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Aircraft Mechanics
Yawing Moment Coefficient in Static Stability and Control Formulas
Yawing moment coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis. And is denoted by C
n
.
Formulas to find Yawing Moment Coefficient in Static Stability and Control
f
x
Yawing Moment Coefficient given Rudder Deflection
Go
f
x
Yawing Moment given Rudder Deflection
Go
f
x
Rudder Control Effectiveness
Go
Static Stability and Control formulas that make use of Yawing Moment Coefficient
f
x
Rudder Deflection Angle given Yawing Moment Coefficient
Go
List of variables in Static Stability and Control formulas
f
x
Dynamic Pressure at Vertical Tail
Go
f
x
Dynamic Pressure at Wing
Go
f
x
Distance between Rudder Hinge Line and Cg
Go
f
x
Vertical Tail Area
Go
f
x
Wingspan
Go
f
x
Wing Reference Area
Go
f
x
Coefficient of Lift
Go
f
x
Deviated Rudder Deflection Angle
Go
f
x
Rudder Deflection Angle
Go
f
x
Negative Yawing Moment
Go
f
x
Yawing Moment with Rudder Deflection Angle
Go
FAQ
What is the Yawing Moment Coefficient?
Yawing moment coefficient is the coefficient associated with the moment that tends to rotate an airplane about its vertical (or yaw) axis.
Can the Yawing Moment Coefficient be negative?
{YesorNo}, the Yawing Moment Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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