| 摘要 |
The utility model relates to the aviation. A converted aerodynamic configuration of aircraft contains a wing of large narrowing, a control surface - an elevator. For increasing the efficiency of control of glider at dive in the tail end of the wing a shutter is mounted so that in the open state it divides the wing into two parts and forms a slot with possibility of adjustment of its dimensions (for example, due to turning of shutter), and in closed state it forms with the parts of wing a continuous aerodynamic profile.
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