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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Isothermal H.P/indicated H.R
Isothermal H.P./shaft H.R
Total output/air input
Compression work/motor input

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

between ~ to i of the blade height
at the base
in the center
at the tip

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

Ramjet
Rocket
Turbojet
Turbo-propeller

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

Increases
Has no effect on
Decreases
None of these

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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