Question: Consider an airplane having an aspect ratio 4 . 1 . The lift curve for the airfoil of the wing of this aircraft is shown

Consider an airplane having an aspect ratio 4.1.
The lift curve for the airfoil of the wing of this aircraft is shown below.
What is the induced drag coefficient CDi if the aircraft is flying at 3 degrees? You may assume an elliptical lift distribution. Check your units!
Consider an airplane having an aspect ratio 4 . 1

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