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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Cylinder clearance in a compressor should be

About 50% of swept volume
As large as possible
As small as possible
About 100% of swept volume

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Can't be compared
Equal
Higher
Lower

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Ericsson cycle
Joule cycle
Carnot cycle
Rankine cycle

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Compressors, Gas Turbines and Jet Engines
In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the

None of these
Efficiency of the engine
Thrust and range of aircraft
Both (A) and (B)

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

More
Same
Less
Depends on other factors

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

None of these
Isothermal
Polytropic
Adiabatic

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