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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Isothermal
None of these
Polytropic
Adiabatic

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

1000°C
1500°C
2000°C
700°C

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

After the inter-cooler
Between the after-cooler and receiver
Before first stage suction
Before the inter-cooler

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

More
Same
Less
Zero

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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

16 bar
256 bar
64 bar
1 bar

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Remains same
Increases/decreases depending on compressor capacity
Decreases
Increases

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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