Moment Coefficient for Fuselage Contribution in Longitudinal Stability Formulas

The Moment Coefficient for Fuselage Contribution is the sum of the contributions of each fuselage component, including the nose, cabin, and tail cone. And is denoted by Cm_0,f.

Formulas to find Moment Coefficient for Fuselage Contribution in Longitudinal Stability

fxPitching Moment Coefficient for Fuselage ContributionGo

fxCoefficient of Pitching Moment Respect to Fuselage ContributionGo

List of variables in Longitudinal Stability formulas

fx Final Correction Factor for Body Fitness Ratio Go

fx Initial Correction Factor for Body Fitness Ratio Go

fx Wing Area Go

fx Mean Aerodynamic Chord Go

fx Average Width of Fuselage Go

fx Wing Zero Lift Angle Go

fx Incidence of Fuselage Camber Line Go

fx Wingspan Go

fx Length of Fuselage Increment Go

FAQ

What is the Moment Coefficient for Fuselage Contribution?

The Moment Coefficient for Fuselage Contribution is the sum of the contributions of each fuselage component, including the nose, cabin, and tail cone.

Can the Moment Coefficient for Fuselage Contribution be negative?

{YesorNo}, the Moment Coefficient for Fuselage Contribution, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

Let Others Know

✖

Facebook

Twitter

Copied!