Question: 5 . 2 Consider an infinite wing with a NACA 1 4 1 2 airfoil section and a chord length of 3 ft . The

5.2 Consider an infinite wing with a NACA 1412 airfoil section and a chord
length of 3 ft . The wing is at an angle of attack of 5 in an airflow velocity
of 100fts at standard sea-level conditions. Calculate the lift, drag, and
moment about the quarter-chord per unit span.
5 . 2 Consider an infinite wing with a NACA 1 4 1

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