Which of the following bladings will give maximum pressure rise in a centrifugal compressor, assuming the same overall dimensions, blade inlet angle and rotational speeds ?

Forward curved blades
Backward curved blades
Radial blades
all of these
✅ The correct answer is option A.

The overall isothermal efficiency of the compressor is defined as the ratio of

work required to compress the air isothermally to the actual work required to compress the air for the same pressure ratio
isothermal power to the shaft power or B.P. of the motor or engine required to drive the compressor
volume of free air delivery per stroke to the swept volume of the piston
isentropic power to th
✅ The correct answer is option B.

Which one of the following is the effect of blade shape on performance of a centrifugal compressor ?

Backward curved blades has poor efficiency
Backward curved blades lead to stable performance
Forward curved blades has higher efficiency
Forward curved blades
✅ The correct answer is option D.