dc.contributor.author | Saraçyakupoğlu, Tamer | |
dc.contributor.author | Delibaş, Heyzem Doğukan | |
dc.contributor.author | Özçelik, Ahmet Devlet | |
dc.date.accessioned | 2022-09-06T10:30:31Z | |
dc.date.available | 2022-09-06T10:30:31Z | |
dc.date.issued | 2022 | en_US |
dc.identifier.issn | 2602-3350 | |
dc.identifier.issn | 2602-3350 | |
dc.identifier.uri | https://hdl.handle.net/11363/3715 | |
dc.description.abstract | This 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.language.iso | eng | en_US |
dc.rights | info:eu-repo/semantics/openAccess | en_US |
dc.rights | Attribution-NonCommercial-NoDerivs 3.0 United States | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/3.0/us/ | * |
dc.subject | Unmanned Aerial Vehicle (UAV) | en_US |
dc.subject | Time to climb | en_US |
dc.subject | Take-off performance | en_US |
dc.subject | Maximum turn rate | en_US |
dc.title | A Computational Determination of a Nozzle Activated Fixed-Wing Uav | en_US |
dc.type | article | en_US |
dc.relation.ispartof | International Journal of 3D Printing Technologies and Digital Industry | en_US |
dc.department | Uygulamalı Bilimler Fakültesi | en_US |
dc.relation.publicationcategory | Konferans Öğesi - Ulusal - Kurum Öğretim Elemanı | en_US |
dc.contributor.institutionauthor | Delibaş, Heyzem Doğukan | |
dc.contributor.institutionauthor | Ahmet Devlet, Özçelik | |