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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1
1.3
1.4
1.2

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

Same
Less
More
Depends on other factors

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

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

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In one cylinder
In two cylinders on both sides of the piston
In two cylinders
In a single cylinder on both sides of the piston

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

In between isothermal and adiabatic
Same as isothermal
Better than isothermal and adiabatic
Same as adiabatic

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Compressors, Gas Turbines and Jet Engines
Gas turbines for power generation are normally used

To enable start thermal power plant
To supply peak load requirements
In emergency
To supply base load requirements

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