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In what proportion should the propulsive thrust be so that the aircraft will decelerate?(a) Thrust is less than airframe drag(b) Thrust is more than airframe drag(c) Greater airspeed(d) Less airspeedI had been asked this question in my homework.The query is from Descent Performance in Aircraft Operations in portion Climb and Descent Performance of Aircraft Performance |
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Answer» The CORRECT answer is (a) THRUST is less than airframe drag |
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