Aerodynamics and Wing Design DS 12.12.14 contains the wing

Chapter 12, Problem 12.12.17

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Aerodynamics and Wing Design DS 12.12.14 contains the wing lift generated in various trials of an airfoil design where the angle of inclination of the airfoil to the horizontal (the angle of attack) is varied over a small range. Can a linear model be effectively used to predict the wing lift generated by an angle of attack within this range?

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