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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating air compressor, without clearance, the compression of air may be

Isothermal
Polytropic
Any one of these
Isentropic

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

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

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Compressors, Gas Turbines and Jet Engines
The fuel consumption in gas turbines is accounted for by

Higher calorific value
Heating value
Higher heating value
Lower heating value

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

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

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

None of these
Centrifugal type
Axial flow type
Radial flow type

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Control temperature
Control fire hazards
Increase efficiency
Control output of turbine

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