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هوافضا::
شهپر(قسمت متحرک بال)
Drag due to the aileron control linkage, dive brake caps,
and aileron hinge gaps is also included in the wing profile drag contribution.
Figure 203 shows typical force/deflection measurements for elevator and ailerons.
Specifically, it must be possible to control the sailplane in roll using ailerons atone, and there must be no significant tendency to drop a wing when both ailerons and rudder are held neutral.
• Control harmony (aileron and rudder)
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