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Compressors, Gas Turbines and Jet Engines

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

Decreases the thermal efficiency
Increases the compressor work
Increases the turbine work
Increases the thermal efficiency

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Isothermal
Adiabatic
None of these
Polytropic

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Compressors, Gas Turbines and Jet Engines
The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is

Clearance volume and leakages
Pressure drop across the valves
All of these
Superheating in compressor

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Compressors, Gas Turbines and Jet Engines
For an irreversible gas turbine cycle, the efficiency and work ratio both depend on

Both pressure ratio and maximum cycle temperature
Pressure ratio alone
Minimum cycle temperature alone
Maximum cycle temperature alone

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Compressors, Gas Turbines and Jet Engines
In jet engines, paraffin is usually used as the fuel because of its

High calorific value
Both (A) and (C) above
Low freezing point
Ease of atomisation

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Brayton or Atkinson cycle
Ericsson cycle
Rankine cycle
Carnot cycle

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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