FIELD: aeronautical engineering; manufacture of aeroplanes with control surfaces in form of ailerons, elevators and rudders. SUBSTANCE: control surface with axial compensation has contour of tip and lower and upper surfaces on which semi-cones changing on trailing edge into corrugation with end shear. Corrugation has amplitude not exceeding half maximum thickness of control surface. EFFECT: enhanced efficiency and improved aerodynamic characteristics of flying vehicle. 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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