Engine weight estimation of fifth generation fighter aircraft for high range and manoeuvrability

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dc.contributor.authorKarabacak, Mustafa
dc.contributor.authorTuran, Onder
dc.date.accessioned2024-02-23T14:49:17Z
dc.date.available2024-02-23T14:49:17Z
dc.date.issued2020
dc.departmentNEÜen_US
dc.description.abstractThis study focuses on afterburner turbofan engine weight estimation for fifth generation fighter aircrafts. Model developed in this study by investigating 26 engine cases categorised by the criteria the requirement of selection amongst to engines expected to be used in fifth generation fighter depend on four parameters with approximate to +/- 25% error. Technology level effect engine weight strongly so parameter reflect technology level is determined based on new technology engines used in fifth generation fighter aircraft by statistical method. Model reflect technology level is expected to be used in conceptual design stages of fifth generation fighter engine.en_US
dc.identifier.endpage246en_US
dc.identifier.issn2050-0467
dc.identifier.issn2050-0475
dc.identifier.issue3en_US
dc.identifier.startpage236en_US
dc.identifier.urihttps://hdl.handle.net/20.500.12452/18105
dc.identifier.volume6en_US
dc.identifier.wosWOS:000607981500005en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.language.isoenen_US
dc.publisherInderscience Enterprises Ltden_US
dc.relation.ispartofInternational Journal Of Sustainable Aviationen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectFifth Fighter Aircraften_US
dc.subjectThrusten_US
dc.subjectWeight Ratioen_US
dc.subjectAfterburneren_US
dc.subjectTurbofanen_US
dc.titleEngine weight estimation of fifth generation fighter aircraft for high range and manoeuvrabilityen_US
dc.typeArticleen_US

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