In a nozzle, once the critical conditions are achieved at the throat, than which of the following remains constant:
A.Density of fluid
B.Velocity of fluid
C.Flow rate
D.All of the above
A.Density of fluid
B.Velocity of fluid
C.Flow rate
D.All of the above
A.larger blades at gas entry and smaller blades at exit
B.smaller blades at gas entry and larger blades at exit
C.identical dlades at exit as well as entry
D.size of blades remains same only angles changes
A.isentropic conditions
B.adiabatic conditions
C.isothermal conditions
D.polytropic conditions
A.Sliding vane type blower
B.Screw compressor
C.Axial flow compressor
D.Centrifugal blower
A.of internal irreversibility of the process due to friction, turbulence, etc.
B.of variation of specific heats with temperature
C.of losses due to incomplete combustion
D.all of the above
A.subsonic speed
B.sonic speed
C.supersonic speed
D.subsonic to supersonic speed
A.leakage of steam through bearings
B.leakage of steam through packings
C.purposely withdrawn steam for process application
D.purposely withdrawn for feed water heating
A.Nozzle control governing
B.Throttle governing
C.Bypass governing
D.Combined throttle and nozzle governing
A.conservation of momentum
B.conservation of energy
C.conservation of mass
D.conservation of velocity head
A.236 m/s
B.336 m/s
C.436 m/s
D.536 m/s