FIELD: aviation.
SUBSTANCE: invention relates to aircraft flight control means. Aerodynamic surface is provided with a steering wheel having axial compensation. Cross-sectional profile of the aerodynamic surface on the whole span or part of its span is clipped at least from one side of this profile directly in front of the steering wheel.
EFFECT: invention is aimed at reducing the aerodynamic drag of an aerodynamic surface with the undeflected steering wheel without reducing the efficiency of the steering wheel and without increasing the pivot points in case of the steering wheel deviation.
5 cl, 4 dwg
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Authors
Dates
2018-12-18—Published
2017-12-20—Filed