Derivative of Wing Lift Coefficient in Static Stability and Control Formulas

Derivative of Wing Lift Coefficient is the lift curve slope, which is a measure of how much lift changes when the angle of attack of an aircraft changes. And is denoted by C_lαw.

Static Stability and Control formulas that make use of Derivative of Wing Lift Coefficient

fxAileron Deflection given Aileron Lift CoefficientGo

fxRoll Control PowerGo

fxRoll Damping CoefficientGo

FAQ

What is the Derivative of Wing Lift Coefficient?

Derivative of Wing Lift Coefficient is the lift curve slope, which is a measure of how much lift changes when the angle of attack of an aircraft changes.

Can the Derivative of Wing Lift Coefficient be negative?

{YesorNo}, the Derivative of Wing Lift Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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