Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Air can be cooled perfectly in between
Better lubrication is possible advantages of multistage
More loss of air due to leakage past the cylinder
Mechanical balance is better

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

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

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