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Aircraft Mechanics
Vertical Tail Efficiency in Directional Stability Formulas
Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft. And is denoted by η
v
.
Formulas to find Vertical Tail Efficiency in Directional Stability
f
x
Vertical Tail Efficiency
Go
f
x
Vertical Tail Efficiency for given Yawing Moment Coefficient
Go
Directional Stability formulas that make use of Vertical Tail Efficiency
f
x
Vertical Tail Volume Ratio for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Lift Curve Slope for given Vertical Tail Efficiency
Go
f
x
Dynamic Pressure at Wing for given Vertical Tail Efficiency
Go
f
x
Dynamic Pressure at Vertical Tail for given Vertical Tail Efficiency
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 Dynamic Pressure
Go
f
x
Wing Dynamic Pressure
Go
f
x
Yawing Moment Coefficient
Go
f
x
Vertical Tail Volume Ratio
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 Efficiency?
Vertical Tail Efficiency is the tail efficiency associated with the vertical tail of an aircraft.
Can the Vertical Tail Efficiency be negative?
{YesorNo}, the Vertical Tail Efficiency, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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