Question: The model in a low-speed wind tunnel is a rectangular wing that spans the entire test section. The wing has a NACA 63-210 airfoil section

The model in a low-speed wind tunnel is a rectangular wing that spans the entire test section. The wing has a NACA 63-210 airfoil section and a chord of 0.145 m and span of 1.0 m. The airflow has the following properties; p = 1.01(10)5 Pa, T = 300 K, and V = 70 m/s. The lift generated by the wing is 250 N. Determine the angle of attack of the wing. Solve this problem in the International System of Units

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