Physics, 30.10.2019 05:31 lilrel8602
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.
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The model in a low-speed wind tunnel is a rectangular wing that spans the entire test section. the w...
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