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
Incidence of Fuselage Camber Line in Longitudinal Stability Formulas
The Incidence of Fuselage Camber Line relative to the fuselage reference line refers to the angle formed between the camber line of the fuselage and the reference line of the fuselage. And is denoted by i
f
.
Longitudinal Stability formulas that make use of Incidence of Fuselage Camber Line
f
x
Pitching Moment Coefficient for Fuselage Contribution
Go
f
x
Coefficient of Pitching Moment Respect to Fuselage Contribution
Go
FAQ
What is the Incidence of Fuselage Camber Line?
The Incidence of Fuselage Camber Line relative to the fuselage reference line refers to the angle formed between the camber line of the fuselage and the reference line of the fuselage.
Can the Incidence of Fuselage Camber Line be negative?
{YesorNo}, the Incidence of Fuselage Camber Line, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!