How to Calculate Yawing Moment with Rudder Deflection Angle?
Yawing Moment with Rudder Deflection Angle calculator uses Yawing Moment with Rudder Deflection Angle = -(Vertical Tail Efficiency Factor*Velocity at Tail Plane)*(Change in Coefficient of Lift of Tail Plane/Change in Rudder Deflection Angle) to calculate the Yawing Moment with Rudder Deflection Angle, Yawing Moment with Rudder Deflection Angle is a measure of the rotational force around the vertical axis of an aircraft, calculated by considering the vertical tail efficiency, velocity at the tail plane, and the change in coefficient of lift at the tail plane with respect to the rudder deflection angle, which is essential for understanding and controlling the aircraft's directional stability. Yawing Moment with Rudder Deflection Angle is denoted by Cnδr symbol.
How to calculate Yawing Moment with Rudder Deflection Angle using this online calculator? To use this online calculator for Yawing Moment with Rudder Deflection Angle, enter Vertical Tail Efficiency Factor (ηv), Velocity at Tail Plane (Vv), Change in Coefficient of Lift of Tail Plane (dCL,v) & Change in Rudder Deflection Angle (dδr) and hit the calculate button. Here is how the Yawing Moment with Rudder Deflection Angle calculation can be explained with given input values -> 0.968 = -((-1.1)*1.32)*(0.2/0.3).