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Aircraft Mechanics
Horizontal Tail Volume Ratio in Longitudinal Stability Formulas
Horizontal Tail Volume Ratio relates the area of the horizontal tail, the distance between tail and aircraft’s c.g., the wing area, and the mean aerodynamic wing chord. And is denoted by V
H
.
Formulas to find Horizontal Tail Volume Ratio in Longitudinal Stability
f
x
Horizontal tail volume ratio
Go
f
x
Horizontal Tail Volume Ratio for given Pitching Moment Coefficient
Go
Longitudinal Stability formulas that make use of Horizontal Tail Volume Ratio
f
x
Tail moment arm for given horizontal tail volume ratio
Go
f
x
Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio
Go
f
x
Wing Reference Area for given Horizontal Tail Volume Ratio
Go
f
x
Horizontal tail area for given tail volume ratio
Go
f
x
Tail Pitching Moment Coefficient for given Tail Volume Ratio
Go
f
x
Tail Efficiency for given Tail Volume Ratio
Go
f
x
Tail Lift Coefficient for given Tail Volume Ratio
Go
List of variables in Longitudinal Stability formulas
f
x
Horizontal Tail Moment Arm
Go
f
x
Horizontal Tail Area
Go
f
x
Reference Area
Go
f
x
Mean Aerodynamic Chord
Go
f
x
Tail Pitching Moment Coefficient
Go
f
x
Tail Efficiency
Go
f
x
Tail Lift Coefficient
Go
FAQ
What is the Horizontal Tail Volume Ratio?
Horizontal Tail Volume Ratio relates the area of the horizontal tail, the distance between tail and aircraft’s c.g., the wing area, and the mean aerodynamic wing chord.
Can the Horizontal Tail Volume Ratio be negative?
{YesorNo}, the Horizontal Tail Volume Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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