The ailerons, which act in opposite directions, are used to roll the aircraft while in straight line flight, and also to assist in turns, when used with rudder.
Aircraft turn is technically termed as banking. It is achieved by combined work of aileron and rudder...
Right Aileron Down is Positive Left Aileron Up is Positive Rudder Left is Positive Elevator Down if Positive The oposites are negative, of course.
The ailerons primarily control roll. Whenever lift is increased, induced drag is also increased. When the stick is moved left to bank the aircraft to the left, the right aileron is lowered which increases lift on the right wing and therefore increases induced drag on the right wing. Using ailerons causes adverse yaw, meaning the nose of the aircraft yaws in a direction opposite to the aileron application. When moving the stick to the left to bank the wings, adverse yaw moves the nose of the aircraft to the right. Adverse yaw is more pronounced for light aircraft with long wings, such as gliders. It is counteracted by the pilot with the rudder. Differential ailerons are ailerons which have been rigged such that the downgoing aileron deflects less than the upward-moving one, reducing adverse yaw. [edit]
Propellers Flaps Elevators Rudder Fuselage Wings Aileron
Ailerons are hinged control surfaces attached to the trailing edge of the wing of a fixed-wing aircraft. The ailerons are used to control the aircraft in roll. The two ailerons are typically interconnected so that one goes down when the other goes up: the downgoing aileron increases the lift on its wing while the upgoing aileron reduces the lift on the other wing, producing a rolling moment about the aircraft's longitudinal axis. The word aileron is French for "little wing."The ailerons are control via the control column inside an aircraft's cockpit. If the control column is turned right, for example, then the right wing aileron will move upwards and the right wing will move downwards and the left wing aileron will move downwards and the left wing will lift, and the aircraft will roll right.On the tail of a fixed wing aircraft, the rudder is also used to conter-act the unwanted yaw, and is controlled by the foot pedals inside the cockpit. When the aircraft is rolled right using the ailerons, the rudder is turned right to help the aircraft begin its turn.The parts that help to bank the airplane are called the ailerons (on the wing next to the 'flaps') and the rudder (on the tail under the 'elevators').Read more: What_part_banks_the_airplane
"Dutch Roll" is a coordination training maneuver sometimes taught to student pilots to help them improve their "stick-and-rudder" technique. The aircraft is alternately rolled as much as 60-degrees left and right while rudder is applied to keep the nose of the aircraft pointed at a fixed point. This is sometimes called "rolling on a fixed heading".The aircraft is rolled in such a way as to maintain an accurate heading without the nose moving from side-to-side (or yawing). The unwanted yaw motion is induced due to aileron drag: The lifting wing (aileron down) is creating more lift than the descending wing (aileron up) and therefore it creates more drag. This pushes the raised wing to the rear, yawing the aircraft toward the raised wing. The pilot counters the yaw by applying rudder in the same direction as the aileron control (left stick, left rudder - right stick, right rudder).A good Dutch Roll involves a series of oscillations in which the pilot maximizes roll while minimizing yaw.As each type of aircraft behaves differently, learning the correct amount and timing of rudder movement can be difficult. The aircraft's configuration and engine thrust settings can make a large difference. Dutch rolls are considerably easier to execute in a glider than in a single-engine aircraft with a nose-mounted propeller.
The wings of an airplane bank to allow it to turn left or right by tilting the wings in the desired direction. This banking motion creates a horizontal component of lift that changes the direction of the aircraft.
Aircraft are controlled in flight by the use of main control stick operating the ailerons and elevator, and the rudder pedals operating the rudder.
The four parts are the Aileron, Spoilers, Flaps, and Slats. Others are the Elevator, and Rudder
The rudder is a part of the vertical stabilizer on an aircraft. When desired, it can move to the left, or the right. The rudder sticking out into the wind creates drag, which causes the aircraft to move along the Yaw axis (left to right).
All aircraft have rudders apart from helicopters. The rudder is used for turning the aircraft while its on the ground or it can be used for moving the nose of the aircraft side to side while flying at low speed.