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
Vertical Tail Moment Arm in Directional Stability Formulas
The Vertical Tail Moment Arm is the distance between the centroid of the vertical tail shape and the center of gravity of the aircraft. And is denoted by 𝒍
v
. Vertical Tail Moment Arm is usually measured using the Meter for Length. Note that the value of Vertical Tail Moment Arm is always positive.
Formulas to find Vertical Tail Moment Arm in Directional Stability
f
x
Vertical Tail Moment Arm for given Side Force
Go
f
x
Vertical Tail Moment Arm for given Lift Curve Slope
Go
f
x
Vertical Tail Moment Arm for Given Yawing Moment Coefficient
Go
f
x
Vertical Tail Moment Arm for given Vertical Tail Volume Ratio
Go
Directional Stability formulas that make use of Vertical Tail Moment Arm
f
x
Moment Produced by Vertical Tail for given Side Force
Go
f
x
Vertical Tail Side Force for Given Moment
Go
f
x
Moment Produced by Vertical Tail for given Lift Curve Slope
Go
f
x
Vertical Tail Lift Curve Slope for Given Moment
Go
f
x
Vertical tail volume ratio
Go
f
x
Vertical tail area for given vertical tail volume ratio
Go
f
x
Vertical Tail Area for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Lift Curve Slope for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Area for given Moment
Go
f
x
Wingspan for Yawing Moment Coefficient given Sideslip Angle and Sidewash Angle
Go
f
x
Dynamic Pressure at Wing for given Yawing Moment Coefficient
Go
f
x
Vertical Tail Dynamic Pressure for given Moment
Go
f
x
Dynamic Pressure at Vertical Tail for given Yawing Moment Coefficient
Go
f
x
Wing Area for given Yawing Moment Coefficient
Go
f
x
Wingspan for given Vertical Tail Volume Ratio
Go
f
x
Wing Area for given Vertical Tail Volume Ratio
Go
f
x
Sidewash Angle for given Moment Produced by Vertical Tail
Go
f
x
Yawing Moment Coefficient for given Vertical Tail Lift Curve Slope
Go
f
x
Sideslip Angle for given Moment Produced by Vertical Tail
Go
f
x
SideSlip Angle for given Yawing Moment Coefficient
Go
f
x
Sidewash Angle given Yawing Moment Coefficient using Wingspan
Go
List of variables in Directional Stability formulas
f
x
Vertical Tail Moment
Go
f
x
Vertical Tail Side Force
Go
f
x
Vertical Tail Lift Curve Slope
Go
f
x
Sideslip Angle
Go
f
x
Sidewash Angle
Go
f
x
Vertical Tail Dynamic Pressure
Go
f
x
Vertical Tail Area
Go
f
x
Yawing Moment Coefficient
Go
f
x
Reference Area
Go
f
x
Wingspan
Go
f
x
Wing Dynamic Pressure
Go
f
x
Vertical Tail Volume Ratio
Go
FAQ
What is the Vertical Tail Moment Arm?
The Vertical Tail Moment Arm is the distance between the centroid of the vertical tail shape and the center of gravity of the aircraft. Vertical Tail Moment Arm is usually measured using the Meter for Length. Note that the value of Vertical Tail Moment Arm is always positive.
Can the Vertical Tail Moment Arm be negative?
No, the Vertical Tail Moment Arm, measured in Length cannot be negative.
What unit is used to measure Vertical Tail Moment Arm?
Vertical Tail Moment Arm is usually measured using the Meter[m] for Length. Millimeter[m], Kilometer[m], Decimeter[m] are the few other units in which Vertical Tail Moment Arm can be measured.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!