FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to flying-wing aircraft. Aircraft comprises at least one channel for draft flow extending through airframe from air intake at airframe surface via jet engine to jet nozzle at airframe surface. Said jet engine is located at least partially ahead of said air intake. Said air intake has curved sections to feed draft flows to engine.
EFFECT: better aircraft concealment.
11 cl, 10 dwg
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