Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To cool the air during compression
To enable compression in two stages
To cool the air at delivery
To minimize the work of compression

ANSWER DOWNLOAD EXAMIANS APP

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

ANSWER DOWNLOAD EXAMIANS APP