Aerodynamic Studies and Conceptual Design of a Small Box-Wing VTOL UAV

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Danupol Sutthison
Prasatporn Wongkamchang
Nukul Sukuprakarn

Abstract

This research presents a study of the aerodynamics of a small box-wing vertical take-off and landing unmanned aerial vehicle with the airfoil S3010, which has a high lift coefficient from the results of a comparison of the airfoils commonly used in small UAV design by the XFLR5 program. This airfoil was used for the modeling of baseline mono-plane UAV and box-wing UAV to compare the aerodynamic characteristics using computational fluid dynamics methods. The results show that box-wing UAVs had a 9.43% higher lift-to-drag than mono-plane UAVs at a cruising speed of 17.5 m/s and an angle of attack of 0°. As the results, the installation of tilt motor has been proposed for the further proceeding in the preliminary design phase.

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How to Cite
Sutthison ด., Wongkamchang ป., & Sukuprakarn น. (2022). Aerodynamic Studies and Conceptual Design of a Small Box-Wing VTOL UAV. Journal of Engineering, RMUTT, 20(1), 49–60. Retrieved from https://ph01.tci-thaijo.org/index.php/jermutt/article/view/245682
Section
Research Articles

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