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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

Adiabatically
Isothermally
Isentropically
Isochronically

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Compressors, Gas Turbines and Jet Engines
Free air is the air at

Atmospheric conditions at any specific location
15°C and 1 kg/cm²
0°C and standard atmospheric conditions
20°C and 1 kg/cm² and relative humidity of 36%

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Compressors, Gas Turbines and Jet Engines
In a jet engine, the air-fuel ratio is

2.5006944444444
1.2506944444444
1.6673611111111
2.0840277777778

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Compressors, Gas Turbines and Jet Engines
The thrust of a jet propulsion power unit can be increased by

All of these
Injecting water into the compressor
Burning fuel after gas turbine
Injecting ammonia into the combustion chamber

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

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

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

None of these
Equal to
More than
Less than

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