Design optimization of a fixed wing aircraft

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dc.authoridPadmanaban, Sanjeevikumar/0000-0003-3212-2750
dc.contributor.authorYayli, Ugur C.
dc.contributor.authorKimet, Cihan
dc.contributor.authorDuru, Anday
dc.contributor.authorCetir, Ozgur
dc.contributor.authorTorun, Ugur
dc.contributor.authorAydogan, Ahmet C.
dc.contributor.authorPadmanaban, Sanjeevikumar
dc.date.accessioned2024-09-29T16:05:16Z
dc.date.available2024-09-29T16:05:16Z
dc.date.issued2017
dc.departmentKarabük Üniversitesien_US
dc.description.abstractSmall aircrafts, Unmanned Aerial Vehicles (UAVs), are used especially for military purposes. Because landing fields are limited in rural and hilly places, take-off or landing distances are very important. In order to achieve a short landing or take-off distance many parameters have to be considered, for instance the design of aircrafts. Hence this paper represents a better design to enlarge the use of fixed wing aircrafts. The document is based on a live and simulated experiments. The various components of designed aircraft are enhanced to create short take-off distance, greater lift and airflow without the need for proper runway area. Therefore, created aerodynamics of the remotely piloted aircraft made it possible to use fixed wing aircrafts in rural areas.en_US
dc.identifier.doi10.12989/aas.2017.4.1.065
dc.identifier.endpage80en_US
dc.identifier.issn2287-528X
dc.identifier.issn2287-5271
dc.identifier.issue1en_US
dc.identifier.scopus2-s2.0-85027343774en_US
dc.identifier.scopusqualityQ3en_US
dc.identifier.startpage65en_US
dc.identifier.urihttps://doi.org/10.12989/aas.2017.4.1.065
dc.identifier.urihttps://hdl.handle.net/20.500.14619/6609
dc.identifier.volume4en_US
dc.identifier.wosWOS:000395247500005en_US
dc.identifier.wosqualityN/Aen_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherTechno-Pressen_US
dc.relation.ispartofAdvances in Aircraft and Spacecraft Scienceen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectfixed wingen_US
dc.subjectaircraften_US
dc.subjecttake-off distanceen_US
dc.subjectdesign optimizationen_US
dc.titleDesign optimization of a fixed wing aircraften_US
dc.typeArticleen_US

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