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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

None of these
Work ratio
Pressure ratio
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

More than
Equal to
Less than
None of these

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Euler
Isentropic efficiency
Compressor efficiency
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
Propulsion efficiency of the following order is obtained in practice

0.6
0.34
0.5
0.72

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Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

Gas turbine
4-stroke diesel engine
Multi cylinder engine
4-stroke petrol engine

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

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

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