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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1.2
1.3
1.4
1

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

Same power
Less power
More/less power depending on other factors
More power

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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 ratio
Pressure coefficient
Slip factor
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Does not require oxygen
Carries its own oxygen
Uses surrounding air
Uses compressed atmospheric air

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

2.0840277777778
1.2506944444444
2.5006944444444
1.6673611111111

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