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Aircraft Mechanics
Tail Incidence Angle in Longitudinal Stability Formulas
Tail Incidence Angle is the angle between the reference chord of the horizontal tail and the fuselage reference line. And is denoted by 𝒊
t
. Tail Incidence Angle is usually measured using the Radian for Angle. Note that the value of Tail Incidence Angle is always negative.
Formulas to find Tail Incidence Angle in Longitudinal Stability
f
x
Angle of incidence of tail
Go
Longitudinal Stability formulas that make use of Tail Incidence Angle
f
x
Angle of Attack at Tail
Go
f
x
Angle of Attack of Wing
Go
f
x
Angle of incidence of wing
Go
f
x
Downwash angle
Go
List of variables in Longitudinal Stability formulas
f
x
Horizontal Tail Angle of Attack
Go
f
x
Wing Angle of Attack
Go
f
x
Wing Incidence Angle
Go
f
x
Downwash Angle
Go
FAQ
What is the Tail Incidence Angle?
Tail Incidence Angle is the angle between the reference chord of the horizontal tail and the fuselage reference line. Tail Incidence Angle is usually measured using the Radian for Angle. Note that the value of Tail Incidence Angle is always negative.
Can the Tail Incidence Angle be negative?
Yes, the Tail Incidence Angle, measured in Angle can be negative.
What unit is used to measure Tail Incidence Angle?
Tail Incidence Angle is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Tail Incidence Angle can be measured.
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