Deflection of Aileron in Static Stability and Control Formulas

The Deflection of Aileron refers to the angular displacement of the aileron control surface from its neutral position. And is denoted by δ_a. Deflection of Aileron is usually measured using the Radian for Angle. Note that the value of Deflection of Aileron is always negative.

Formulas to find Deflection of Aileron in Static Stability and Control

fxDeflection Angle given Lift CoefficientGo

Static Stability and Control formulas that make use of Deflection of Aileron

fxAileron Section lift Coefficient given Aileron DeflectionGo

fxAileron Deflection given Aileron Lift CoefficientGo

fxAileron Control Effectiveness given Aileron DeflectionGo

fxAileron Section Lift Coefficient given Control EffectivenessGo

fxLift Coefficient Slope Roll ControlGo

List of variables in Static Stability and Control formulas

fx Lift Coefficient Roll Control Go

fx Lift Coefficient Slope Roll Control Go

fx Flap Effectiveness Parameter Go

FAQ

What is the Deflection of Aileron?

The Deflection of Aileron refers to the angular displacement of the aileron control surface from its neutral position. Deflection of Aileron is usually measured using the Radian for Angle. Note that the value of Deflection of Aileron is always negative.

Can the Deflection of Aileron be negative?

Yes, the Deflection of Aileron, measured in Angle can be negative.

What unit is used to measure Deflection of Aileron?

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

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