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Compressors, Gas Turbines and Jet Engines

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

1.3
1.4
1
1.2

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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Higher
Same
Lower
Dependent on other factors

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

5 to 8 bar
10 to 15 bar
8 to 10 bar
1 to 5 bar

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Less loss of air due to leakage past the cylinder
Less power requirement
Better mechanical balance
Lower volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

1.00 kg/cm²
0.53 kg/cm²
1.03 kg/cm²
1.06 kg/cm²

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Compressors, Gas Turbines and Jet Engines
Propulsion efficiency of the following order is obtained in practice

0.34
0.6
0.5
0.72

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