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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a closed cycle gas turbine, the air is compressed

Polytropically
Isentropically
None of these
Isothermally

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

In the direction of motion of blades
Equal to zero
Depending on the velocity
Opposite to the direction of motion of blades

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase speed
Reduce turbine size
Increase power output
Increase temperature

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

May increase or decrease depending on clearance volume
Increase
Remain same
Decrease

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Can be driven at a very high speed
Produces uniform torque
Has more efficiency
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The ratio of the discharge pressure to the inlet pressure of air is called

Compression ratio
Volumetric efficiency
Compressor efficiency
Expansion ratio

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