Aircraft’s landing speed In the design of certain small turboprop aircraft, the landing speed V (in ft/sec) is determined by the formula W = 0.00334V2S, where W is the gross weight (in pounds) of the aircraft and S is the surface area (in ft2) of the wings. If the gross weight of the aircraft is between 7500 pounds and 10,000 pounds and S = 210 ft2, determine the range of the landing speeds in miles per hour.
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