Suppose the airplane of Prob. 7.116 takes off at sea level without benefit of flaps and with

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Suppose the airplane of Prob. 7.116 takes off at sea level without benefit of flaps and with constant lift coefficient and take-off speed of 100 mi/h.
(a) Estimate the take-off distance if the thrust is 10 kN.
(b) How much thrust is needed to make the take-off distance 1250 m?
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