Question: Consider a light, single-engine airplane, such as the Piper Super Cub. If the maximum gross weight of the airplane is 6700 N, the wing
Consider a light, single-engine airplane, such as the Piper Super Cub. If the maximum gross weight of the airplane is 6700 N, the wing area is 35 m, and the maximum lift coefficient is 2.1 with flaps down, calculate the stalling speed at sea level. Assume po = 1.225 kg/m. The stalling speed at sea level is km/h.
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