FIELD: aviation.
SUBSTANCE: invention relates to aircrafts made in aerodynamic scheme "flying wing". Aircraft comprises an air intake device, a power plant located in the wing, a propulsion system traction control system of the power plant, a flight control and stabilization system. Air intake device is installed with possibility of rotation relative to longitudinal wing axis in plane of its construction horizontal by angle α in range from 0° up to 90°. Control system is configured to change direction of thrust vector in plane of construction horizontal by angle β=α in direction opposite to direction of rotation of air intake device.
EFFECT: invention is aimed at improvement of aerodynamic quality at all flight modes and reduction of radar visibility of the aircraft.
1 cl, 6 dwg
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