Compressors, Gas Turbines and Jet Engines
The specific output per kg mass flow rate of a gas turbine (having fixed efficiencies of compressor and turbine and fixed higher and lower temperature) with increase in pressure ratio will

Increase first at slow rate and then fast
First increase, reach maximum and then decrease
Increase first at fast rate and then slow
Decrease continuously

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion

The propulsive matter is ejected from within the propelled body
None of these
The propulsive matter is caused to flow around the propelled body
Its functioning does not depend upon presence of air

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