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Aircraft Mechanics
Change in Rudder Deflection Angle in Static Stability and Control Formulas
The change in rudder deflection angle refers to the variation in the angle by which the rudder is deflected from its initial position. And is denoted by d
δr
.
Static Stability and Control formulas that make use of Change in Rudder Deflection Angle
f
x
Yawing Moment with Rudder Deflection Angle
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FAQ
What is the Change in Rudder Deflection Angle?
The change in rudder deflection angle refers to the variation in the angle by which the rudder is deflected from its initial position.
Can the Change in Rudder Deflection Angle be negative?
{YesorNo}, the Change in Rudder Deflection Angle, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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