FIELD: the invention refers to the field of aviation particularly to installations researching vortex formations under the air intakes of flying vehicles.
SUBSTANCE: the installation has a control panel, an electrical engine, a blast blower with conduits for charging and suction of air with dampers, control cocks of air consumption through air intakes and output apparatus, a block of U-shaped differential manometers for measuring of the speed of the flow in the channels of the air intakes, a wind installation. It also has a model of an aircraft and a facility of technical servicing, a gas deflector, the surface of division of mediums (an imitator of the surface of an aerodrome), lighting equipment.
EFFECT: the technical result is in getting complete picture of the processes of vortex formation under air intakes with taking into consideration the influence of the glider, the front strut if the undercarriage and distribution of the technical servicing facilities at changing of wind conditions.
2 dwg
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