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For cylinders coefficient of lift is approximately half of coefficient of drag while they are equal for Aerofoils.

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For cylinders coefficient of lift is approximately half of coefficient of drag while they are equal for Aerofoils.

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coefficient of drag in 0 lift

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0.08

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0.016

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It depends on the Reduced Velocity and amplitude of oscillation. Lift Coefficient could be as high as 1.0, and as low as -10.0 at very low reduced velocities.

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