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Exergetic effects of some design parameters on the small turbojet engine for unmanned air vehicle applications

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dc.contributor.authorTuran, Önder
dc.contributor.orcid0000-0003-0303-4313
dc.date.accessioned2025-11-13T09:13:53Z
dc.date.issued2012-04-11
dc.identifier.doihttps://doi.org/10.1016/j.energy.2012.03.030
dc.identifier.endpage61
dc.identifier.issn0360-5442
dc.identifier.issue1
dc.identifier.openalexW2008151076
dc.identifier.startpage51
dc.identifier.urihttps://hdl.handle.net/11421/838
dc.identifier.urihttps://doi.org/10.1016/j.energy.2012.03.030
dc.identifier.volume46
dc.language.isoen
dc.relation.ispartofEnergy
dc.rightsrestrictedAccess
dc.subjectTurbojet
dc.subjectExergy
dc.subjectGas compressor
dc.subjectMach number
dc.subjectThrust
dc.subjectOverall pressure ratio
dc.subjectTurbine
dc.subjectAerospace engineering
dc.subjectRange (aeronautics)
dc.subjectThrust specific fuel consumption
dc.subjectAutomotive engineering
dc.subjectEngineering
dc.subjectEnvironmental science
dc.subjectMechanical engineering
dc.subjectFuel efficiency
dc.subjectProcess engineering
dc.subject.sdg7
dc.titleExergetic effects of some design parameters on the small turbojet engine for unmanned air vehicle applications
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5079427167

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