Aerodynamic Performance of Hex-Rotor UAV Considering the Horizontal Airflow
In this paper, the aerodynamic performance of a Hex-rotor unmanned aerial vehicle (UAV) with different rotational speeds (1500−2300 RPM) considering the horizontal airflow conditions is analyzed by both simulations and experiments.A low-speed wind tunnel experiments platform is applied to measure the thrust, torque, and power consumption of a