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Steam Nozzles and Turbines problems


  • 1. During flow through a nozzle, no heat is supplied or rejected by the steam.

  • Options
  • A. Agree
  • B. Disagree
  • Discuss
  • 2. Which of the following statement is correct?

  • Options
  • A. The efficiency of steam turbines is greater than steam engines.
  • B. A flywheel is a must for steam turbine.
  • C. The turbine blades do not change the direction of steam issuing from the nozzle
  • D. The pressure of steam, in reaction turbines, is increased in fixed blades as well as in moving blades
  • Discuss
  • 3. Steam turbines may be classified according to

  • Options
  • A. direction of steam flow
  • B. number of stages
  • C. mode of steam action
  • D. all of these
  • Discuss
  • 4. In a nozzle, the effect of supersaturation is to increase the dryness fraction of steam.

  • Options
  • A. Yes
  • B. No
  • Discuss
  • 5. In a nozzle, the effect of supersaturation is to

  • Options
  • A. decrease dryness fraction of steam
  • B. decrease specific volume of steam
  • C. increase the entropy
  • D. increase the heat drop
  • Discuss
  • 6. For a Parson's reaction turbine, if ?1 and ?2 are fixed blade angles at inlet and exit respectively and ?1 and ?2 are the moving blade angles at entrance and exit respectively, then

  • Options
  • A. ?1 = ?2 and ?1 = ?2
  • B. ?1 = ?1 and ?2 = ?2
  • C. ?1 < ?1 and ?2 > ?2
  • D. ?1 = ?2 and ?1 = ?2
  • Discuss
  • 7. When the cross-section of a nozzle __________ continuously from entrance to exit, it is called a convergent nozzle.

  • Options
  • A. increases
  • B. decreases
  • Discuss
  • 8. The efficiency of an impulse turbine is maximum when (where Vb = Blade speed, V = Absolute velocity of steam entering the blade, and ? = Nozzle angle)

  • Options
  • A. Vb = 0.5 V cos ?
  • B. Vb = V cos ?
  • C. Vb = 0.5 V2 cos ?
  • D. Vb = V2 cos?
  • Discuss
  • 9. The expansion of steam in a nozzle follows

  • Options
  • A. Carnot cycle
  • B. Rankine cycle
  • C. Joule cycle
  • D. Stirling cycle
  • Discuss
  • 10. In a 50% reaction turbine stage, tangential component of absolute velocity at rotor inlet is 537 m/s and the blade velocity is 454 m/s. The power output in kW of steam will be

  • Options
  • A. 260 kW
  • B. 282 kW
  • C. 296 kW
  • D. 302 kW
  • Discuss

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