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Maximum endurance and range versus airspeed. The maximum endurance condition would be obtained at the point of minimum power required since this would
Maximum endurance and range versus airspeed. The maximum endurance condition would be obtained at the point of minimum power required since this would require the lowest fuel flow to keep the airplane in a steady, level flight. Maximum range condition would occur where the ratio of speed to power required is greatest. The maximum range condition is obtained at maximum lift/drag ratio (L/Dmax)