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7. A NACA 0008 airfoil rapidly changes angle of attack from 3 degrees to 8 degrees. The chord of the airfoil is 0.3 m,
7. A NACA 0008 airfoil rapidly changes angle of attack from 3 degrees to 8 degrees. The chord of the airfoil is 0.3 m, the free stream velocity is 10 m/s, and the airfoil is operating in air at standard conditions. How much circulation is shed into the wake of the airfoil? (10)
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To calculate the circulation shed into the wake of the airfoil we can use the concept of the KuttaJo...
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Fundamentals of Aerodynamics
Authors: J. Anderson
2nd Edition
978-0071254083, 1259129918, 71254080, 70016798, 9781259129919, 978-0070016798
