Induced Drag Coefficient in Flow over Airfoils and Wings Formulas

The Induced Drag Coefficient is a dimensionless parameter that describes a relation between the coefficient of the lift and the aspect ratio. And is denoted by C_D,i.

Formulas to find Induced Drag Coefficient in Flow over Airfoils and Wings

fxInduced Drag CoefficientGo

fxInduced Drag Coefficient given Total Drag CoefficientGo

Flow over Airfoils and Wings formulas that make use of Induced Drag Coefficient

fxTotal Drag Coefficient for Subsonic Finite WingGo

fxProfile Drag Coefficient given Total Drag CoefficientGo

fxAspect Ratio given Span Efficiency FactorGo

List of variables in Flow over Airfoils and Wings formulas

fx Induced Drag Go

fx Free Stream Dynamic Pressure Go

fx Reference Area Go

fx Total Drag Coefficient Go

fx Profile Drag Coefficient Go

FAQ

What is the Induced Drag Coefficient?

The Induced Drag Coefficient is a dimensionless parameter that describes a relation between the coefficient of the lift and the aspect ratio.

Can the Induced Drag Coefficient be negative?

{YesorNo}, the Induced Drag Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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