FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering and can be used in designing streamlined bodies for aircraft. Streamlined body comprises outer shell, oncoming flow braking and streamline areas, flow control device and mixing chamber. Outlet device abuts on said mixing chamber. Flow control device comprises multiple micro holes and suction chambers, connection channel, sucker with inlet and decelerated fluid medium feed channel. Said sucker comprises the case making and intake chamber with inlet and outlet and nozzle with inlet. Said streamlined body is n engine nacelle and aircraft airframe airfoil.
EFFECT: decreased weight, electric power savings.
12 cl, 7 dwg
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