Vertical Tail Side Force in Directional Stability Formulas

Vertical Tail Side Force is the side force acting on the vertical tail of an aircraft. And is denoted by Y_v. Vertical Tail Side Force is usually measured using the Newton for Force. Note that the value of Vertical Tail Side Force is always negative.

Formulas to find Vertical Tail Side Force in Directional Stability

fxVertical Tail Side ForceGo

fxVertical Tail Side Force for Given MomentGo

Directional Stability formulas that make use of Vertical Tail Side Force

fxVertical Tail Lift Curve SlopeGo

fxVertical Tail Angle of Attack for given Vertical Tail Side ForceGo

fxVertical Tail Dynamic Pressure for given Vertical Tail Side ForceGo

fxVertical Tail Area for given Vertical Tail Side ForceGo

fxMoment Produced by Vertical Tail for given Side ForceGo

fxVertical Tail Moment Arm for given Side ForceGo

List of variables in Directional Stability formulas

fx Vertical Tail Lift Curve Slope Go

fx Vertical Tail Angle of Attack Go

fx Vertical Tail Area Go

fx Vertical Tail Dynamic Pressure Go

fx Vertical Tail Moment Go

fx Vertical Tail Moment Arm Go

FAQ

What is the Vertical Tail Side Force?

Vertical Tail Side Force is the side force acting on the vertical tail of an aircraft. Vertical Tail Side Force is usually measured using the Newton for Force. Note that the value of Vertical Tail Side Force is always negative.

Can the Vertical Tail Side Force be negative?

Yes, the Vertical Tail Side Force, measured in Force can be negative.

What unit is used to measure Vertical Tail Side Force?

Vertical Tail Side Force is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Vertical Tail Side Force can be measured.

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