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Cyclic Oxidation Behaviour of MoSi<sub>2</sub> and MoSi<sub>2</sub>-Si<sub>3</sub>N<sub>4</sub> Composites for Aircraft Gas Turbine Elements

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dc.contributor.authorUzunonat, Yağız
dc.contributor.authorSinem Cevik Uzgur
dc.contributor.authorSeyid Fehmi Diltemiz
dc.contributor.authorMelih Cemal Kuşhan
dc.contributor.orcid0000-0002-0992-7190
dc.contributor.orcid0000-0002-3952-4456
dc.contributor.orcid0000-0002-9427-6192
dc.date.accessioned2025-11-13T12:18:52Z
dc.date.issued2011-02-01
dc.identifier.doihttps://doi.org/10.4028/www.scientific.net/amr.214.349
dc.identifier.endpage353
dc.identifier.issn1022-6680
dc.identifier.openalexW1974832339
dc.identifier.startpage349
dc.identifier.urihttps://hdl.handle.net/11421/9642
dc.identifier.urihttps://doi.org/10.4028/www.scientific.net/amr.214.349
dc.identifier.volume214
dc.language.isoen
dc.relation.ispartofAdvanced materials research
dc.rightsrestrictedAccess
dc.subjectMaterials science
dc.subjectGas turbines
dc.subjectChemical engineering
dc.subjectFracture toughness
dc.subjectMetallurgy
dc.subjectMechanical engineering
dc.subjectEngineering
dc.subject.sdg7
dc.titleCyclic Oxidation Behaviour of MoSi<sub>2</sub> and MoSi<sub>2</sub>-Si<sub>3</sub>N<sub>4</sub> Composites for Aircraft Gas Turbine Elements
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5086950730

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