The invention discloses an aircraft for achieving vertical take-off and landing and flight through slip flow lift force of wings and belongs to the technical field of aviation. The aircraft comprisesan aircraft body, the wings, drive devices and the like. The multiple drive devices are arranged above the front edges of the wings, the wings are directly fixed or longitudinally hinged to the aircraft body, the attack angles of the wings can be adjusted, the drive devices are directly fixed or hinged to the wings and can longitudinally tilt to change the air blowing angles of the drive devices,horizontal tails can be longitudinally hinged to the corresponding wings or the aircraft body, and the attack angles of the horizontal tails can be longitudinally adjusted; the drive devices blow high-speed airflow in the chordwise direction to the upper surfaces of the wings, the airflow quickly flows through the upper surfaces and the lower surfaces of the wings to generate the flow speed difference, and wing lift force is generated; and through adjustment of the attack angles theta of the wings, or the air blowing angles alpha of the drive devices blowing air to the surfaces of the wings, or the attack angles beta of the horizontal tails, the blowing direction of the airflow relative to the aircraft body is changed, powers are increased and decreased in cooperation with the drive devices, and the aircraft vertically takes off and lands or hovers. The aircraft has the beneficial effects that vertical take-off and landing and high-speed flight working conditions can be compatible, andthe aircraft is high in flight efficiency, safe, reliable and the like.