(National Aviation University, 2024-04) Panchuk, Yevhen; Панчук, Євген
In recent times, there has been a surge in interest surrounding the development and deployment of unmanned aerial vehicles (UAVs), encompassing both fixed-wing aircraft and copter configurations, with sizes ranging from mere tens of centimeters to several meters. For many developers, the aerodynamic characteristics of UAVs may not pose an immediate concern, especially when the aircraft boasts substantial power capabilities. However, as missions extend to longer durations, achieving optimal aerodynamic performance becomes increasingly pertinent.
