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On-design exergy analysis of a combustor for a turbojet engine: a parametric study

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dc.contributor.authorTuran, Önder
dc.contributor.authorÖnder Turan
dc.contributor.orcid0000-0002-9185-3927
dc.contributor.orcid0000-0003-0303-4313
dc.date.accessioned2025-11-13T10:54:01Z
dc.date.issued2017-08-25
dc.identifier.doihttps://doi.org/10.1108/aeat-12-2016-0254
dc.identifier.endpage724
dc.identifier.issn1748-8842
dc.identifier.issue5
dc.identifier.openalexW2747669011
dc.identifier.startpage719
dc.identifier.urihttps://hdl.handle.net/11421/5600
dc.identifier.urihttps://doi.org/10.1108/aeat-12-2016-0254
dc.identifier.volume89
dc.language.isoen
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.rightsrestrictedAccess
dc.subjectCombustor
dc.subjectExergy
dc.subjectExergy efficiency
dc.subjectEngineering
dc.subjectGas compressor
dc.subjectTurbojet
dc.subjectOverall pressure ratio
dc.subjectBrayton cycle
dc.subjectEnvironmental science
dc.subjectTurbine
dc.subjectMechanical engineering
dc.subjectProcess engineering
dc.subjectAutomotive engineering
dc.subjectCombustion
dc.subjectChemistry
dc.titleOn-design exergy analysis of a combustor for a turbojet engine: a parametric study
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5079427167

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