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Situation 2

Aircraft landing speed. In the design of certain small turbo propaircraft, the landing speed V (inft/sec) is determined by the formula W = weight (in pounds)ofthe aircraft and S is the surface are (in ft) of the wings. If the gross 0.0033V'S, where Wis the gross weight of the aircraft is between 7500 pounds and 10,000pounds and S = 210ft². determinethe range of the landing speeds inmiles per hour.
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