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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

0.53 kg/cm²
1.06 kg/cm²
1.03 kg/cm²
1.00 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the

Adiabatic temperature drop in the stage
Total adiabatic temperature drop
Total temperature drop in the stage
Total temperature drop

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Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

None of the listed here
Critical pressure
Discharge pressure
Back pressure

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

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

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

More/less power depending on other factors
More power
Same power
Less power

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Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Anything
Highest
Atmospheric
Lowest

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