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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

10 kg/cm²
25 kg/cm²
6 kg/cm²
16 kg/cm²

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Ericsson cycle
Brayton or Atkinson cycle
Rankine cycle
Carnot cycle

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Increase of work ratio
Decrease of work ratio
Decrease of thermal efficiency
Both (A) and (B) above

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Compressors, Gas Turbines and Jet Engines
A closed gas turbine in which fuel is burnt directly in the air is not possible because of

High friction losses
High specific volume
Paucity of O2
Increasing gas temperature

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

These engines can work on several fuels
They can generate very high thrust
They are not air breathing engines
They have high propulsion efficiency

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Equal
Lower
Higher
Can't be compared

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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