Using the Prandtl-Glauert rule, calculate the lift coefficient for an NACA 2412 airfoil at 5 angle of

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Using the Prandtl-Glauert rule, calculate the lift coefficient for an NACA 2412 airfoil at 5° angle of attack in a Mach 0.6 free stream. (Refer to Fig. 4.5 for the original airfoil data.)

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