Induced Lift Slope Factor of Finite Wing in Lift Distribution Formulas

The Induced Lift Slope Factor of Finite Wing is a function of the Fourier coefficients which have been used for the lift curve slope expression for the finite wing of the general planform. And is denoted by τ_FW.

Formulas to find Induced Lift Slope Factor of Finite Wing in Lift Distribution

fxInduced Lift Slope Factor given Lift Curve Slope of Finite WingGo

List of variables in Lift Distribution formulas

fx Wing Aspect Ratio GLD Go

fx 2D Lift Curve Slope Go

fx Lift Curve Slope Go

FAQ

What is the Induced Lift Slope Factor of Finite Wing?

The Induced Lift Slope Factor of Finite Wing is a function of the Fourier coefficients which have been used for the lift curve slope expression for the finite wing of the general planform.

Can the Induced Lift Slope Factor of Finite Wing be negative?

{YesorNo}, the Induced Lift Slope Factor of Finite Wing, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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