Question: The wing with aspect ratio A = 5 has a drag coefficient Cp = 0.01 when the lift coefficient is C = 0.8. Evaluate
The wing with aspect ratio A = 5 has a drag coefficient Cp = 0.01 when the lift coefficient is C = 0.8. Evaluate the drag coefficient for the wing with A = 10 at the same value of lift coefficient. Evaluate also the profile drag.
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