Moment Coefficient about Leading Edge in Flow over Airfoils and Wings Formulas

Moment Coefficient about Leading Edge is obtained by dividing the moment about the leading edge by the dynamic pressure, the area, and the chord of the airfoil. And is denoted by C_m,le.

Formulas to find Moment Coefficient about Leading Edge in Flow over Airfoils and Wings

fxMoment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil TheoryGo

Flow over Airfoils and Wings formulas that make use of Moment Coefficient about Leading Edge

fxCenter of Pressure Location for Cambered AirfoilGo

List of variables in Flow over Airfoils and Wings formulas

fx Lift Coefficient Go

FAQ

What is the Moment Coefficient about Leading Edge?

Moment Coefficient about Leading Edge is obtained by dividing the moment about the leading edge by the dynamic pressure, the area, and the chord of the airfoil.

Can the Moment Coefficient about Leading Edge be negative?

{YesorNo}, the Moment Coefficient about Leading Edge, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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