Exergy analysis of a turbofan aircraft engine

dc.contributor.authorTurgut, Enis T.
dc.contributor.authorKarakoc, T. Hikmet
dc.contributor.authorHepbasli, Arif
dc.contributor.authorRosen, Marc A.
dc.date.accessioned2019-10-27T20:20:36Z
dc.date.available2019-10-27T20:20:36Z
dc.date.issued2009
dc.departmentEge Üniversitesien_US
dc.description.abstractAn exergy analysis is reported for a General Electric turbofan engine (the CF6-80) using sea-level data. The effects on exergy efficiencies and exergy destructions are investigated of modifying the isentropic efficiencies of turbomachinery components. The most irreversible units in the system are found to be the fan and the core engine exhaust, with exergy loss rates of 47.3 MW and 35.9 MW, respectively, and the combustion chamber, with an exergy destruction rate of 31.5 MW. The exergy efficiencies of the fan and the core engine exhausts are found to be 12.9 and 12.7%, respectively.en_US
dc.identifier.doi10.1504/IJEX.2009.023997
dc.identifier.endpage199en_US
dc.identifier.issn1742-8297
dc.identifier.issn1742-8300
dc.identifier.issn1742-8297en_US
dc.identifier.issn1742-8300en_US
dc.identifier.issue2en_US
dc.identifier.scopusqualityQ3en_US
dc.identifier.startpage181en_US
dc.identifier.urihttps://doi.org/10.1504/IJEX.2009.023997
dc.identifier.urihttps://hdl.handle.net/11454/41650
dc.identifier.volume6en_US
dc.identifier.wosWOS:000265449200003en_US
dc.identifier.wosqualityQ3en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherInderscience Enterprises Ltden_US
dc.relation.ispartofInternational Journal of Exergyen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectexergy analysisen_US
dc.subjectturbofan engineen_US
dc.subjectBrayton cycleen_US
dc.subjectefficiencyen_US
dc.subjectaerospaceen_US
dc.subjectaircraften_US
dc.titleExergy analysis of a turbofan aircraft engineen_US
dc.typeArticleen_US

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