Vertical Tail Angle of Attack in Directional Stability Formulas

Vertical Tail Angle of Attack is the angle of attack experienced by the vertical tailplane of an aircraft. And is denoted by α_v. Vertical Tail Angle of Attack is usually measured using the Radian for Angle. Note that the value of Vertical Tail Angle of Attack is always negative.

Formulas to find Vertical Tail Angle of Attack in Directional Stability

fxVertical Tail Angle of AttackGo

fxVertical Tail Angle of Attack for given Vertical Tail Side ForceGo

Directional Stability formulas that make use of Vertical Tail Angle of Attack

fxVertical Tail Side ForceGo

fxVertical Tail Lift Curve SlopeGo

fxVertical Tail Dynamic Pressure for given Vertical Tail Side ForceGo

fxVertical Tail Area for given Vertical Tail Side ForceGo

fxSideslip Angle for AircraftGo

fxSidewash angleGo

List of variables in Directional Stability formulas

fx Sidewash Angle Go

fx Sideslip Angle Go

fx Vertical Tail Side Force Go

fx Vertical Tail Lift Curve Slope Go

fx Vertical Tail Dynamic Pressure Go

fx Vertical Tail Area Go

FAQ

What is the Vertical Tail Angle of Attack?

Vertical Tail Angle of Attack is the angle of attack experienced by the vertical tailplane of an aircraft. Vertical Tail Angle of Attack is usually measured using the Radian for Angle. Note that the value of Vertical Tail Angle of Attack is always negative.

Can the Vertical Tail Angle of Attack be negative?

Yes, the Vertical Tail Angle of Attack, measured in Angle can be negative.

What unit is used to measure Vertical Tail Angle of Attack?

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

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