FIELD: transport.
SUBSTANCE: aircraft (10) comprises fuselage (12) whereto secured are the shaped wings (18, 20), nose section (52), vortex regulator (72) at wing edge built-up shaped to balance the onrush development of vortices by the edge at moderately large angle of attack. Aircraft comprises detachable means with the incident wave radar radiated dissipation device located above the aircraft hot part.
EFFECT: improved aerodynamic characteristics at better radar signature.
8 cl, 29 dwg
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