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Energy and exergy analysis at different hybridization factors for hybrid electric propulsion light utility helicopter engine

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dc.contributor.authorKoruyucu, Elif
dc.contributor.orcid0000-0001-9217-382X
dc.date.accessioned2025-11-13T10:12:32Z
dc.date.issued2019-09-13
dc.identifier.doihttps://doi.org/10.1016/j.energy.2019.116105
dc.identifier.endpage116105
dc.identifier.issn0360-5442
dc.identifier.openalexW2972795408
dc.identifier.startpage116105
dc.identifier.urihttps://hdl.handle.net/11421/3451
dc.identifier.urihttps://doi.org/10.1016/j.energy.2019.116105
dc.identifier.volume189
dc.language.isoen
dc.relation.ispartofEnergy
dc.rightsrestrictedAccess
dc.subjectExergy
dc.subjectExergy efficiency
dc.subjectPropulsion
dc.subjectEnvironmental science
dc.subjectAltitude (triangle)
dc.subjectElectrically powered spacecraft propulsion
dc.subjectCombustion
dc.subjectChemistry
dc.subjectPhysics
dc.subjectThermodynamics
dc.subjectMathematics
dc.subject.sdg7
dc.titleEnergy and exergy analysis at different hybridization factors for hybrid electric propulsion light utility helicopter engine
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5011434994

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