7. A NACA 0008 airfoil rapidly changes angle of attack from 3 degrees to 8 degrees....

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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, 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) 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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The question provided is related to the concept of circulation in aerodynamics specifically referring to a scenario in which an airfoil changes its an... View the full answer