Coefficient of Lift vs Angle of Attack

A Graph of AOA on the X Axis vs CL on the Y Axis.

X Axis scale is -180 degrees to + 180 degrees. Y Axis scale is -2 to + 2.

Aerofoil shape

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Coefficient of Lift vs Angle of Attack

A Graph of AOA on the X Axis vs CL on the Y Axis.

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