Question: A rectangular wing with a NACA 0 0 0 6 airfoil section having an aspect ratio of 3 . 5 is flying at M =

A rectangular wing with a NACA 0006 airfoil section having an aspect ratio of 3.5 is
flying at M =0.85 at a height of 12 km. What is the airfoil section and the aspect
ratio for an equivalent wing in an incompressible flow?
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