Wing Aspect Ratio GLD in Lift Distribution Formulas

Wing Aspect Ratio GLD is defined as the ratio of the square of wingspan to the wing area or wingspan over wing chord for a rectangular planform. And is denoted by AR_GLD.

Formulas to find Wing Aspect Ratio GLD in Lift Distribution

fxAspect Ratio given Induced Drag FactorGo

Lift Distribution formulas that make use of Wing Aspect Ratio GLD

fxLift Coefficient given Span Efficiency FactorGo

fxInduced Drag Coefficient given Span Efficiency FactorGo

fxInduced Lift Slope Factor given Lift Curve Slope of Finite WingGo

fxInduced Drag Factor given Induced Drag CoefficientGo

fxLift Coefficient given Induced Drag FactorGo

fxSpan Efficiency Factor given Induced Drag CoefficientGo

fxInduced Drag Coefficient given Induced Drag FactorGo

List of variables in Lift Distribution formulas

fx Induced Drag Factor Go

fx Lift Coefficient GLD Go

fx Induced Drag Coefficient GLD Go

FAQ

What is the Wing Aspect Ratio GLD?

Wing Aspect Ratio GLD is defined as the ratio of the square of wingspan to the wing area or wingspan over wing chord for a rectangular planform.

Can the Wing Aspect Ratio GLD be negative?

{YesorNo}, the Wing Aspect Ratio GLD, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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