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

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

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

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

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