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Simulation-based steady-state aero-thermal model for small-scale turboprop engine

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dc.contributor.authorKıyak, Emre
dc.contributor.authorTolga Yasa
dc.contributor.authorEmre Kıyak
dc.contributor.orcid0000-0002-8609-3353
dc.contributor.orcid0000-0002-7242-2507
dc.contributor.orcid0000-0002-5253-3613
dc.date.accessioned2025-11-13T11:24:32Z
dc.date.issued2017-03-06
dc.identifier.doihttps://doi.org/10.1108/aeat-02-2015-0062
dc.identifier.endpage210
dc.identifier.issn1748-8842
dc.identifier.issue2
dc.identifier.openalexW2586545711
dc.identifier.startpage203
dc.identifier.urihttps://hdl.handle.net/11421/6694
dc.identifier.urihttps://doi.org/10.1108/aeat-02-2015-0062
dc.identifier.volume89
dc.language.isoen
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.rightsrestrictedAccess
dc.subjectTurboprop
dc.subjectCrankshaft
dc.subjectEngineering
dc.subjectGas compressor
dc.subjectController (irrigation)
dc.subjectControl theory (sociology)
dc.subjectPerformance prediction
dc.subjectTurbine
dc.subjectThrust
dc.subjectAutomotive engineering
dc.subjectControl engineering
dc.subjectSimulation
dc.subjectComputer science
dc.subjectMechanical engineering
dc.titleSimulation-based steady-state aero-thermal model for small-scale turboprop engine
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5041694956

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