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

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

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Compressors, Gas Turbines and Jet Engines
The compressor capacity is defined as the

Volume of air sucked by the compressor during its suction stroke
Volume of air delivered by the compressor
None of these
Actual volume of the air delivered by the compressor when reduced to normal temperature and pressure conditions

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