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In transonic region the thrust is inversely proportional to drag.

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in Aircraft Performance by (558k points)
In transonic region the thrust is inversely proportional to drag.

(a) True

(b) False

I had been asked this question in class test.

The above asked question is from High Performance Climb topic in chapter Climb and Descent Performance of Aircraft Performance

1 Answer

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Best answer
Correct answer is (a) True

Best explanation: In transonic region the thrust is inversely proportional to drag. Acceleration across the transonic region can be assisted by reducing rate of climb of the aircraft but the priority is given to increase in kinetic energy of the aircraft.

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