larger air handling ability per unit frontal area
higher pressure ratio per stage
aerofoil blades are used
higher average velocities
same as isothermal
same as adiabatic
better than isothermal and adiabatic
in between isothermal and adiabatic
1.03 kg/cm2
1.06 kg/cm2
1.00 kg/cm2
0.53 kg/cm2
increases
decreases
remains constant
first decreases and then increases
large discharge at high pressure
low discharge at high pressure
large discharge at low pressure
low discharge at low pressure