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Aircraft Mechanics
Rudder Deflection Angle in Static Stability and Control Formulas
Rudder Deflection Angle is a lateral force and hence a bigger yawing moment (N), leading to a more pronounced yaw. And is denoted by δ
r
. Rudder Deflection Angle is usually measured using the Radian for Angle. Note that the value of Rudder Deflection Angle is always negative.
Formulas to find Rudder Deflection Angle in Static Stability and Control
f
x
Rudder Deflection Angle given Yawing Moment Coefficient
Go
Static Stability and Control formulas that make use of Rudder Deflection Angle
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x
Yawing Moment Coefficient given Rudder Deflection
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f
x
Rudder Control Effectiveness
Go
List of variables in Static Stability and Control formulas
f
x
Dynamic Pressure at Vertical Tail
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f
x
Dynamic Pressure at Wing
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f
x
Distance between Rudder Hinge Line and Cg
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f
x
Vertical Tail Area
Go
f
x
Wingspan
Go
f
x
Wing Reference Area
Go
f
x
Lift Coefficient
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f
x
Deviated Rudder Deflection Angle
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f
x
Yawing Moment Coefficient
Go
FAQ
What is the Rudder Deflection Angle?
Rudder Deflection Angle is a lateral force and hence a bigger yawing moment (N), leading to a more pronounced yaw. Rudder Deflection Angle is usually measured using the Radian for Angle. Note that the value of Rudder Deflection Angle is always negative.
Can the Rudder Deflection Angle be negative?
Yes, the Rudder Deflection Angle, measured in Angle can be negative.
What unit is used to measure Rudder Deflection Angle?
Rudder Deflection Angle is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Rudder Deflection Angle can be measured.
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