FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to short take-off and landing aircraft. 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 on aerodynamic profile upper convex surface between profile front edge and its top point. To create control forces and moments, propulsion units uniformly arranged along wing span can independently vary thrust force. Number of propulsion units shall be even. Motors used can be turbojet engines, impellers with high-speed electric motors or impellers driven by piston ICE.
EFFECT: higher efficiency of aircraft, efficiency of control, simplified design.
1 cl, 3 dwg
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