Aircraft based on active flow control technology of collaborative jet flow

The invention provides an aircraft based on a collaborative jet flow active flow control technology, the collaborative jet flow technology is an active flow control technology, the aircraft is controlled by adopting an air flow blowing and sucking mode, and the invention provides an aircraft applying a new concept flow control method, and relates to the technical field of aviation pneumatics. The aircraft applying the collaborative jet technology adopts a conventional layout and comprises a fuselage, wings and an empennage, and an air compressor, an air suction device and an air blowing device are clamped in the aircraft, so that the purpose of collaborative jet is achieved. The main wing comprises a first wing section and a second wing section, the first wing section is connected with the fuselage, and the second wing section is connected with the end, away from the fuselage, of the first wing section. The front end of the upper wing surface of the second wing section is provided with a blowing port, and the