Turbofan engine weight estimation for preliminary design

dc.contributor.authorKarabacak, Mustafa
dc.contributor.authorTuran, Onder
dc.date.accessioned2024-02-23T14:31:45Z
dc.date.available2024-02-23T14:31:45Z
dc.date.issued2019
dc.departmentNEÜen_US
dc.description.abstractThe aim of the study is to prepare weight estimation model of turbofan engines to help designer in the conceptual stages of modem turbofan design. To achieve this purpose, statistical data is used on yielding robust analytical expression and experiments are conducted to prepare model for turbofan engine weight estimation is not easy due to the high cost and insufficient technical facility. Turbofan engine classified into five categories (three shaft turbofan engine, light weight two shaft turbofan engine, medium weight two shaft turbofan engine, high weight two shaft turbofan engine and two shaft geared turbofan engine) and turbofan engine weight model is developed for each category separately to increase model sensitivity. Model sensitivity is investigated for each category by error analysis to give idea about model reflection of real world to conceptual designer.en_US
dc.identifier.doi10.1504/IJSA.2019.101745
dc.identifier.endpage100en_US
dc.identifier.issn2050-0467
dc.identifier.issn2050-0475
dc.identifier.issue2en_US
dc.identifier.startpage87en_US
dc.identifier.urihttps://doi.org/10.1504/IJSA.2019.101745
dc.identifier.urihttps://hdl.handle.net/20.500.12452/15340
dc.identifier.volume5en_US
dc.identifier.wosWOS:000483360100001en_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.subjectTurbofan Engine Weighten_US
dc.subjectThrust To Weight Ratioen_US
dc.subjectBypass Ratioen_US
dc.subjectAircraften_US
dc.titleTurbofan engine weight estimation for preliminary designen_US
dc.typeArticleen_US

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