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Aerothermal Investigation of a Turbine Cooling Channel with U-Bend

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dc.contributor.authorIsa Kavas
dc.contributor.authorYasa, Tolga
dc.contributor.authorTolga Yasa
dc.contributor.authorDilek Funda Kurtuluş
dc.contributor.orcid0000-0002-7242-2507
dc.contributor.orcid0000-0002-0678-9474
dc.date.accessioned2025-11-13T22:54:10Z
dc.date.issued2017-11-08
dc.identifier.doihttps://doi.org/10.1007/978-3-319-67134-5_10
dc.identifier.openalexW2767672143
dc.identifier.urihttps://hdl.handle.net/11421/15686
dc.identifier.urihttps://doi.org/10.1007/978-3-319-67134-5_10
dc.language.isoen
dc.rightsrestrictedAccess
dc.subjectTurbulence
dc.subjectNusselt number
dc.subjectMechanics
dc.subjectTurbine
dc.subjectHeat transfer
dc.subjectInlet
dc.subjectMechanical engineering
dc.subjectReynolds number
dc.subjectTurbine blade
dc.subjectGas turbines
dc.subjectHeat flux
dc.subjectMaterials science
dc.subjectEngineering
dc.subjectPhysics
dc.subject.sdg7
dc.titleAerothermal Investigation of a Turbine Cooling Channel with U-Bend
dc.typebook-chapter
dspace.entity.typePublication
local.authorid.openalexA5053241819

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