FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to short take-off and landing aircraft structures. Aircraft comprises airfoil section with top bulged surface. Propulsion units are arranged in channels connecting air intakes of constant area and slotted nozzles arranged on upper surface of wing between inlet device and rear edge of profile. Constant area inlet devices can be arranged in an arbitrary area of the upper convex surface of the aerofoil between the leading edge of the profile and its upper point. To create control forces and moments propulsion units are arranged in two groups located transversely to direction of flight, with uniform disposition relative to longitudinal axis of aircraft in composition of each group and possibility to independently vary thrust force.
EFFECT: higher efficiency of aircraft and its reliability, efficiency of control, simplified design.
4 cl, 5 dwg
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