The V-tail design utilizes two slanted tail surfaces to perform the same functions as the surfaces of a conventional elevator and rudder configuration. The fixed surfaces act as both horizontal and vertical stabilizers.
The movable surfaces, which are usually called ruddervators, are connected through a special linkage that allows the control wheel to move both surfaces simultaneously. On the other hand, displacement of the rudder pedals moves the surfaces differentially, thereby providing directional control. When both rudder and elevator controls are moved by the pilot, a control mixing mechanism moves each surface the appropriate amount. The control system for the V-tail is more complex than that required for a conventional tail. In addition, the V-tail design is more susceptible to Dutch roll tendencies than a conventional tail and total reduction in drag is only minimal.
Ruddervator—A pair of control surfaces on the tail of an aircraft arranged in the form of a V. These surfaces, when moved together by the control wheel, serve as elevators, and when moved differentially by the rudder pedals, serve as a rudder.
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
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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,...