Compressors, Gas Turbines and Jet Engines
In the axial flow gas turbine, the work ratio is the ratio of

Compressor work and turbine work
Output and input
Actual compressor work and theoretical compressor work
Actual total head temperature drop to the isentropic total head drop from total head inlet to static head outlet

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Compressors, Gas Turbines and Jet Engines
Choose the correct statement

Gas turbines has flat efficiency at part loads
Gas turbines have high standby losses and require lot of maintenance
Gas turbine is capable of rapid start up and loading
Gas turbine requires lot of cooling water

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