A NACA 4415 airfoil is mounted in a high-speed subsonic wind tunnel. The lift coefficient is measured

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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 is 0.65, at what angle of attack is the airfoil?

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Fundamentals Of Aerodynamics

ISBN: 9781259129919

6th Edition

Authors: John Anderson

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Posted Date: May 13, 2024 01:18 PM

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A NACA 4415 airfoil is mounted in a high-speed subsonic wind tunnel. The lift coefficient is measured

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Expert Answer:

To determine the angle of attack we need to use the lift coefficient data and the Mach numb... View the full answer

Fundamentals Of Aerodynamics

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