FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Wing 1 comprises wing center section made up of shaped bearing disk 2 with front and rear edges along generatrix of bearing disk. Panels 3 are jointed with wing center section bearing disk 2 on its sides so that the shape of front and rear edges of said disk 2 are unchanged along said generatrix in plan. Wing panels 3 feature trapezoidal and sweep and/or rectangular aerodynamic shape. Wing 1 has aerodynamic extensions 4 made along wing lengthwise axis at wing front on both sides that feature triangular and ogival aerodynamic shape in plan.
EFFECT: higher maneuverability.
5 cl, 7 dwg
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