An NACA 4415 airfoil is mounted in a high-speed subsonic wind tunnel
An NACA 4415 airfoil is mounted in a high-speed subsonic wind tunnel. The lift coefficient is measured as 0.85. If the test-section Mach number is 0.7, at what angle of attack is the airfoil? The correct answer and explanation is : To determine the angle of attack (α) of an NACA 4415 airfoil given the […]
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