Skin Friction Drag Coefficient in Flow over Airfoils and Wings Formulas

Skin Friction Drag Coefficient is obtained by dividing the skin friction drag by the product of dynamic pressure and reference area. And is denoted by C_f.

Formulas to find Skin Friction Drag Coefficient in Flow over Airfoils and Wings

fxSkin Friction Drag Coefficient for Flat Plate in Laminar FlowGo

fxSkin Friction Drag Coefficient for Flat Plate in Turbulent FlowGo

List of variables in Flow over Airfoils and Wings formulas

fx Reynolds Number for Laminar Flow Go

fx Reynolds Number for Turbulent Flow Go

FAQ

What is the Skin Friction Drag Coefficient?

Skin Friction Drag Coefficient is obtained by dividing the skin friction drag by the product of dynamic pressure and reference area.

Can the Skin Friction Drag Coefficient be negative?

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

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