A Computational Determination of a Nozzle Activated Fixed-Wing Uav

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dc.contributor.authorSaraçyakupoğlu, Tamer
dc.contributor.authorDelibaş, Heyzem Doğukan
dc.contributor.authorÖzçelik, Ahmet Devlet
dc.date.accessioned2022-09-06T10:30:31Z
dc.date.available2022-09-06T10:30:31Z
dc.date.issued2022en_US
dc.departmentUygulamalı Bilimler Fakültesien_US
dc.description.abstractThis paper proposes new methods and strategies for the propulsion of a mini Unmanned Aerial Vehicle (UAV). Typically, the UAVs are propelled by new technology batteries, fossil fuels, and hybrid systems. An experimental research regarding the usage of compressed air has been carried out. In total 13 nozzles have been installed to the fuselage of the UAV in terms of gaining 3-axis movement during flight. At the end of the manuscript, a MATLAB (Mathworks, US) program is provided in terms of calculating the maximum force and the flying time with the gained force. The UAV, whose design is presented, will be ideal for both defense and border security tasks, as it can move over the vehicle, has extremely high portability, and has a small physical footprint.en_US
dc.identifier.issn2602-3350
dc.identifier.issn2602-3350
dc.identifier.trdizinid1120202en_US
dc.identifier.urihttps://hdl.handle.net/11363/3715
dc.identifier.urihttps://search.trdizin.gov.tr/tr/yayin/detay/1120202
dc.indekslendigikaynakTR-Dizinen_US
dc.institutionauthorDelibaş, Heyzem Doğukan
dc.institutionauthorAhmet Devlet, Özçelik
dc.language.isoenen_US
dc.relation.ispartofInternational Journal of 3D Printing Technologies and Digital Industryen_US
dc.relation.publicationcategoryKonferans Öğesi - Ulusal - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectUnmanned Aerial Vehicle (UAV)en_US
dc.subjectTime to climben_US
dc.subjectTake-off performanceen_US
dc.subjectMaximum turn rateen_US
dc.titleA Computational Determination of a Nozzle Activated Fixed-Wing Uaven_US
dc.typeArticleen_US

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