A. Larger air handling ability per unit frontal area
B. Higher pressure ratio per stage
C. Aerofoil blades are used
D. Higher average velocities
A. 1.03 kg/cm2
B. 1.06 kg/cm2
C. 1.00 kg/cm2
D. 0.53 kg/cm2
A. Centrifugal pump
B. Reciprocating pump
C. Turbine
D. Sliding vane compressor
A. Increase
B. Decrease
C. Remain same
D. May increase/decrease depending on clearance volume
A. Pressure ratio
B. Maximum cycle temperature
C. Minimum cycle temperature
D. All of the above
A. Brayton or atkinson cycle
B rAnkine cycle
C. Carnot cycle
D. Erricsson cycle
A. To supply base load requirements
B. To supply peak load requirements
C. To enable start thermal power plant
D. In emergency
A. Mass flow rate
B. Pressure ratio
C. Change in load
D. Stagnation pressure at the outlet
A. Pressure ratio
B. Pressure coefficient
C. Degree of reaction
D. Slip factor
A. Same as isothermal
B. Same as adiabatic
C. Better than isothermal and adiabatic
D. In between isothermal and adiabatic