Let’s say this airfoil was used in a specific airplane. This airplane is flying at 135 mph (60.4 m/s), has a wing area of 150 ft2 (13.94 m2), and flying at an angle of attack of 1º. How much lift will the wings generate? Use the lift equation that was discussed in Lecture 11, and give your answer in Newtons. Also, use an air density of 1.22 kg/m3
** 1 degree of attack is 0.65.
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