The yawing moment is the tendency of an aircraft to rotate around its vertical axis (yaw). This motion is typically caused by asymmetrical aerodynamic forces acting on the aircraft, such as those created by the vertical tail fin.
- CnrW: Yawing moment damping coefficient contributed by the wing. This component represents the aerodynamic forces and moments generated by the wing that contribute to the damping of yawing motion.
- Cnrv: Yawing moment damping coefficient contributed by the vertical tail. This component represents the aerodynamic forces and moments generated by the vertical tail fin that contribute to the damping of yawing motion.