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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Isentropic compression
Adiabatic compression
Isothermal compression
Ideal compression

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Compressors, Gas Turbines and Jet Engines
The work ratio of a gas turbine plant is defined as the ratio of

Actual heat drop and isentropic heat drop
Net work output and isentropic heat drop
Net work output and work done by turbine
Net work output and heat supplied

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Compressors, Gas Turbines and Jet Engines
For slow speed large capacity compressor, following type of valve will be best suited

Any of the above
Disc or feather type
Poppet valve
Mechanical valve of the Corliss, sleeve, rotary or semi rotary type

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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

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

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Compressors, Gas Turbines and Jet Engines
A closed gas turbine in which fuel is burnt directly in the air is not possible because of

High specific volume
Paucity of O2
Increasing gas temperature
High friction losses

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

None of these
Remain same
Increase
Decrease

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