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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
For speed above 3000 km/hour, it is more advantageous to use

Rockets
Turbojet engine
Ramjet engine
Propellers

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

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

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Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

1.06 kg/cm²
1.03 kg/cm²
0.53 kg/cm²
1.00 kg/cm²

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

256 bar
16 bar
64 bar
1 bar

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a gas turbine as compared to a diesel plant is

Same
More
Less
Depends on other factors

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Centrifugal pump
Reciprocating pump
Turbine
Sliding vane compressor

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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