The Aerodynamic Effects of Pressure Mahgnitude and Blowing Angle on Lateral Autonomous Performance of UAVs
Yazarlar (2)
Prof. Dr. Tuğrul Oktay Erciyes Üniversitesi, Türkiye
Dr. Öğr. Üyesi Öztürk Özdemir KANAT Kastamonu Üniversitesi, Türkiye
| Bildiri Türü | Tebliğ/Bildiri | Bildiri Dili | İngilizce |
| Bildiri Alt Türü | Tam Metin Olarak Yayınlanan Tebliğ (Uluslararası Kongre/Sempozyum) | ||
| Bildiri Niteliği | Alanında Hakemli Uluslararası Kongre/Sempozyum | ||
| Kongre Adı | 5th International Conference on Engineering and Natural Sciences | ||
| Kongre Tarihi | 12-06-2019 / 16-06-2019 | ||
| Basıldığı Ülke | Çek Cumhuriyeti | Basıldığı Şehir | Prag |
| UAK Araştırma Alanları |
Aerodinamik
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| Özet |
| In this study, the effects on the lateral flight control system of the UAVs are investigated by improving using active flow control technique the vortex occurring on the upper surface of the UAVs’ wing during the straight flight. Blowing which is one of the flow control methods for an aircraft is preferred for this study. In order to obtain the best blowing data, carrying out numerical analysis of different angles of attack the effects of blowing angle and different pressure magnitude on the aerodynamic performance of the UAV are evaluated. In order to evaluate the aerodynamic performance, changes in the lift and drag coefficient values on the aircraft were considered. Lateral flight performance of UAVs is analyzed with MATLAB/Simulink program according to the pressure and blowing angle values at which aerodynamic performance is highest. As a result, it has been observed that there are significant improvements in UAV's lateral autonomous flight performance compared to the initial values. |
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