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Aircraft Mechanics
Vertical Tail Area in Directional Stability Formulas
The Vertical Tail Area is the area of the surface of the vertical tail, including the submerged area to the fuselage centerline. And is denoted by S
v
. Vertical Tail Area is usually measured using the Square Meter for Area. Note that the value of Vertical Tail Area is always positive.
Formulas to find Vertical Tail Area in Directional Stability
f
x
Vertical Tail Area for given Vertical Tail Side Force
Go
f
x
Vertical tail area for given vertical tail volume ratio
Go
f
x
Vertical Tail Area for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Area for given Moment
Go
Directional Stability formulas that make use of Vertical Tail Area
f
x
Vertical Tail Side Force
Go
f
x
Vertical Tail Lift Curve Slope
Go
f
x
Vertical Tail Angle of Attack for given Vertical Tail Side Force
Go
f
x
Vertical Tail Dynamic Pressure for given Vertical Tail Side Force
Go
f
x
Moment Produced by Vertical Tail for given Lift Curve Slope
Go
f
x
Vertical Tail Moment Arm for given Lift Curve Slope
Go
f
x
Vertical Tail Lift Curve Slope for Given Moment
Go
f
x
Vertical Tail Moment Arm for Given Yawing Moment Coefficient
Go
f
x
Vertical tail volume ratio
Go
f
x
Vertical Tail Moment Arm for given Vertical Tail Volume Ratio
Go
f
x
Vertical Tail Lift Curve Slope for given Yawing Moment Coefficient
Go
f
x
Wingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle
Go
f
x
Dynamic Pressure at Wing for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Dynamic Pressure for given Moment
Go
f
x
Dynamic Pressure at Vertical Tail for given Yawing Moment Coefficient
Go
f
x
Wing Area for given Yawing Moment Coefficient
Go
f
x
Wingspan for given Vertical Tail Volume Ratio
Go
f
x
Wing Area for given Vertical Tail Volume Ratio
Go
f
x
Sidewash Angle for given Moment Produced by Vertical Tail
Go
f
x
Yawing Moment Coefficient for given Vertical Tail Lift Curve Slope
Go
f
x
Sideslip Angle for given Moment Produced by Vertical Tail
Go
f
x
SideSlip Angle for given Yawing Moment Coefficient
Go
f
x
Sidewash Angle given Yawing Moment Coefficient using Wingspan
Go
List of variables in Directional Stability formulas
f
x
Vertical Tail Side Force
Go
f
x
Vertical Tail Lift Curve Slope
Go
f
x
Vertical Tail Angle of Attack
Go
f
x
Vertical Tail Dynamic Pressure
Go
f
x
Vertical Tail Volume Ratio
Go
f
x
Reference Area
Go
f
x
Wingspan
Go
f
x
Vertical Tail Moment Arm
Go
f
x
Yawing Moment Coefficient
Go
f
x
Wing Dynamic Pressure
Go
f
x
Sideslip Angle
Go
f
x
Sidewash Angle
Go
f
x
Vertical Tail Moment
Go
FAQ
What is the Vertical Tail Area?
The Vertical Tail Area is the area of the surface of the vertical tail, including the submerged area to the fuselage centerline. Vertical Tail Area is usually measured using the Square Meter for Area. Note that the value of Vertical Tail Area is always positive.
Can the Vertical Tail Area be negative?
No, the Vertical Tail Area, measured in Area cannot be negative.
What unit is used to measure Vertical Tail Area?
Vertical Tail Area is usually measured using the Square Meter[m²] for Area. Square Kilometer[m²], Square Centimeter[m²], Square Millimeter[m²] are the few other units in which Vertical Tail Area can be measured.
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