Optimization of the winglet geometry of a small airplane-type UAV wing

Authors

  • Serhii Zubets National Aviation University
  • Sviatoslav Yutskevych National Aviation University
  • Olexandr Yakobchuk National Aviation University

Keywords:

winglets, aerodynamics, UAV

Abstract

This study provides an analysis of the impact of key geometric parameters of winglets on the lift-to-drag (L/D) ratio for airplane-type UAV. The results of this analysis, conducted using Statgraphics Centurion, are presented and discussed.

Additional Files

Published

2025-03-28

Issue

2024: XI Всесвітній конгрес “Авіація в XXI столітті” – “Безпека в авіації та космічні технології”

Section

Design, strength and durability of aviation machines