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Aircraft Mechanics
Tail Efficiency in Longitudinal Stability Formulas
Tail Efficiency is defined as the ratio of dynamic pressure associated with the tail to dynamic pressure associated with an aircraft’s wing. And is denoted by η.
Formulas to find Tail Efficiency in Longitudinal Stability
f
x
Tail Efficiency for given Pitching Moment Coefficient
Go
f
x
Tail Efficiency for given Tail Volume Ratio
Go
f
x
Tail Efficiency for given lift coefficients
Go
Longitudinal Stability formulas that make use of Tail Efficiency
f
x
Tail Pitching Moment Coefficient for given Tail Efficiency
Go
f
x
Tail Moment Arm for given Tail Moment Coefficient
Go
f
x
Tail Area for given Tail Moment Coefficient
Go
f
x
Tail Pitching Moment Coefficient for given Tail Volume Ratio
Go
f
x
Horizontal Tail Volume Ratio for given Pitching Moment Coefficient
Go
f
x
Tail Lift Coefficient for given Tail Volume Ratio
Go
f
x
Total Lift Coefficient of Wing-Tail Combination
Go
f
x
Wing Lift Coefficient of wing-tail combination
Go
f
x
Tail Lift Coefficient of Wing-Tail Combination
Go
f
x
Tail area for given tail efficiency
Go
f
x
Tail Lift Coefficient for given Pitching Moment Coefficient
Go
List of variables in Longitudinal Stability formulas
f
x
Tail Pitching Moment Coefficient
Go
f
x
Reference Area
Go
f
x
Mean Aerodynamic Chord
Go
f
x
Horizontal Tail Moment Arm
Go
f
x
Horizontal Tail Area
Go
f
x
Tail Lift Coefficient
Go
f
x
Horizontal Tail Volume Ratio
Go
f
x
Lift Coefficient
Go
f
x
Wing Lift Coefficient
Go
FAQ
What is the Tail Efficiency?
Tail Efficiency is defined as the ratio of dynamic pressure associated with the tail to dynamic pressure associated with an aircraft’s wing.
Can the Tail Efficiency be negative?
{YesorNo}, the Tail Efficiency, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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