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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Air-fuel ratio in a jet engine will be of the order of

2.5006944444444
0.83402777777778
0.62569444444444
0.41736111111111

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Compressors, Gas Turbines and Jet Engines
The work ratio of a gas turbine plant is defined as the ratio of

Net work output and heat supplied
Actual heat drop and isentropic heat drop
Net work output and work done by turbine
Net work output and isentropic heat drop

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Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Collect more air
Provide robust structure
Convert kinetic energy of air into pressure energy
Beautify the shape

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

Has no effect on
Increases
None of these
Decreases

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Compressors, Gas Turbines and Jet Engines
In a reciprocating air compressor, the compression work per kg of air

Decreases as clearance volume increases
Increases as clearance volume decreases
Increases as clearance volume increases
Is independent of clearance volume

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To increase the efficiency
To save fuel
To reduce the exit temperature
To increase the output

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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