FIELD: aviation.
SUBSTANCE: streamlining control is based on changing the direction of the incoming airflow from the counter to the radial outflow relative to the aircraft (LA) using a heated, gas-permeable porous insert on the aircraft front end. The heating of the gas-permeable porous insert is carried out by means of electric induction heating.
EFFECT: simplification of the system of influencing the flow and increasing the speed of streamlining control.
1 dwg
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Authors
Dates
2017-06-01—Published
2015-12-16—Filed