How to Calculate Yawing Moment Coefficient given Rudder Deflection?
Yawing Moment Coefficient given Rudder Deflection calculator uses Yawing Moment Coefficient = -(Dynamic Pressure at Vertical Tail/Dynamic Pressure at Wing)*((Distance between Rudder Hinge Line and Cg*Vertical Tail Area)/(Wingspan*Wing Reference Area))*(Coefficient of Lift/Deviated Rudder Deflection Angle)*Rudder Deflection Angle to calculate the Yawing Moment Coefficient, Yawing Moment Coefficient given Rudder Deflection is a measure of the rotational force around the vertical axis of an aircraft, caused by the deflection of the rudder, and is influenced by the dynamic pressure at the vertical tail, the distance between the rudder hinge line and center of gravity, and the wing reference area, this coefficient is a critical parameter in aircraft design, as it affects the stability and control of the aircraft during flight. Yawing Moment Coefficient is denoted by Cn symbol.
How to calculate Yawing Moment Coefficient given Rudder Deflection using this online calculator? To use this online calculator for Yawing Moment Coefficient given Rudder Deflection, enter Dynamic Pressure at Vertical Tail (Qv), Dynamic Pressure at Wing (Qw), Distance between Rudder Hinge Line and Cg (lv), Vertical Tail Area (Sv), Wingspan (b), Wing Reference Area (s), Coefficient of Lift (dcl), Deviated Rudder Deflection Angle (dδr) & Rudder Deflection Angle (δr) and hit the calculate button. Here is how the Yawing Moment Coefficient given Rudder Deflection calculation can be explained with given input values -> 7.614642 = -(60/90)*((5.5*5)/(6.7*8.5))*((-3.9)/1.3)*7.5.