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Aircraft Mechanics
Tail Pitching Moment Coefficient in Longitudinal Stability Formulas
Tail Pitching Moment Coefficient is the coefficient of pitching moment associated with the horizontal tail of an aircraft. And is denoted by Cm
t
.
Formulas to find Tail Pitching Moment Coefficient in Longitudinal Stability
f
x
Tail Pitching Moment Coefficient
Go
f
x
Tail Pitching Moment Coefficient for given Tail Efficiency
Go
f
x
Tail Pitching Moment Coefficient for given Tail Volume Ratio
Go
Longitudinal Stability formulas that make use of Tail Pitching Moment Coefficient
f
x
Tail Pitching Moment for given Moment Coefficient
Go
f
x
Mean Aerodynamic Chord for given Tail Pitching Moment Coefficient
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 Efficiency for given Pitching Moment Coefficient
Go
f
x
Horizontal Tail Volume Ratio for given Pitching Moment Coefficient
Go
f
x
Tail Efficiency for given Tail Volume Ratio
Go
f
x
Tail Lift Coefficient for given Tail Volume Ratio
Go
f
x
Tail Lift Coefficient for given Pitching Moment Coefficient
Go
List of variables in Longitudinal Stability formulas
f
x
Pitching Moment due to Tail
Go
f
x
Freestream Density
Go
f
x
Flight Velocity
Go
f
x
Reference Area
Go
f
x
Mean Aerodynamic Chord
Go
f
x
Tail Efficiency
Go
f
x
Horizontal Tail Area
Go
f
x
Horizontal Tail Moment Arm
Go
f
x
Tail Lift Coefficient
Go
f
x
Horizontal Tail Volume Ratio
Go
FAQ
What is the Tail Pitching Moment Coefficient?
Tail Pitching Moment Coefficient is the coefficient of pitching moment associated with the horizontal tail of an aircraft.
Can the Tail Pitching Moment Coefficient be negative?
{YesorNo}, the Tail Pitching Moment Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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