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Aircraft Mechanics
Vertical Tail Volume Ratio in Directional Stability Formulas
Vertical Tail Volume Ratio relates to the area of the vertical tail, the distance between the centroid of vertical tail area and aircraft’s e.g., the wing area, and the wingspan. And is denoted by V
v
.
Formulas to find Vertical Tail Volume Ratio in Directional Stability
f
x
Vertical tail volume ratio
Go
f
x
Vertical Tail Volume Ratio for given Yawing Moment Coefficient
Go
Directional Stability formulas that make use of Vertical Tail Volume Ratio
f
x
Vertical Tail Moment Arm for given Vertical Tail Volume Ratio
Go
f
x
Vertical tail area for given vertical tail volume ratio
Go
f
x
Vertical Tail Efficiency for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Lift Curve Slope for given Vertical Tail Efficiency
Go
f
x
Wingspan for given Vertical Tail Volume Ratio
Go
f
x
Wing Area for given Vertical Tail Volume Ratio
Go
f
x
Yawing Moment Coefficient for given Vertical Tail Volume Ratio
Go
f
x
Sideslip Angle given Yawing Moment Coefficient and Tail Efficiency
Go
f
x
Sidewash Angle for given Yawing Moment Coefficient
Go
List of variables in Directional Stability formulas
f
x
Vertical Tail Moment Arm
Go
f
x
Vertical Tail Area
Go
f
x
Reference Area
Go
f
x
Wingspan
Go
f
x
Yawing Moment Coefficient
Go
f
x
Vertical Tail Efficiency
Go
f
x
Vertical Tail Lift Curve Slope
Go
f
x
Sideslip Angle
Go
f
x
Sidewash Angle
Go
FAQ
What is the Vertical Tail Volume Ratio?
Vertical Tail Volume Ratio relates to the area of the vertical tail, the distance between the centroid of vertical tail area and aircraft’s e.g., the wing area, and the wingspan.
Can the Vertical Tail Volume Ratio be negative?
{YesorNo}, the Vertical Tail Volume Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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