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dc.contributor.authorBaklacıoğlu, Tolga
dc.date.accessioned2019-10-20T19:32:53Z
dc.date.available2019-10-20T19:32:53Z
dc.date.issued2015
dc.identifier.issn0001-9240
dc.identifier.urihttps://hdl.handle.net/11421/18673
dc.descriptionWOS: 000350615700003en_US
dc.description.abstractIn this study, development of a new fuel flow rate model for the climbing phase of flight was achieved using a genetic algorithm (GA) method. Two modelling approaches were performed using real flight data records (FDRs) from a medium-weight transport-category aircraft. The first model considered the dependency of fuel consumption only with respect to altitude, whereas the effects of both altitude and true airspeed (TAS) were included in the second model. The proposed models are improvements on existing models because the relationship between fuel flow rate, flight altitude, and TAS can be deduced using the derived formulations. Both modelling approaches were found to provide accurate results after performing an error analysis for fuel flow rate values. It was clear that incorporating the TAS effect into the second model enhanced the accuracy of the model, but the first model was also found to be appropriate for practical usage.en_US
dc.language.isoengen_US
dc.publisherRoyal Aeronautical Socen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titleFuel flow-rate modelling of transport aircraft for the climb flight using genetic algorithmsen_US
dc.typearticleen_US
dc.relation.journalAeronautical Journalen_US
dc.contributor.departmentAnadolu Üniversitesi, Havacılık ve Uzay Bilimleri Fakültesi, Uçak Gövde Motor Bakım Bölümüen_US
dc.identifier.volume119en_US
dc.identifier.issue1212en_US
dc.identifier.startpage173en_US
dc.identifier.endpage183en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US]
dc.contributor.institutionauthorBaklacıoğlu, Tolga


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