With differential ailerons, one aileron is raised a greater distance than the other aileron is lowered for a given movement of the control wheel. This produces an increase in drag on the descending wing.
The greater drag results from deflecting the up aileron on the descending wing to a greater angle than the down aileron on the rising wing. While adverse yaw is reduced, it is not eliminated completely.
Brief and clear explanations of Aircraft Weight Control. This article describes about Aircraft Weight Control as a part of Aeronautical Knowledge Handbook.
AIRCRAFT SYSTEMS - OUTSIDE AIR TEMPERATURE GAUGE AND FUEL INJECTION SYSTEMS
OUTSIDE AIR TEMPERATURE GAUGE Most airplanes also are equipped with an outside air temperature (OAT) gauge calibrated in both degrees Celsi...
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The correct name for the tail section of an airplane is empennage. The empennage includes the entire tail group, consisting of fixed su...
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The control forces may be excessively high in some airplanes, and in order to decrease them, the manufacturer may use balance tabs. They loo...
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The fuselage includes the cabin and/or cockpit, which contains seats for the occupants and the controls for the airplane. In addition,...