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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Mechanical efficiency of gas turbines as compared to I.C engines is

Same
Lower
Higher
None of these

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

Single stage compression
None of these
Multistage compression with intercooling
Multistage compression without intercooling

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

Turbojet
Ramjet
Turbo-propeller
Rocket

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Compressors, Gas Turbines and Jet Engines
The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is

Superheating in compressor
Clearance volume and leakages
Pressure drop across the valves
All of these

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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 increases
Increases as clearance volume decreases
Is independent of clearance volume

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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