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Effect of Superplastic Forming Exposure on Fatigue Crack Propagation Behavior of Ti-6Al-4V Alloy

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dc.contributor.authorJeong, Daeho-
dc.contributor.authorKwon, Yongnam-
dc.contributor.authorGoto, Masahiro-
dc.contributor.authorKim, Sangshik-
dc.date.accessioned2022-12-26T20:03:29Z-
dc.date.available2022-12-26T20:03:29Z-
dc.date.issued2016-09-
dc.identifier.issn1598-9623-
dc.identifier.issn2005-4149-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/15287-
dc.description.abstractThe effect of superplastic forming (SPF) exposure on the. (strain)-N (number of cycles to failure) fatigue and fatigue crack propagation (FCP) behaviors of Ti-6Al-4V (Ti64) alloy was examined at 298 and 473 K. To simulate the thermal exposure during superplastic forming process, the mill-annealed Ti64 alloy sheet was heated in the vacuum chamber with the pre-determined temperature profile. Notable microstructural change during the SPF exposure included the shape of transformed beta phase from fine and round particles in the as-received specimen to coarse angular particles in the as-exposed specimen. The effective grain size tended to increase with the exposure, enhancing the slip reversibility and the resistance to FCP. However, the crack hindering effect by fine, particle-like beta phase became weak with the exposure, offseting the beneficial effect associated with the increment of effective grain size. The effect of SPF exposure on epsilon-N fatigue and FCP behavior of mill-annealed Ti64 alloy was therefore marginal, excluding the effect of alpha-case (the oxygen-enriched phase) on the surface.-
dc.format.extent8-
dc.language영어-
dc.language.isoENG-
dc.publisherKOREAN INST METALS MATERIALS-
dc.titleEffect of Superplastic Forming Exposure on Fatigue Crack Propagation Behavior of Ti-6Al-4V Alloy-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.doi10.1007/s12540-016-6075-9-
dc.identifier.scopusid2-s2.0-84983427653-
dc.identifier.wosid000381929100001-
dc.identifier.bibliographicCitationMETALS AND MATERIALS INTERNATIONAL, v.22, no.5, pp 747 - 754-
dc.citation.titleMETALS AND MATERIALS INTERNATIONAL-
dc.citation.volume22-
dc.citation.number5-
dc.citation.startPage747-
dc.citation.endPage754-
dc.type.docTypeArticle-
dc.identifier.kciidART002141336-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasssci-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.description.journalRegisteredClasskci-
dc.relation.journalResearchAreaMaterials Science-
dc.relation.journalResearchAreaMetallurgy & Metallurgical Engineering-
dc.relation.journalWebOfScienceCategoryMaterials Science, Multidisciplinary-
dc.relation.journalWebOfScienceCategoryMetallurgy & Metallurgical Engineering-
dc.subject.keywordPlusALPHA-CASE FORMATION-
dc.subject.keywordPlusTITANIUM-ALLOY-
dc.subject.keywordPlusMECHANICAL-PROPERTIES-
dc.subject.keywordPlusMICROSTRUCTURE-
dc.subject.keywordPlusSTEEL-
dc.subject.keywordPlusTEMPERATURE-
dc.subject.keywordPlusSEAWATER-
dc.subject.keywordPlusFRACTURE-
dc.subject.keywordPlusTOOL-
dc.subject.keywordAuthorfatigue crack propagation-
dc.subject.keywordAuthormetal-
dc.subject.keywordAuthormechanical properties-
dc.subject.keywordAuthorTi-6Al-4V-
dc.subject.keywordAuthormicrostructure-
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