Yawing Moment evaluator uses Yawing Moment = Yawing Moment Coefficient*Dynamic Pressure*Reference Area*Characteristic Length to evaluate the Yawing Moment, Yawing Moment is a measure of the rotational force that causes an aircraft to turn or yaw around its vertical axis, affected by factors such as air density, wing surface area, and length of the aircraft, it is a critical parameter in aerodynamics, influencing the stability and control of an aircraft during flight. Yawing Moment is denoted by 𝑵 symbol.
How to evaluate Yawing Moment using this online evaluator? To use this online evaluator for Yawing Moment, enter Yawing Moment Coefficient (Cn), Dynamic Pressure (q), Reference Area (S) & Characteristic Length (𝓁) and hit the calculate button.