Aerodynamic layout of stalling multi-rotor vertical take-off and landing unmanned aerial vehicle

The invention, which relates to the technical field of aerodynamic layout of aircrafts, discloses an aerodynamic layout of a stalling multi-rotor vertical take-off and landing unmanned aerial vehicle,which comprises a vehicle body, wings, empennages and a level flight power unit. Each wing comprises a fixed section and a stalling rotor wing, and the stalling rotor wing is mounted at the far end of the fixed section on each side of the vehicle body through a telescopic mechanism; the stalling rotor wing is arranged below the fixed section, and a groove capable of being attached to the upper surface of any wing section of the stalling rotor wing capable is formed in the bottom surface of the fixed section; and the windward sides of the wing sections of the stalling rotor wings outside the grooves face the same direction as the windward sides of the fixed sections. Vertical lifting power is provided for the unmanned aerial vehicle through the stalling rotor wings, the stalling rotor wings are retracted to form p