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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Increase
Decrease
May increase or decrease depending on clearance volume
Remain same

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Compressors, Gas Turbines and Jet Engines
The ratio of work done per cycle to the swept volume in case of compressor is called

Compression ratio
Mean effective pressure
Compressor efficiency
Compression index

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Adiabatic compression
Isentropic compression
Polytropic compression
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
The efficiency of jet engine is

Lower at low speed
Higher at high speed
Higher at high altitudes
Same at all altitudes

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Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Impeller channel losses
All of the listed here
Inlet losses
Diffuser losses

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

Single stage compression
Multistage compression with intercooling
Multistage compression without intercooling
None of these

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