FIELD: aircraft engineering.SUBSTANCE: supersonic aircraft comprises fuselage, short-span wing with large sweep extension in root part, vertical fins with rudder, power plant with air intake, elevons. On wing leading edge aerodynamic tooth is installed, and on wing trailing edge fixed planes with slots along wing chord are made, comprising single aerofoil section with outer wings.EFFECT: invention is aimed at expansion of angle of attack at subsonic fight speeds.1 cl, 12 dwg
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