logo

CuriousTab

CuriousTab

Discussion


Home Mechanical Engineering Steam Nozzles and Turbines Comments

  • Question
  • In a Parson's turbine stage, blade velocity is 320 m/s at the mean radius and rotor blade exit angle is 30°. For minimum kinetic energy of the steam leaving the stage, the steam velocity at the exit of the rotor will be


  • Options
  • A. 160/3 m/s
  • B. 320/3 m/s
  • C. 640/3 m/s
  • D. 640 m/s

  • Correct Answer
  • 640/3 m/s 


  • Steam Nozzles and Turbines problems


    Search Results


    • 1. If the critical pressure ratio for steam is 0.546, then the steam is initially

    • Options
    • A. wet steam
    • B. dry saturated steam
    • C. superheated steam
    • D. none of these
    • Discuss
    • 2. In velocity compounding of an impulse turbine, the expansion of steam takes place in a nozzle or a set of nozzles from the boiler pressure to condenser pressure.

    • Options
    • A. True
    • B. False
    • Discuss
    • 3. The pressure velocity compounded impulse turbine allows a bigger pressure drop and hence __________ number of stages are required.

    • Options
    • A. more
    • B. less
    • Discuss
    • 4. De-Laval turbine is a

    • Options
    • A. simple impulse turbine
    • B. simple reaction turbine
    • C. impulse-reaction turbine
    • D. none of these
    • Discuss
    • 5. The effect of supersaturation is that the

    • Options
    • A. mass of the steam discharged increases
    • B. entropy and specific volume of the steam increases
    • C. exit velocity of steam reduces
    • D. all of these
    • Discuss
    • 6. In an impulse turbine, steam expands

    • Options
    • A. wholly in blades
    • B. wholly in nozzle
    • C. partly in the nozzle and partly in blades
    • D. none of these
    • Discuss
    • 7. A nozzle is said to be a convergent-divergent nozzle, when the cross-section of a nozzle first decreases from its entrance to throat and then increases from its throat to exit.

    • Options
    • A. True
    • B. False
    • Discuss
    • 8. In an ideal impulse turbine, the

    • Options
    • A. absolute velocity at the inlet of moving blade is equal to that at the outlet
    • B. relative velocity at the inlet of the moving blade is equal to that at the outlet
    • C. axial velocity at inlet is equal to that at the outlet
    • D. whirl velocity at inlet is equalto that at the outlet
    • Discuss
    • 9. The effect of bleeding is that

    • Options
    • A. it increases the thermodynamic efficiency of the turbine
    • B. boiler is supplied with hot water
    • C. it decreases the power developed by the turbine
    • D. all of the above
    • Discuss
    • 10. A single stage turbine is not used because it requires large reduction gearing due to very high rotational speed.

    • Options
    • A. Agree
    • B. Disagree
    • Discuss


    Comments

    There are no comments.

Enter a new Comment