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Investigation of Impact Behavior of TIG Welded Inconel 718 at Aircraft Engine Operating Temperatures

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dc.contributor.authorUzunonat, Yağız
dc.contributor.orcid0000-0002-0992-7190
dc.date.accessioned2025-11-13T22:51:34Z
dc.date.issued2017-03-20
dc.identifier.doihttps://doi.org/10.4028/www.scientific.net/msf.890.339
dc.identifier.endpage343
dc.identifier.issn0255-5476
dc.identifier.openalexW2600155601
dc.identifier.startpage339
dc.identifier.urihttps://hdl.handle.net/11421/15545
dc.identifier.urihttps://doi.org/10.4028/www.scientific.net/msf.890.339
dc.identifier.volume890
dc.language.isoen
dc.relation.ispartofMaterials science forum
dc.rightsrestrictedAccess
dc.subjectMaterials science
dc.subjectCharpy impact test
dc.subjectWelding
dc.subjectInconel
dc.subjectDuctility (Earth science)
dc.subjectGas tungsten arc welding
dc.subjectMetallurgy
dc.subjectScanning electron microscope
dc.subjectComposite material
dc.subjectUltimate tensile strength
dc.subjectArc welding
dc.subjectCreep
dc.subject.sdg7
dc.titleInvestigation of Impact Behavior of TIG Welded Inconel 718 at Aircraft Engine Operating Temperatures
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5086950730

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