Angle of Zero Lift in Flow over Airfoils and Wings Formulas

The Angle of Zero Lift is the angle of attack at which an airfoil does not produce any lift. And is denoted by α₀. Angle of Zero Lift is usually measured using the Degree for Angle. Note that the value of Angle of Zero Lift is always negative. Typically, the value of Angle of Zero Lift lies in the range from -3 to 1.5.

Flow over Airfoils and Wings formulas that make use of Angle of Zero Lift

fxLift Coefficient for Cambered AirfoilGo

FAQ

What is the Angle of Zero Lift?

The Angle of Zero Lift is the angle of attack at which an airfoil does not produce any lift. Angle of Zero Lift is usually measured using the Degree for Angle. Note that the value of Angle of Zero Lift is always negative. Typically, the value of Angle of Zero Lift lies in the range from -3 to 1.5.

Can the Angle of Zero Lift be negative?

Yes, the Angle of Zero Lift, measured in Angle can be negative.

What unit is used to measure Angle of Zero Lift?

Angle of Zero Lift is usually measured using the Degree[°] for Angle. Radian[°], Minute[°], Second[°] are the few other units in which Angle of Zero Lift can be measured.

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