Design, Analysis and Manufacturing of Twist Morphing Wing for UAV Purpose

The main obstacle in the design of an effective fixed-wing aircraft is the reduction of induced drag, which is a significant factor in the total drag experienced at low speeds. One approach to address this issue is by implementing a twist morphing wing, which aids in minimizing wing tip vortices and eliminating drag caused by gaps and discontinuities between the wing and control surfaces. This research study primarily focuses on examining the aerodynamic properties of a twist morphing wing specifically tailored for unmanned aerial vehicle (UAV) flight characteristics. Numerical analyses are utilized to conduct an analytical comparison between a conventional fixed wing and the morphed wing design. Additionally, a functional prototype of the twist morphing wing, complete with an actuating mechanism, is developed.