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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

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

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

More loss of air due to leakage past the cylinder
Air can be cooled perfectly in between
Better lubrication is possible advantages of multistage
Mechanical balance is better

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Thrust power and propulsive power
Propulsive power and fuel input
Thrust power and fuel energy
Engine output and propulsive power

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

No flow of air
Reducing mass flow rate with increase in pressure ratio
Increased inclination of chord with air steam
Fixed mass flow rate regardless of pressure ratio

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Compressors, Gas Turbines and Jet Engines
The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called

Isothermal efficiency
Mechanical efficiency
Volumetric efficiency
Compressor efficiency

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Lower power consumption per unit of air delivered
Higher volumetric efficiency
Decreased discharge temperature
All of these

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