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 Efficiency Factor in Static Stability and Control Formulas
Vertical Tail Efficiency Factor is defined as the ratio of the yawing moment produced by the vertical tail to the product of its surface area and the square of the wingspan. And is denoted by η
v
.
Static Stability and Control formulas that make use of Vertical Tail Efficiency Factor
f
x
Yawing Moment with Rudder Deflection Angle
Go
FAQ
What is the Vertical Tail Efficiency Factor?
Vertical Tail Efficiency Factor is defined as the ratio of the yawing moment produced by the vertical tail to the product of its surface area and the square of the wingspan.
Can the Vertical Tail Efficiency Factor be negative?
{YesorNo}, the Vertical Tail Efficiency Factor, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!