Induced Lift Slope Factor in Flow over Airfoils and Wings Formulas

The Induced Lift Slope Factor 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.

Flow over Airfoils and Wings formulas that make use of Induced Lift Slope Factor

fx2D Lift Curve Slope of Airfoil given Lift Slope of Finite WingGo

fxAspect Ratio of Wing given Lift Curve Slope of Finite WingGo

fxLift Curve Slope for Finite WingGo

FAQ

What is the Induced Lift Slope Factor?

The Induced Lift Slope Factor 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 be negative?

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

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