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

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

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

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