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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

0.1%
0.5%
5%
1.0%

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

Pumps
Axial compressor
Centrifugal compressor
All of these

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Either (A) or (B)
Engine
None of these
Electric motor

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Compressors, Gas Turbines and Jet Engines
For an irreversible gas turbine cycle, the efficiency and work ratio both depend on

Minimum cycle temperature alone
Both pressure ratio and maximum cycle temperature
Pressure ratio alone
Maximum cycle temperature alone

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Lost work
Compression of inlet air
Reduction of speed of incoming air and conversion of part of it into pressure energy
Increasing speed of incoming air

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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