“…At present, the unmanned aerial vehicle (UAV) industry has a wide range of application prospects in both military and civilian operations [ 1 ]. With the effectiveness advantages such as taking off and landing without a runway, autonomous operation, and a wide scope of work, multi-rotor UAVs, as the most commonly used type of UAV, are widely employed in military reconnaissance [ 2 , 3 , 4 ], military strikes [ 5 ], disaster rescue, tilt photography imaging, agricultural applications [ 6 , 7 ], logistics transportation, exploration, and other fields [ 8 , 9 ]. However, due to the many rotating lift surfaces [ 10 ], strong coupling interference [ 11 ], obvious unsteady flow, and poor stability [ 12 ] of multi-rotor UAVs, it is essential to understand the mechanisms of their aerodynamic characteristics.…”