Hands on experience with aircraft yaw control

mgupta50 154 views 9 slides May 13, 2017
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About This Presentation

Hands on experience with aircraft yaw control


Slide Content

AIRCRAFT YAW MOTION Submitted by- Prachi S ahu 14/610 Submitted to- Sir A nshul B ansal

INTRODUCTION A three dimensional coordinate system can be defined through the center of gravity with each axis of this coordinate system perpendicular to the other two axes. The orientation of the aircraft by the amount of rotation of the parts of the aircraft along these  principal axes . The  yaw axis  is perpendicular to the wings and lies in the plane of the aircraft centerline.

A  yaw motion  is a side to side movement of the nose of the aircraft. The yawing motion is being caused by the deflection of the  rudder of aircraft . The rudder is a hinged section at the rear of the vertical stabilizer.

WORKING By changing the angle of deflection at the rear of an airfoil changes the amount of lift generated by the foil. For the vertical stabilizer and rudder, the orientation of the airfoil causes a side force to be generated. With greater deflection of the rudder to the left, the side force increases to the right . With greater deflection to the right, the side force increases to the left.

The lift generated by the rudder acts through the center of pressure of the rudder and vertical stabilizer and is located at some distance from the center of gravity of the aircraft. The change in side force created by deflecting the rudder generates a torque about the center of gravity which causes the airplane to rotate. The pilot uses this ability to keep the nose of the aircraft pointed in the direction of travel.

On all aircraft, the vertical stabilizer and rudder create a symmetric airfoil .   This produces no side force when the rudder is aligned with the stabilizer and allows the combination to produce either positive or negative side force, depending on the deflection of the rudder . Some fighter planes have two vertical stabilizers and rudders because of the need to control the plane with multiple, very powerful engines.

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