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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of jet engine is

Lower at low speed
Same at all altitudes
Higher at high speed
Higher at high altitudes

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Radial flow compressors
All of these
Pumps
Axial flow compressors

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Compressors, Gas Turbines and Jet Engines
The indicated work per unit mass of air delivered is

Inversely proportional to clearance volume
Directly proportional to clearance volume
Greatly affected by clearance volume
Not affected by clearance volume

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature

0.05
0.005
0.001
0.01

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Adiabatic compression
Isothermal compression
Polytropic compression
Isentropic compression

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

1 bar
256 bar
16 bar
64 bar

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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