Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Work done by turbine and net work output
Net work output and work done by turbine
Work done by turbine and heat supplied
Net work output and heat supplied

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Compressors, Gas Turbines and Jet Engines
Pick up the false statement

Gas turbine is a self starting unit
Exhaust losses in gas turbine are high due to large mass flow rate
Overall efficiency of gas turbine plant is lower than that of a reciprocating engine
Gas turbine does not require huge quantity of water like steam plant

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in gas turbine results in

Increase in net output but decrease in thermal efficiency
Decrease in both thermal efficiency and net output
Increase in both thermal efficiency and net output
Increase in thermal efficiency but decrease in net output

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