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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Fighter bombers use following type of engine

Turbojet
Rocket
Turbo-propeller
Ramjet

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It requires cooling water for its operation
It is bulky
None of these
It is inefficient

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

16 kg/cm²
10 kg/cm²
25 kg/cm²
6 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Increases
Remain unaffected
May increase or decrease depending on compressor capacity
Decreases

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Compressors, Gas Turbines and Jet Engines
Which is false statement about multistage compression?

The moisture in air is condensed in the inter-cooler
It is best suited for compression ratios around 7:1
Volumetric efficiency is high
Power consumption per unit of air delivered is low

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Does not change
Remain same
Decrease
Increase

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