A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV
Yıl: 2022 Cilt: 6 Sayı: 2 Sayfa Aralığı: 292 - 306 Metin Dili: İngilizce DOI: 10.46519/ij3dptdi.1128158 İndeks Tarihi: 12-09-2022
A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV
Öz: 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.
Anahtar Kelime: Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık
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| APA | SARAÇYAKUPOGLU T, DELİBAŞ H, Özçelik A (2022). A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. , 292 - 306. 10.46519/ij3dptdi.1128158 |
| Chicago | SARAÇYAKUPOGLU TAMER,DELİBAŞ HEYZEM DOĞUKAN,Özçelik Ahmet Devlet A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. (2022): 292 - 306. 10.46519/ij3dptdi.1128158 |
| MLA | SARAÇYAKUPOGLU TAMER,DELİBAŞ HEYZEM DOĞUKAN,Özçelik Ahmet Devlet A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. , 2022, ss.292 - 306. 10.46519/ij3dptdi.1128158 |
| AMA | SARAÇYAKUPOGLU T,DELİBAŞ H,Özçelik A A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. . 2022; 292 - 306. 10.46519/ij3dptdi.1128158 |
| Vancouver | SARAÇYAKUPOGLU T,DELİBAŞ H,Özçelik A A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. . 2022; 292 - 306. 10.46519/ij3dptdi.1128158 |
| IEEE | SARAÇYAKUPOGLU T,DELİBAŞ H,Özçelik A "A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV." , ss.292 - 306, 2022. 10.46519/ij3dptdi.1128158 |
| ISNAD | SARAÇYAKUPOGLU, TAMER vd. "A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV". (2022), 292-306. https://doi.org/10.46519/ij3dptdi.1128158 |
| APA | SARAÇYAKUPOGLU T, DELİBAŞ H, Özçelik A (2022). A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. International Journal of 3D Printing Technologies and Digital Industry, 6(2), 292 - 306. 10.46519/ij3dptdi.1128158 |
| Chicago | SARAÇYAKUPOGLU TAMER,DELİBAŞ HEYZEM DOĞUKAN,Özçelik Ahmet Devlet A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. International Journal of 3D Printing Technologies and Digital Industry 6, no.2 (2022): 292 - 306. 10.46519/ij3dptdi.1128158 |
| MLA | SARAÇYAKUPOGLU TAMER,DELİBAŞ HEYZEM DOĞUKAN,Özçelik Ahmet Devlet A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. International Journal of 3D Printing Technologies and Digital Industry, vol.6, no.2, 2022, ss.292 - 306. 10.46519/ij3dptdi.1128158 |
| AMA | SARAÇYAKUPOGLU T,DELİBAŞ H,Özçelik A A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. International Journal of 3D Printing Technologies and Digital Industry. 2022; 6(2): 292 - 306. 10.46519/ij3dptdi.1128158 |
| Vancouver | SARAÇYAKUPOGLU T,DELİBAŞ H,Özçelik A A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV. International Journal of 3D Printing Technologies and Digital Industry. 2022; 6(2): 292 - 306. 10.46519/ij3dptdi.1128158 |
| IEEE | SARAÇYAKUPOGLU T,DELİBAŞ H,Özçelik A "A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV." International Journal of 3D Printing Technologies and Digital Industry, 6, ss.292 - 306, 2022. 10.46519/ij3dptdi.1128158 |
| ISNAD | SARAÇYAKUPOGLU, TAMER vd. "A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV". International Journal of 3D Printing Technologies and Digital Industry 6/2 (2022), 292-306. https://doi.org/10.46519/ij3dptdi.1128158 |
