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Application of thermodynamic laws on a military helicopter engine

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dc.contributor.authorÇoban, Kahraman
dc.contributor.authorKarakoç, T. Hikmet
dc.contributor.authorT. Hikmet Karakoç
dc.contributor.orcid0000-0002-3084-1586
dc.contributor.orcid0000-0003-0855-3147
dc.contributor.orcid0000-0001-8182-8667
dc.date.accessioned2025-11-13T09:31:30Z
dc.date.issued2017-08-01
dc.identifier.doihttps://doi.org/10.1016/j.energy.2017.07.179
dc.identifier.endpage1436
dc.identifier.issn0360-5442
dc.identifier.openalexW2740380161
dc.identifier.startpage1427
dc.identifier.urihttps://hdl.handle.net/11421/1390
dc.identifier.urihttps://doi.org/10.1016/j.energy.2017.07.179
dc.identifier.volume140
dc.language.isoen
dc.relation.ispartofEnergy
dc.rightsrestrictedAccess
dc.subjectExergy
dc.subjectCombustion chamber
dc.subjectTurbine
dc.subjectExergy efficiency
dc.subjectCombustion
dc.subjectGas turbines
dc.subjectEnvironmental science
dc.subjectEngineering
dc.subjectNuclear engineering
dc.subjectEngine power
dc.subjectPower (physics)
dc.subjectAutomotive engineering
dc.subjectMechanical engineering
dc.subjectWaste management
dc.subjectThermodynamics
dc.subjectChemistry
dc.subjectPhysics
dc.subject.sdg7
dc.titleApplication of thermodynamic laws on a military helicopter engine
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5035343670
local.authorid.openalexA5031272314

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