Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor with clearance volume

May increase/decrease depending on compressor capacity
Decreases with increase in compression ratio
In not dependent upon compression ratio
Increases with increase in compression ratio

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

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

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Compressors, Gas Turbines and Jet Engines
Which one of the following is the effect of blade shape on performance of a centrifugal compressor?

Forward curved blades has higher efficiency
Backward curved blades lead to stable performance
Forward curved blades produce lower pressure ratio
Backward curved blades has poor efficiency

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