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
Final Correction Factor for Body Fitness Ratio in Longitudinal Stability Formulas
Final Correction Factor for Body Fitness Ratio can be quantified by the fuselage fineness ratio (FR), defined as the body length divided by its maximum diameter. And is denoted by k
2
.
Longitudinal Stability formulas that make use of Final Correction Factor for Body Fitness Ratio
f
x
Pitching Moment Coefficient for Fuselage Contribution
Go
FAQ
What is the Final Correction Factor for Body Fitness Ratio?
Final Correction Factor for Body Fitness Ratio can be quantified by the fuselage fineness ratio (FR), defined as the body length divided by its maximum diameter.
Can the Final Correction Factor for Body Fitness Ratio be negative?
{YesorNo}, the Final Correction Factor for Body Fitness Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!