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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in efficiency
Increase in flow and decrease in efficiency
Increase in flow
Decrease in flow

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Compressors, Gas Turbines and Jet Engines
Which of the following fuels can be used in turbojet engines?

Liquid hydrogen
High speed diesel oil
Methyl alcohol
Kerosene

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Remain same
Increase
May increase or decrease depending on clearance volume
Decrease

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

700°C
1000°C
500°C
200°C

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

Pumps
Axial compressor
All of these
Centrifugal compressor

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
20 bar
50 bar
30 bar

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