Compressors, Gas Turbines and Jet Engines
Intercooling in gas turbines

Increases net output and thermal efficiency both
Increases net output but decreases thermal efficiency
Decreases net output but increases thermal efficiency
Decreases net output and thermal efficiency both

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Compressors, Gas Turbines and Jet Engines
Which of the following statement is correct relating to rocket engines?

The stagnation conditions exist at the combustion chamber
The exit velocities of exhaust gases are much higher than those in jet engine
All of these
The combustion chamber in a rocket engine is directly analogous to the reservoir of a supersonic wind tunnel

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Compressors, Gas Turbines and Jet Engines
Pick up the false statement

Overall efficiency of gas turbine plant is lower than that of a reciprocating engine
Gas turbine is a self starting unit
Exhaust losses in gas turbine are high due to large mass flow rate
Gas turbine does not require huge quantity of water like steam plant

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