Question: assuming that this surface is located 2 0 feet behind the wing? Is this force upwards, or downwards? Assume that, due to its shape, it

assuming that this surface is located 20 feet behind the wing? Is this force upwards, or downwards?
Assume that, due to its shape, it has an Oswald efficiency of 0.88. The wing features a NACA 4416 airfoil without flaps. What is the induced drag coefficient of this wing if it is operating at an angle of attack of 6 degrees?
assuming that this surface is located 2 0 feet

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