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 Refers to Tail Plane/Change in Rudder Deflection Angle) to calculate the Yawing Moment with Rudder Deflection Angle, The yawing moment with rudder deflection angle formula is defined as the rotational force exerted on an aircraft around its vertical axis due to the angle by which the rudder is deflected. Yawing Moment with Rudder Deflection Angle is denoted by C_{nδr} 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 (η_{v}), Velocity at Tail Plane (V_{v}), Change in Coefficient of Lift Refers to Tail Plane (d_{CL,v}) & Change in Rudder Deflection Angle (d_{δr}) 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).