Roll Control Power in Static Stability and Control Formulas

Roll Control Power is a function of the roll inertia of an airplane and the roll-control power of the ailerons. And is denoted by Cl_δα. Roll Control Power is usually measured using the Radian for Angle. Note that the value of Roll Control Power is always positive.

Formulas to find Roll Control Power in Static Stability and Control

fxRoll Control PowerGo

List of variables in Static Stability and Control formulas

fx Derivative of Wing Lift Coefficient Go

fx Flap Effectiveness Parameter Go

fx Wing Area Go

fx Wingspan Go

fx Chord Go

fx Initial Length Go

fx Final Length Go

FAQ

What is the Roll Control Power?

Roll Control Power is a function of the roll inertia of an airplane and the roll-control power of the ailerons. Roll Control Power is usually measured using the Radian for Angle. Note that the value of Roll Control Power is always positive.

Can the Roll Control Power be negative?

No, the Roll Control Power, measured in Angle cannot be negative.

What unit is used to measure Roll Control Power?

Roll Control Power is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Roll Control Power can be measured.

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