FormulaDen.com
Physics
Chemistry
Math
Chemical Engineering
Civil
Electrical
Electronics
Electronics and Instrumentation
Materials Science
Mechanical
Production Engineering
Financial
Health
You are here
-
Home
»
Physics
»
Aerospace
»
Aircraft Mechanics
Horizontal Tail Angle of Attack in Longitudinal Stability Formulas
The Horizontal Tail Angle of Attack (AoA) refers to the angle between the chord line of the horizontal stabilizer (including the elevator) and the relative airflow. And is denoted by α
t
. Horizontal Tail Angle of Attack is usually measured using the Radian for Angle. Note that the value of Horizontal Tail Angle of Attack is always negative.
Formulas to find Horizontal Tail Angle of Attack in Longitudinal Stability
f
x
Angle of Attack at Tail
Go
Longitudinal Stability formulas that make use of Horizontal Tail Angle of Attack
f
x
Angle of Attack of Wing
Go
f
x
Angle of incidence of wing
Go
f
x
Downwash angle
Go
f
x
Angle of incidence of tail
Go
List of variables in Longitudinal Stability formulas
f
x
Wing Angle of Attack
Go
f
x
Wing Incidence Angle
Go
f
x
Downwash Angle
Go
f
x
Tail Incidence Angle
Go
FAQ
What is the Horizontal Tail Angle of Attack?
The Horizontal Tail Angle of Attack (AoA) refers to the angle between the chord line of the horizontal stabilizer (including the elevator) and the relative airflow. Horizontal Tail Angle of Attack is usually measured using the Radian for Angle. Note that the value of Horizontal Tail Angle of Attack is always negative.
Can the Horizontal Tail Angle of Attack be negative?
Yes, the Horizontal Tail Angle of Attack, measured in Angle can be negative.
What unit is used to measure Horizontal Tail Angle of Attack?
Horizontal Tail Angle of Attack is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Horizontal Tail Angle of Attack can be measured.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!