| Neural network based redesign of morphing UAV for simultaneous improvement of roll stability and maximum lift/drag ratio T Oktay, S Arik, I Turkmen, M Uzun, H Celik Aircraft Engineering and Aerospace Technology 90 (8), 1203-1212, 2018 | 26 | 2018 |
| A novel learning algorithm to estimate the optimum fuselage drag coefficient T Oktay, H Çelik, M Uzun Sakarya University Journal of Science 21 (1), 63-68, 2017 | 10 | 2017 |
| PID based hierarchical autonomous system performance maximization of a hybrid unmanned aerial vehicle (HUAV) T OKTAY, U Metin, H ÇELİK, M KONAR Anadolu University Journal of Science and Technology A-Applied Sciences and …, 2017 | 9 | 2017 |
| Aerodynamic nose shape optimization for performance maximization of morphing autonomous aerial robot T Oktay, M Uzun, I Yılmaz, M Konar International Conference on Engineering and Natural Science, Sarajevo …, 2016 | 9 | 2016 |
| Maximum lift/drag ratio improvement of TUAVs via small aerodynamic modifications T Oktay, M Uzun, OO Kanat Aircraft Engineering and Aerospace Technology 90 (9), 1438-1444, 2018 | 7 | 2018 |
| MALE UAV selection in interval Type-2 fuzzy sets environment S Çoban, K Kiracı, E Akan, M Uzun Journal of Intelligent & Fuzzy Systems, 1-28, 2022 | 3 | 2022 |
| Simultaneous UAV having actively sweep angle morphing wing and flight control system design M Uzun, T Oktay Aircraft Engineering and Aerospace Technology 95 (7), 1062-1068, 2023 | 2 | 2023 |
| A novel biomimetic wing design and optimizing aerodynamic performance U Metin, M Özdemir, ÇV YILDIRIM, S Çoban Journal of Aviation 6 (1), 12-25, 2022 | 2 | 2022 |
| Aerodynamic Performance Improvement with Morphing Winglet Design U Metin, S Çoban Journal of Aviation 5 (1), 16-21, 2021 | 2 | 2021 |
| Reducing motion blur by constrained control of helicopter vibration H Çelik, T Oktay, İ Türkmen, M Uzun The 2nd International Conference on Engineering and Natural Sciences (ICENS …, 2016 | 2 | 2016 |
| Electrically Driven VTOL Flying Car Designing and Aerodynamic Analysis U Metin, S Çoban Avrupa Bilim ve Teknoloji Dergisi, 815-821, 2021 | 1 | 2021 |
| Aerodynamic shape improvement for fines maximization of TUAVs T Oktay, M Uzun 3rd International Conference on Engineering and Natural Sciences (ICENS 2017 …, 2017 | 1 | 2017 |
| The aerodynamic force estimation of a swept-wing UAV using ANFIS based on metaheuristic algorithms M Uzun, HH Bilgiç, EH Çopur, S Çoban The Aeronautical Journal 128 (1322), 739-755, 2024 | | 2024 |
| Fluid-structure coupled simulation-based investigation and thrust/efficiency calculation for a UAV twin-blade propeller U Metin, Ç Hasan, K Abdullah, Ç Sezer Erciyes Üniversitesi Fen Bilimleri Enstitüsü Dergisi 39 (2), 183-191, 2023 | | 2023 |
| Structural comparison of vertical and horizontal layout of carrying arms of rotary-wing UAV with finite element analysis A Kocamer, H ÇINAR, S ÇOBAN, U Metin European Mechanical Science 7 (2), 122-127, 2023 | | 2023 |
| Static Analysis and Design of Fixed-Wing Tactical Unmanned Aerial Vehicle (TUAV) Retractable Main Landing Gear A Kocamer, M Uzun, S Çoban Asrel Aerospace Research Letters 1 (2), 125-131, 2022 | | 2022 |
| Static Analysis and Design of Fixed-Wing Tactical Unmanned Aerial Vehicle (TUAV) Retractable Main Landing Gear A KOCAMER, M UZUN, S ÇOBAN ASREL, 125, 0 | | |
(Full) Professor Dr. Tugrul OktayErciyes UniversityVerified email at erciyes.edu.tr
