Yazar "Eraslan, Yüksel" için listeleme
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Impacts of Tapered Wingtip on Lateral-Directional Stability Coefficients of a Morphing Fixed-wing UAV
Oktay, Tuğrul; Eraslan, Yüksel (Giresun Üniversitesi, 2023)Recent developments in unmanned aerial vehicle (UAV) technologies have shown the possibility of morphing applications to provide improvement in various performance metrics in the desired manner. In rotary-wing UAVs, ... -
Numerical Investigation of Effects of Airspeed and Rotational Speed on Quadrotor UAV Propeller Thrust Coefficient
Oktay, Tuğrul; Eraslan, Yüksel (Journal of aviation (Online), 2021)In this article, a numerical investigation was performed on a quadrotor unmanned aeroial vehicles (UAV) propeller to examine the effects of airspeed and rotational speed on thrust coefficient, which is one of the most ... -
Simultaneous flight control system and twist-morphing wing design of an unmanned aerial vehicle
Eraslan ,Yüksel; Oktay, Tugrul (Niğde Ömer Halisdemir Üniversitesi, 2024)Son yıllarda malzeme teknolojilerindeki gelişmelerle birlikte hava aracı tasarımı alanında başkalaşım teknolojilerinin de uygulamaları yaygınlaşmıştır. Bu bağlamda, bu çalışmada, sabit kanatlı bir insansız hava aracı (İHA) ... -
Stability Evaluation of a Fixed-Wing Unmanned Aerial Vehicle with Morphing Wingtip
Oktay, Tuğrul; Eraslan, Yüksel (Edit Publishing, 2022)Aeronautical applications of morphing technologies are continued to increase their popularity and wide spread application during last years. The technology takes place in not only military, but also civil applications that ...
