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EndsemNov 20252019 patternBE Mech

Turbomachinery SPPU Endsem Question Paper Nov 2025

All 8 questions from this SPPU endsem paper, as printed. Read them here or open the PDF.

Subject code
402043
Pattern
2019 pattern
Exam
Endsem
Session
Nov 2025
Max. marks
50
Time
2 Hours
Semester
VII
Paper code
[6584]-219

Printed for: B.E. (Mechanical)

Instructions to the candidates

  1. Answer Q.1 or Q.2, Q.3 or Q.4, Q.5 or Q.6, Q.7 or Q.8.
  2. Neat diagrams must be drawn wherever necessary.
  3. Use of steam table/Mollier chart is allowed.
  4. Use of non programmable calculator is allowed.
  5. Figures to the right indicates full marks.

Questions

  1. Q1

    1. a)

      Show that the efficiency of a free jet striking normally on a series of flat plates mounted on the periphery of a wheel can never exceed 50%.

      [6]
    2. b)

      A double jet Pelton wheel has a specific speed of 14 and is required to deliver 1000 kW. The turbine is supplied through pipeline from a reservoir whose level is 400 m above the nozzles. Allowing 5% frictional loss in the pipe, Calculate: i) Speed of the turbine ii) Diameter of jets and iii) Mean diameter of bucket circle. Take C v = 0.98, speed ratio = 0.46, and overall efficiency of turbine = 85%. The specific speed is based on power output per jet.

      [8]
  2. Q2

    1. a)

      Explain the functions of following i) casing of Pelton wheel ii) Notch of bucket iii) Governing mechanism.

      Also asked:May 2025 ·May 2024

      [6]
    2. b)

      A Francis turbine with an overall efficiency of 80% is required to produce 130 kW. It is working under a head of 10 m. The peripheral velocity is 0.24 2gH and the radial velocity of flow at inlet is 0.9 2gH . The wheel runs at 150 rpm and the hydraulic losses in the turbine are 10% of 2 the available energy. Assuming radial discharge, determine- i) The guide blade angle ii) The wheel vane angle at inlet iii) Diameter of the wheel at inlet and iv) Width of the wheel at inlet

      [8]
  3. Q3

    1. a)

      Why governing of steam turbines is necessary? Explain with neat sketch throttle governing of Steam turbine.

      [6]
    2. b)

      In an impulse turbine (with a single row wheel) the mean diameter of the blades is 1.05 m and the speed is 3000 rpm. The nozzle angle is 18 º , the ratio of blade speed to steam speed is 0.42 and the ratio of the relative velocity at outlet from the blades to that at inlet is 0.84. The outlet angle of the blades is to be made 3 ° less than the inlet angle. The steam flow rate is 10 kg/sec. Draw the velocity diagrams for the blades and Calculate : i) Tangential thrust on the blades ii) Axial thrust on the blades and iii) Resultant thrust on the blades.

      [6]
  4. Q4

    1. a)

      Explain degree of reaction in steam turbines? Why 100% reaction steam turbine is not possible?

      [6]
    2. b)

      In a reaction steam turbine, the blade tips are inclined at 35 º and 20 º in the direction of motion. The guide blades are of the same shape as the moving blades, but reversed in direction. At a certain place in the turbine, the drum diameter is 1 m and the blades are 10 cm high. At this place, the steam has a pressure of 1.75 bar and dryness 0.935. If the speed of this turbine is 250 rpm and the steam passes through the blades without shock, find the mass of steam flow and power developed in the ring of moving blades. Velocity of flow is 10.8 m/sec and remains constant from inlet to outlet. Specific volume of dry saturated steam at a pressure of 1.75 bar is 1.004 m 3 /kg.

      [6]
  5. Q5

    1. a)

      What do you mean by cavitation? Explain the phenomenon of cavitation in centrifugal pump.

      Also asked:May 2025 ·May 2024

      [6]
    2. b)

      A centrifugal pump has effective areas of flow of 15 cm 2 and 17.5 cm 2 at outlet and inlet respectively. Water enters the impeller radially with 5 m/sec. The vanes are set back at 25 º to the tangent at outlet. The 3 peripheral velocities of vane tips at outlet and inlet are 30 m/sec and 15 m/sec respectively. The manometric efficiency is 80%. Neglecting impeller losses, Determine- i) Percentage of outlet velocity head recovered in the diffuser passage. ii) Inlet angle of diffuser vanes.

      [6]
  6. Q6

    1. a)

      Discuss various methods of priming of centrifugal pump.

      [6]
    2. b)

      This part has equations that don’t show as text. Open the PDF to read it.

      [6]
  7. Q7

    1. a)

      The following data is used for a centrifugal compressor. Diameter of inlet eye of the compressor impeller = 35 cm, Mass flow rate =10 kg/sec, Total pressure ratio = 3.6, Axial velocity at inlet = 140 m/sec, Velocity in delivery pipe = 120 m/sec, Tip speed of impeller = 460 m/sec, Speed of compressor = 18000 rpm, Total head isentropic efficiency = 85% Ambient condition = 1.013 bar and 15 º C. Find - i) Static pressure and temperature at inlet and outlet ii) Static pressure ratio iii) Work done per kg and iv) Theoretical power

      [6]
    2. b)

      What is prewhirl in a centrifugal compressor? Why is it necessary?

      [6]
  8. Q8

    1. a)

      Explain the phenomenon of surging and stalling in an axial flow compressor.

      [6]
    2. b)

      Explain various losses in axial flow compressor. 

      [6]