In the design of certain small turbo-prop aircraft, the
Chapter 2, Problem 51(choose chapter or problem)
In the design of certain small turbo-prop aircraft, the landing speed V (in ) is determined by the formula , where W is the gross weight (in pounds) of the aircraft and S is the surface area (in ) of the wings. If the gross weight of the aircraft is between 7500 pounds and 10,000 pounds and , determine the range of the landing speeds in miles per hour.
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