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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isentropically
Isothermally
Adiabatically
Isochronically

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler work is known as

Pressure coefficient
Work coefficient
Polytropic reaction
Slip factor

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as adiabatic
In between isothermal and adiabatic
Same as isothermal
Better than isothermal and adiabatic

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Maximum cycle temperature
Pressure ratio
All of these
Minimum cycle temperature

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Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Pressure coefficient
Pressure ratio
Degree of reaction
Slip factor

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

Isothermal
None of these
Polytropic
Adiabatic

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