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

ANSWER DOWNLOAD EXAMIANS APP

Compressors, Gas Turbines and Jet Engines
The overall isothermal efficiency of compressor is defined as the ratio of

Power to drive compressor to isothermal h.p.
Work to compress air isothermally to work for actual compression
Isothermal h.p. to adiabatic h.p.
Isothermal h.p. to the BHP of motor

ANSWER DOWNLOAD EXAMIANS APP