Change in Coefficient of Lift of Tail Plane in Static Stability and Control Formulas

The Change in Coefficient of Lift of Tail Plane refers to the variation in lift generated by the tailplane of an aircraft. And is denoted by d_CL,v.

Static Stability and Control formulas that make use of Change in Coefficient of Lift of Tail Plane

fxYawing Moment with Rudder Deflection AngleGo

What is the Change in Coefficient of Lift of Tail Plane?

The Change in Coefficient of Lift of Tail Plane refers to the variation in lift generated by the tailplane of an aircraft.

Can the Change in Coefficient of Lift of Tail Plane be negative?

{YesorNo}, the Change in Coefficient of Lift of Tail Plane, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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