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A NACA 4415 airfoil is mounted in a high-speed subsonic wind tunnel. The lift coefficient is measured as 0.8. If the test section Mach number
A NACA 4415 airfoil is mounted in a high-speed subsonic wind tunnel. The lift coefficient is measured as 0.8. If the test section Mach number is 0.65, at what angle of attack is the airfoil?
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