & Lin, J. (2025). Deformation, strength and corrosion resistance evolutions of AA7475 under creep-ageing with various pre-treatments. Materials Science and Engineering: A, 948, 149278 is available at https://doi.org/10.1016/j.msea.2025.149278.en_US
dc.subjectAA7475en_US
dc.subjectCorrosion resistanceen_US
dc.subjectCreep deformationen_US
dc.subjectCreep-ageingen_US
dc.subjectMicrostructural evolutionen_US
dc.subjectStrength evolutionen_US
dc.titleDeformation, strength and corrosion resistance evolutions of AA7475 under creep-ageing with various pre-treatmentsen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume948-
dc.identifier.doi10.1016/j.msea.2025.149278-
dcterms.abstractMulti-step ageing has been developed as a novel treatment for 7xxx aluminium alloys to achieve both high strength and superior corrosion resistance. When creep-ageing these multi-step aged Al-Zn-Mg-Cu alloys to fabricate large scale aerospace components, however, effective strategies to enhance their creep deformation while maintaining a satisfactory balance between strength and corrosion resistance remain lacking. This study systemically investigated the evolution of deformation, strength and corrosion resistance during creep-ageing of a multi-aged AA7475 with various pre-treatments including stress-free and stressed pre-ageing. The effects of the pre-treatments on the material behaviour were examined through uniaxial creep-ageing and subsequent tensile tests, intergranular corrosion (IGC) tests, and corresponding microstructural investigations. It was found that during the creep-ageing process, the creep deformation was promoted, while the strength and corrosion resistance were reduced in the pre-treated specimens when compared to the as-received material. Specifically, the tensile creep aged (TCA) pre-treated specimens exhibited the largest reduction in material strength, while those with pre-aged initial state have the most decrease in corrosion resistance. Creep-ageing of materials in various initial states led to the increase in grain boundary precipitate (GBP) size and precipitate free zone (PFZ) width to varying extents, as well as diverse distributions of precipitates along grain boundaries, which exerted substantial effects on the deformation, strength evolution, and corrosion resistance of the material. This study provides valuable insights into developing feasible treatment strategies to improve creep deformation and enhance creep-ageing efficiency in high strength Al-Zn-Mg-Cu alloys, while maintaining an optimal balance between strength and corrosion resistance of the material.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationMaterials science and engineering. A, Structural materials : properties, microstructure and processing, Dec. 2025, v. 948, 149278-
dcterms.isPartOfMaterials science and engineering. A, Structural materials : properties, microstructure and processing-
dcterms.issued2025-12-
dc.identifier.scopus2-s2.0-105018943694-
dc.identifier.eissn1873-4936-
dc.identifier.artn149278-
dc.description.validate202602 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOSen_US
dc.description.fundingSourceSelf-fundeden_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryCCen_US
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