2022 102501

End Semester Examination - 2022

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer of the following (Any seven questions only):

Q1.1

Where is a water hammer developed?

a)

Reservoir

b)

Penstock

c)

Turbine blades

d)

Pipeline

Q1.2

The force of impingement of a jet on a vane increases, if

a)

the vane angle is increased

b)

the vane angle is decreased

c)

the pressure is reduced

d)

the vane is moved against the jet

Q1.3

The fluid coming into the centrifugal pump is accelerated by

a)

throttle

b)

impeller

c)

nozzle

d)

governor

Q1.4

The overall efficiency of a reaction turbine is the ratio of

a)

actual work available at the turbine to the energy imparted to the wheel

b)

work done on the wheel to the energy (or head of water) actually supplied to the turbine.

c)

power produced by the turbine to the energy actually supplied by the turbine

d)

None of the above.

Q1.5

A jet of water issues from a nozzle with a velocity of $ 20~m/s $ and it impinges normally on a flat plate moving away from it at $ 10~m/s $. If the cross-sectional area of the jet is $ 0.02~m^2 $ and the density of water is taken as $ 1000~kg/m^3 $, then the force developed on the plate will be

a)

10 N

b)

100 N

c)

1000 N

d)

2000 N

Q1.6

Which of the following turbine has least efficiency

a)

Pelton turbine

b)

Kaplan turbine

c)

Francis turbine

d)

Propeller turbine

Q1.7

The unit speed $ N_u $ of a turbine having a rotational speed of $ N $ and head $ H $ is equal to

a)

NHNH

b)

N/H0.5N/H^{0.5}

c)

HNHN

d)

(H/N)0.5(H/N)^{0.5}

Q1.8

What does Euler's equation of turbo machines relate to?

a)

Discharge and head

b)

Discharge and velocities

c)

Head and power

d)

Head and velocities

Q1.9

Without residual whirl in the flow at the entrance to a draft tube, the best cone angle is

a)

1010^{\circ}

b)

1212^{\circ}

c)

88^{\circ}

d)

2424^{\circ}

Q1.10

A centrifugal pump is started with its delivery valve kept

a)

fully open

b)

fully shut

c)

partially open

d)

50% open

Q.2 Solve both questions :

Q2.1

Show that the force exerted by a jet of water on moving inclined plane in the direction of jet is given by $ F_x = \rho a (V - u)^2 \sin^2 \theta $
Where, $ a = $ area of jet, $ \theta = $ inclination of the plate with the jet and $ V = $ velocity of jet

Q2.2

Show the general layout of a hydro-electric power plant and explain each component in brief.

Q.3 Solve both questions :

Q3.1

What is a hydraulic turbine? How are they classified? With the help of neat sketch, explain the construction and working of a Pelton wheel turbine.

Q3.2

An inward flow reaction turbine has external and internal diameters as 1 m and 0.5 m respectively. The turbine is running at 200 r.p.m. and width of turbine at inlet is 200 mm. The velocity of flow through the runner is constant and is equal to $ 1.8~m/s $. The guide blades make an angle of $ 10^{\circ} $ to the tangent of the wheel and the discharge at the outlet of the turbine is radial. Calculate all velocity vectors and draw the inlet and outlet velocity triangles. Also calculate mass flow through the runner/second, power developed and hydraulic efficiency.

Q.4 Solve both questions :

Q4.1

Draw a schematic of a Francis turbine and explain briefly its construction and working.

Q4.2

A turbine is to operate under a head of 28 m at 200 r.p.m. The discharge and overall efficiency of the turbine are $ 8.5~m^3/s $ and 89%, respectively. Determine (i) specific speed of the turbine, (ii) power generated and (iii) types of turbine.

Q.5 Solve both questions :

Q5.1

Explain different component parts of a centrifugal pump.

Q5.2

A centrifugal pump delivers water at the rate of 40 litres / sec for a total head of 30 m. Find the output of the pump. If the overall efficiency of the set consisting of the pump and the electric motor is 75%, find the power required to drive the motor.

Q.6 Solve both questions :

Q6.1

What is model analysis? What are the advantages and applications of model testing?

Q6.2

A 1:8 model of 12 ft diameter turbine is operated at 600 r.p.m. under a net head of 54.0 ft. Under this mode of operation, the bhp and Q of the model were observed, to be 332 hp and 62 cfs, respectively. From the above data compute (i) the specific speed of the model and the value of $ \sigma $ (ii) the efficiency and shaft torque of the model, (iii) the efficiency of the prototype, (iv) the flow rate and horsepower of the prototype if it is operated at 450 r.p.m. under a net head of 200 ft.

Q.7 Solve both questions :

Q7.1

What are the causes of cavitation? How will you prevent the cavitation in hydraulic Machines?

Q7.2

Define Indicator diagram. How will you prove that area of indicator diagram is proportional to the work done by the reciprocating pump?

Q.8 Write short notes on the following:

Q8.1

Governing of water turbine

Q8.2

Draft Tube.

Q.9 Write short notes on any two of the following:

Q9.1

Turbine

Q9.2

Specific speed of pump

Q9.3

Priming of pump

Q9.4

Slip in reciprocating pump


2022 V4 102501

End Semester Examination - 2022

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer of the following (Any seven questions only):

Q1.1

Where is a water hammer developed?

a)

Reservoir

b)

Penstock

c)

Turbine blades

d)

Pipeline

Q1.2

The force of impingement of a jet on a vane increases, if

a)

the vane angle is increased

b)

the vane angle is decreased

c)

the pressure is reduced

d)

the vane is moved against the jet

Q1.3

The fluid coming into the centrifugal pump is accelerated by

a)

throttle

b)

impeller

c)

nozzle

d)

governor

Q1.4

The overall efficiency of a reaction turbine is the ratio of

a)

actual work available at the turbine to the energy imparted to the wheel

b)

work done on the wheel to the energy (or head of water) actually supplied to the turbine.

c)

power produced by the turbine to the energy actually supplied by the turbine

d)

None of the above.

Q1.5

A jet of water issues from a nozzle with a velocity of $ 20~m/s $ and it impinges normally on a flat plate moving away from it at $ 10~m/s $. If the cross-sectional area of the jet is $ 0.02~m^2 $ and the density of water is taken as $ 1000~kg/m^3 $, then the force developed on the plate will be

a)

10 N

b)

100 N

c)

1000 N

d)

2000 N

Q1.6

Which of the following turbine has least efficiency

a)

Pelton turbine

b)

Kaplan turbine

c)

Francis turbine

d)

Propeller turbine

Q1.7

The unit speed $ N_u $ of a turbine having a rotational speed of $ N $ and head $ H $ is equal to

a)

NHNH

b)

N/H0.5N/H^{0.5}

c)

HNHN

d)

(H/N)0.5(H/N)^{0.5}

Q1.8

What does Euler's equation of turbo machines relate to?

a)

Discharge and head

b)

Discharge and velocities

c)

Head and power

d)

Head and velocities

Q1.9

Without residual whirl in the flow at the entrance to a draft tube, the best cone angle is

a)

1010^{\circ}

b)

1212^{\circ}

c)

88^{\circ}

d)

2424^{\circ}

Q1.10

A centrifugal pump is started with its delivery valve kept

a)

fully open

b)

fully shut

c)

partially open

d)

50% open

Q.2 Solve both questions :

Q2.1

Show that the force exerted by a jet of water on moving inclined plane in the direction of jet is given by $ F_x = \rho a (V - u)^2 \sin^2 \theta $
Where, $ a = $ area of jet, $ \theta = $ inclination of the plate with the jet and $ V = $ velocity of jet

Q2.2

Show the general layout of a hydro-electric power plant and explain each component in brief.

Q.3 Solve both questions :

Q3.1

What is a hydraulic turbine? How are they classified? With the help of neat sketch, explain the construction and working of a Pelton wheel turbine.

Q3.2

An inward flow reaction turbine has external and internal diameters as 1 m and 0.5 m respectively. The turbine is running at 200 r.p.m. and width of turbine at inlet is 200 mm. The velocity of flow through the runner is constant and is equal to $ 1.8~m/s $. The guide blades make an angle of $ 10^{\circ} $ to the tangent of the wheel and the discharge at the outlet of the turbine is radial. Calculate all velocity vectors and draw the inlet and outlet velocity triangles. Also calculate mass flow through the runner/second, power developed and hydraulic efficiency.

Q.4 Solve both questions :

Q4.1

Draw a schematic of a Francis turbine and explain briefly its construction and working.

Q4.2

A turbine is to operate under a head of 28 m at 200 r.p.m. The discharge and overall efficiency of the turbine are $ 8.5~m^3/s $ and 89%, respectively. Determine (i) specific speed of the turbine, (ii) power generated and (iii) types of turbine.

Q.5 Solve both questions :

Q5.1

Explain different component parts of a centrifugal pump.

Q5.2

A centrifugal pump delivers water at the rate of 40 litres / sec for a total head of 30 m. Find the output of the pump. If the overall efficiency of the set consisting of the pump and the electric motor is 75%, find the power required to drive the motor.

Q.6 Solve both questions :

Q6.1

What is model analysis? What are the advantages and applications of model testing?

Q6.2

A 1:8 model of 12 ft diameter turbine is operated at 600 r.p.m. under a net head of 54.0 ft. Under this mode of operation, the bhp and Q of the model were observed, to be 332 hp and 62 cfs, respectively. From the above data compute (i) the specific speed of the model and the value of $ \sigma $ (ii) the efficiency and shaft torque of the model, (iii) the efficiency of the prototype, (iv) the flow rate and horsepower of the prototype if it is operated at 450 r.p.m. under a net head of 200 ft.

Q.7 Solve both questions :

Q7.1

What are the causes of cavitation? How will you prevent the cavitation in hydraulic Machines?

Q7.2

Define Indicator diagram. How will you prove that area of indicator diagram is proportional to the work done by the reciprocating pump?

Q.8 Write short notes on the following:

Q8.1

Governing of water turbine

Q8.2

Draft Tube.

Q.9 Write short notes on any two of the following:

Q9.1

Turbine

Q9.2

Specific speed of pump

Q9.3

Priming of pump

Q9.4

Slip in reciprocating pump


2021 102501

B.Tech Examination, 2021

Time 3 hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Questions

Q1

Choose the correct answer (any seven) :

a)

Buckets and blades used in a turbine are used to

a)

(i) alter the direction of water

b)

(ii) switch off the turbine

c)

(iii) regulate the wind speed

d)

(iv) regenerate the power

b)

_______ is the electric power obtained from the energy of the water.

a)

(i) Roto dynamic power

b)

(ii) Thermal power

c)

(iii) Nuclear power

d)

(iv) Hydroelectric power

c)

In reaction turbine hydraulic efficiency is

a)

(i) ratio of actual work at the turbine to the energy imparted to the wheel

b)

(ii) ratio of work done on the wheel to energy that is supplied to the turbine

c)

(iii) ratio of power produced by the turbine to the energy actually supplied by the turbine

d)

(iv) ratio of work done on the wheel to the energy (or head of water) actually supplied to the turbine

d)

In what type of turbine water enters in radial direction and leaves axial direction?

a)

(i) Tangential flow turbine

b)

(ii) Axial flow turbine

c)

(iii) Outward flow turbine

d)

(iv) Mixed flow turbine

e)

Head under which Kaplan turbine is operated is

a)

(i) 1070 meters10-70\text{ meters}

b)

(ii) 70100 meters70-100\text{ meters}

c)

(iii) 100200 meters100-200\text{ meters}

d)

(iv) Above 200 meters200\text{ meters}

f)

The difference between gross head and friction losses is

a)

(i) net head

b)

(ii) gross head

c)

(iii) manometric head

d)

(iv) net positive suction head

g)

Pipes of largest diameter which carry water from reservoir to the turbines is known as

a)

(i) head stock

b)

(ii) tail race

c)

(iii) tail stock

d)

(iv) pen stock

h)

Different velocities in a centrifugal pump are determined by using

a)

(i) Froude number

b)

(ii) Reynolds number

c)

(iii) velocity triangle

d)

(iv) overall efficiency

i)

A multistage centrifugal pump has more than two

a)

(i) pumps

b)

(ii) impellers

c)

(iii) turbines

d)

(iv) magnetic pumps

j)

If we raise the liquid level in the suction vessel, cavitation

a)

(i) increases

b)

(ii) decreases

c)

(iii) same

d)

(iv) independent

[14 Marks]
Q2

Answer the following:

a)

A jet of water from a nozzle is deflected through 6060^\circ from its original direction by curved plate which it enters tangentially without shock with a velocity of 30 m/s30\text{ m/s} and leaves with a mean velocity of 25 m/s25\text{ m/s}. If the discharge from the nozzle is 0.8 kg/s0.8\text{ kg/s}, calculate the magnitude and direction of the resultant force on the vane, if the vane is stationary.

[8 Marks]
b)

A jet strikes tangentially a smooth curved vane moving in the same direction as the jet, and the jet gets reversed in the direction. Show that the maximum efficiency is slightly less than 6060 percent.

[6 Marks]
Q3

Answer the following:

a)

Define the degree of reaction. Find out the value of degree of reaction ($R$) for Pelton turbine and Reaction turbine.

[6 Marks]
b)

A single jet Pelton wheel runs at 300 r.p.m.300\text{ r.p.m.} under a head of 510 m510\text{ m}. The jet diameter is 200 mm200\text{ mm}, its deflection inside the bucket is 165165^\circ and its relative velocity is reduced by 15%15\% due to friction. Determine— (i) water power; (ii) resultant force on the bucket; (iii) overall efficiency. Take : Mechanical losses = 3%3\%, coefficient of velocity = 0.980.98, and speed ratio = 0.460.46.

[8 Marks]
Q4

Answer the following:

a)

What do you mean by hydraulic turbine? Give the comparison between impulse and reaction turbines.

[5 Marks]
b)

An inward flow reaction turbine has external and internal diameters as 1.08 m1.08\text{ m} and 0.54 m0.54\text{ m}. The turbine is running at 200 r.p.m.200\text{ r.p.m.} The width of the turbine at inlet is 240 mm240\text{ mm} and velocity of flow through the runner is constant and is equal to 2.16 m/s2.16\text{ m/s}. The guide blades make an angle of 1010^\circ to the tangent of the wheel and discharge at the outlet of the turbine is radial. Draw the inlet and outlet velocity triangles and determine— (i) the absolute velocity of water at inlet of the runner; (ii) the velocity of whirl at inlet; (iii) the relative velocity at inlet; (iv) the runner blade angles; (v) width of runner at outlet; (vi) weight of water flowing through the runner per second; (vii) head at inlet of the turbine; (viii) power developed; (ix) hydraulic efficiency of the turbine.

[9 Marks]
Q5

Answer the following:

a)

What is a draft tube? Can we use draft tube in an impulse turbine? Describe different types of draft tubes with neat sketches.

[6 Marks]
b)

State the advantages and disadvantages of a Francis turbine over a Pelton wheel.

[3 Marks]
c)

Explain with neat sketch the working of a Kaplan turbine. What is the difference between a propeller turbine and a Kaplan turbine?

[5 Marks]
Q6

Answer the following:

a)

What is cavitation? Enumerate some methods to avoid cavitation in water turbines.

[6 Marks]
b)

A Francis turbine is to operate under a head of 24 m24\text{ m}. If it generates 2000 kW2000\text{ kW} power and the overall efficiency turbine is 90 percent90\text{ percent}, determine speed ($N$) and discharge of the turbine.

[8 Marks]
Q7

Answer the following:

a)

Explain briefly, with neat sketches, the following types of casings in centrifugal pumps: (i) Volute casing (ii) Vortex casing

[5 Marks]
b)

The impeller of a centrifugal pump having external and internal diameters 450 mm450\text{ mm} and 200 mm200\text{ mm} respectively, width at outlet 50 mm50\text{ mm} and running at 1200 r.p.m.1200\text{ r.p.m.} works against a head of 45 m45\text{ m}. The velocity of flow through the impeller is constant and equal to 3.0 m/s3.0\text{ m/s}. The vanes are set back at an angle of 4040^\circ at outlet. Determine (i) inlet vane angle, (ii) work done by the impeller on water per second and (iii) manometric efficiency.

[9 Marks]
Q8

Answer the following:

a)

It is required to pump water out of deep well under a total head of 90 m90\text{ m}. A number of identical pumps of design speed 1000 r.p.m.1000\text{ r.p.m.} and specific speed 3030 with a rated capacity of 0.15 m3/s0.15\text{ m}^3\text{/s} are available. How many pumps are required and how should they be connected whether in series or in parallel?

[7 Marks]
b)

Two geometrically similar pumps are running at the same speed of 1000 r.p.m.1000\text{ r.p.m.} One pump has an impeller diameter of 3 mm3\text{ mm} and lifts water at the rate of 0.02 m3/s0.02\text{ m}^3\text{/s} against a head of 15 m15\text{ m}. Determine the head and impeller diameter of the other pump to deliver half the discharge.

[7 Marks]
Q9

Answer the following:

a)

What is priming? Why is it necessary?

[3 Marks]
b)

Describe the principle and working of a reciprocating pump. How are they classified?

[6 Marks]
c)

Define slip, percentage slip and negative slip of a reciprocating pump.

[5 Marks]

2020 021510

B.Tech 5th Semester Special Exam., 2020

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer (any seven):

Q1.1

Reciprocating pump is a/an

a)

negative displacement pump

b)

positive displacement pump

c)

diaphragm pump

d)

emulsion pump

Q1.2

How many numbers of valves are required for the rotary pump?

a)

0

b)

1

c)

2

d)

3

Q1.3

When the casing in a centrifugal pump decelerates the flow, what increases?

a)

Flow rate

b)

Temperature

c)

Volume

d)

Pressure

Q1.4

The fundamental significance of all the turbo-machinery is

a)

conservation of momentum

b)

conservation of mass

c)

conservation of heat

d)

conservation of speed

Q1.5

Kaplan turbine is a/an

a)

tangential-flow turbine

b)

radial-flow turbine

c)

axial-flow turbine

d)

mixed-flow turbine

Q1.6

The function of the draft tube is

a)

to increase the pressure of the exiting fluid

b)

to increase the kinetic energy of exiting fluid

c)

to allow the turbine to be set below tail water level

d)

to keep pressure at runner outlet above the atmospheric pressure

Q1.7

In which turbine, the pressure energy of water is first converted into kinetic energy by means of nozzle kept close to the runner?

a)

Impulse turbine

b)

Reaction turbine

c)

Both (i) and (ii)

d)

None of the above

Q1.8

If the blades of the axial flow turbine are fixed, these are called

a)

Kaplan turbine

b)

Propeller turbine

c)

Francis turbine

d)

Pelton turbine

Q1.9

Which compressors are suitable for large volume flow rates of above $ 1200~m^3/min $?

a)

Centrifugal compressors

b)

Axial flow compressors

c)

Reciprocating compressors

d)

Both (i) and (ii)

Q1.10

Which among the following is the formula for force when it strikes the plate?

a)

ρaV2\rho a V^2

b)

ρaV\rho a V

c)

ρa\rho a

d)

maEm a E

Q.2 Solve both questions :

Q2.1

Show that the force exerted by a jet of water on an inclined fixed plane in the direction of jet is given by $ F_x = \rho a V^2 \sin^2 \theta $
where, $ a = $ area of the jet, $ \theta = $ inclination of the plate with the jet and $ V = $ velocity of the jet.

Q2.2

A jet of water of diameter 50 mm moving with a velocity of $ 25~m/s $ impinges on a fixed curved plate tangentially at one end at an angle of $ 30^{\circ} $ to the horizontal. Calculate the resultant force of the jet on the plate if the jet is deflected through an angle of $ 50^{\circ} $. Take $ g = 10~m/s^2 $.

Q.3 Solve both questions :

Q3.1

Find an expression for the propelling force and the work done per second on a tank which is provided with an orifice through which jet of water is coming out and tank is free to move.

Q3.2

Define the degree of reaction. Find out the value of degree of reaction (R) for Pelton turbine and actual reaction turbine.

Q.4 Solve both questions :

Q4.1

How will you classify the turbines?

Q4.2

A reaction turbine works at 450 r.p.m. under a head of 120 meters. Its diameter at inlet is 120 cm and the flow area is $ 0.4~m^2 $. The angles made by absolute and relative velocities at inlet are $ 20^{\circ} $ and $ 60^{\circ} $ respectively with the tangential velocity. Determine (i) volume flow rate, (ii) power developed and (iii) hydraulic efficiency.

Q.5 Solve both questions :

Q5.1

What is a draft tube? Why is it used in a reaction turbine? Describe different types of draft tubes with neat sketches.

Q5.2

A turbine is to operate under a head of 25 m at 200 r.p.m. The discharge and overall efficiencies of the turbine are $ 9~m^3/s $ and 90% simultaneously. Determine (i) specific speed of the turbine, (ii) power generated and (iii) type of turbine.

Q.6 Solve both questions :

Q6.1

Differentiate between (i) Kaplan and Propeller turbines and (ii) Centrifugal and Reciprocating pumps.

Q6.2

The cylinder bore diameter of a single-acting reciprocating pump is 150 mm and its stroke is 300 mm. The pump runs at 50 r.p.m. and lifts water through a height of 25 m. The delivery pipe is 22 m long and 100 mm in diameter. Find the theoretical discharge and the theoretical power required to run the pump. If the actual discharge is 4.2 litres/s, find the percentage slip. Also, determine the acceleration head at the beginning and middle of the delivery stroke.

Q.7 Solve all three questions :

Q7.1

What is priming? Why is it necessary?

Q7.2

Draw and discuss the operating characteristic curves of a centrifugal pump.

Q7.3

A centrifugal pump is to discharge $ 0.118~m^3/s $ at a speed of 1450 r.p.m. against a head of 25 m. The impeller diameter is 250 mm, its width at outlet is 50 mm and manometric efficiency is 75%. Determine the vane angle at the outer periphery of the impeller.

Q.8 Solve both questions :

Q8.1

Find the number of pumps required to take water from a deep well under a total head of 89 m. All the pumps are identical and are running at 800 r.p.m. The specific speed of each pump is given as 25 while the rated capacity of each pump is $ 0.16~m^3/s $.

Q8.2

Describe with a neat sketch the construction and working of single-stage single-acting reciprocating air compressor. Also explain its actual P-V diagram.

Q.9 Solve both questions :

Q9.1

What do you mean by multistage compression? State its advantages.

Q9.2

Determine the impeller diameters and the width at the impeller exit and the power required to drive the compressor from the following data:
Speed (N) = 12500 rev/min
Mass flow rate (m) = 15 kg/s
Pressure ratio = 4:1
Isentropic efficiency = 75%
Slip factor = 0.9
Flow coefficient at impeller exit = 0.3
Hub diameter of the eye = 15 cm
Axial velocity of air at entry to and exit from the impeller = 150 m/s
Stagnation temperature at inlet = 295 K
Stagnation pressure at inlet = 1.0 bar
Assume equal pressure ratio in the impeller and diffuser.


2020 SPECIAL 021510

B.Tech 5th Semester Special Exam., 2020

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer (any seven):

Q1.1

Reciprocating pump is a/an

a)

negative displacement pump

b)

positive displacement pump

c)

diaphragm pump

d)

emulsion pump

Q1.2

How many numbers of valves are required for the rotary pump?

a)

0

b)

1

c)

2

d)

3

Q1.3

When the casing in a centrifugal pump decelerates the flow, what increases?

a)

Flow rate

b)

Temperature

c)

Volume

d)

Pressure

Q1.4

The fundamental significance of all the turbo-machinery is

a)

conservation of momentum

b)

conservation of mass

c)

conservation of heat

d)

conservation of speed

Q1.5

Kaplan turbine is a/an

a)

tangential-flow turbine

b)

radial-flow turbine

c)

axial-flow turbine

d)

mixed-flow turbine

Q1.6

The function of the draft tube is

a)

to increase the pressure of the exiting fluid

b)

to increase the kinetic energy of exiting fluid

c)

to allow the turbine to be set below tail water level

d)

to keep pressure at runner outlet above the atmospheric pressure

Q1.7

In which turbine, the pressure energy of water is first converted into kinetic energy by means of nozzle kept close to the runner?

a)

Impulse turbine

b)

Reaction turbine

c)

Both (i) and (ii)

d)

None of the above

Q1.8

If the blades of the axial flow turbine are fixed, these are called

a)

Kaplan turbine

b)

Propeller turbine

c)

Francis turbine

d)

Pelton turbine

Q1.9

Which compressors are suitable for large volume flow rates of above $ 1200~m^3/min $?

a)

Centrifugal compressors

b)

Axial flow compressors

c)

Reciprocating compressors

d)

Both (i) and (ii)

Q1.10

Which among the following is the formula for force when it strikes the plate?

a)

ρaV2\rho a V^2

b)

ρaV\rho a V

c)

ρa\rho a

d)

maEm a E

Q.2 Solve both questions :

Q2.1

Show that the force exerted by a jet of water on an inclined fixed plane in the direction of jet is given by $ F_x = \rho a V^2 \sin^2 \theta $
where, $ a = $ area of the jet, $ \theta = $ inclination of the plate with the jet and $ V = $ velocity of the jet.

Q2.2

A jet of water of diameter 50 mm moving with a velocity of $ 25~m/s $ impinges on a fixed curved plate tangentially at one end at an angle of $ 30^{\circ} $ to the horizontal. Calculate the resultant force of the jet on the plate if the jet is deflected through an angle of $ 50^{\circ} $. Take $ g = 10~m/s^2 $.

Q.3 Solve both questions :

Q3.1

Find an expression for the propelling force and the work done per second on a tank which is provided with an orifice through which jet of water is coming out and tank is free to move.

Q3.2

Define the degree of reaction. Find out the value of degree of reaction (R) for Pelton turbine and actual reaction turbine.

Q.4 Solve both questions :

Q4.1

How will you classify the turbines?

Q4.2

A reaction turbine works at 450 r.p.m. under a head of 120 meters. Its diameter at inlet is 120 cm and the flow area is $ 0.4~m^2 $. The angles made by absolute and relative velocities at inlet are $ 20^{\circ} $ and $ 60^{\circ} $ respectively with the tangential velocity. Determine (i) volume flow rate, (ii) power developed and (iii) hydraulic efficiency.

Q.5 Solve both questions :

Q5.1

What is a draft tube? Why is it used in a reaction turbine? Describe different types of draft tubes with neat sketches.

Q5.2

A turbine is to operate under a head of 25 m at 200 r.p.m. The discharge and overall efficiencies of the turbine are $ 9~m^3/s $ and 90% simultaneously. Determine (i) specific speed of the turbine, (ii) power generated and (iii) type of turbine.

Q.6 Solve both questions :

Q6.1

Differentiate between (i) Kaplan and Propeller turbines and (ii) Centrifugal and Reciprocating pumps.

Q6.2

The cylinder bore diameter of a single-acting reciprocating pump is 150 mm and its stroke is 300 mm. The pump runs at 50 r.p.m. and lifts water through a height of 25 m. The delivery pipe is 22 m long and 100 mm in diameter. Find the theoretical discharge and the theoretical power required to run the pump. If the actual discharge is 4.2 litres/s, find the percentage slip. Also, determine the acceleration head at the beginning and middle of the delivery stroke.

Q.7 Solve all three questions :

Q7.1

What is priming? Why is it necessary?

Q7.2

Draw and discuss the operating characteristic curves of a centrifugal pump.

Q7.3

A centrifugal pump is to discharge $ 0.118~m^3/s $ at a speed of 1450 r.p.m. against a head of 25 m. The impeller diameter is 250 mm, its width at outlet is 50 mm and manometric efficiency is 75%. Determine the vane angle at the outer periphery of the impeller.

Q.8 Solve both questions :

Q8.1

Find the number of pumps required to take water from a deep well under a total head of 89 m. All the pumps are identical and are running at 800 r.p.m. The specific speed of each pump is given as 25 while the rated capacity of each pump is $ 0.16~m^3/s $.

Q8.2

Describe with a neat sketch the construction and working of single-stage single-acting reciprocating air compressor. Also explain its actual P-V diagram.

Q.9 Solve both questions :

Q9.1

What do you mean by multistage compression? State its advantages.

Q9.2

Determine the impeller diameters and the width at the impeller exit and the power required to drive the compressor from the following data:
Speed (N) = 12500 rev/min
Mass flow rate (m) = 15 kg/s
Pressure ratio = 4:1
Isentropic efficiency = 75%
Slip factor = 0.9
Flow coefficient at impeller exit = 0.3
Hub diameter of the eye = 15 cm
Axial velocity of air at entry to and exit from the impeller = 150 m/s
Stagnation temperature at inlet = 295 K
Stagnation pressure at inlet = 1.0 bar
Assume equal pressure ratio in the impeller and diffuser.


2020 102501

B.Tech 5th Semester Exam., 2020 (New Course)

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct option of the following (any seven):

Q1.1

In hydraulic turbines,

a)

inlet energy is greater than the outlet energy

b)

outlet energy is greater than the inlet energy

c)

inlet energy is equal to the outlet energy

d)

None of the above

Q1.2

Which principle is used in hydraulic turbines?

a)

Faraday's law

b)

Newton's second law

c)

Charles' law

d)

Bragg's law

Q1.3

Which among the following is not a unit quantity of turbine?

a)

Unit speed

b)

Unit discharge

c)

Unit power

d)

Unit temperature

Q1.4

The overall efficiency of a reaction turbine is the ratio of

a)

actual work available at the turbine to the energy imparted to the wheel

b)

work done on the wheel to the energy (or head of water) actually supplied to the turbine

c)

power produced by the turbine to the energy actually supplied by the turbine

d)

None of the above

Q1.5

How many valves are there in rotary pump?

a)

3

b)

4

c)

5

d)

6

Q1.6

The ratio of power at the shaft of turbine and power delivered by water to runner is known as

a)

overall efficiency

b)

volumetric efficiency

c)

hydraulic efficiency

d)

mechanical efficiency

Q1.7

Which of the following turbines has least efficiency?

a)

Pelton turbine

b)

Kaplan turbine

c)

Francis turbine

d)

Propeller turbine

Q1.8

The hydraulic efficiency of Pelton turbine will be maximum when the blade velocity is equal to

a)

V/6V/6

b)

V/3V/3

c)

V/2V/2

d)

V/4V/4

Q1.9

When the casing in a centrifugal pump decelerates the flow, what does increase?

a)

Temperature

b)

Pressure

c)

Volume

d)

Flow rate

Q1.10

Centrifugal pump works by imparting

a)

potential energy

b)

kinetic energy

c)

heat energy

d)

electrical energy

Q.2 Solve both questions :

Q2.1

A jet of water strikes with a velocity of $ 35~m/s $ a flat plate inclined at $ 30^{\circ} $ with the axis of the jet. If the cross-sectional area of the jet is $ 25~cm^2 $, determine- (i) the force exerted by the jet on the plate; (ii) the components of the force in the direction normal to the jet; (iii) the ratio in which the discharge gets divided after striking the plate.

Q2.2

A jet of water of diameter 60 mm moving with a velocity of $ 40~m/s $, strikes a curved fixed plate tangentially at one end at an angle of $ 30^{\circ} $ to horizontal. The jet leaves the plate at an angle of $ 20^{\circ} $ to the horizontal. Find the force exerted by the jet on the plate in the horizontal and vertical directions.

Q.3 Solve both questions :

Q3.1

A Pelton wheel, having a mean bucket diameter of 1.2 m, is running at 1000 r.p.m. The net head on the Pelton wheel is 840 m. If the side clearance angle is $ 15^{\circ} $ and discharge through the nozzle is $ 0.12~m^3/s $ determine (i) power available at the nozzle, and (ii) hydraulic efficiency of the turbine.

Q3.2

Describe, with the help of sketches, the working of an impulse turbine.

Q.4 Solve both questions :

Q4.1

What is a hydraulic turbine? How will you classify them?

Q4.2

In an inward flow reaction turbine, the head on the turbine is 32 m. The external and internal diameters are 1.43 m and 0.71 m respectively. The velocity of flow through the runner is constant and equal to $ 3.2~m/s $. The guide blade angle is $ 10^{\circ} $ and the runner vanes are rigid at inlet. If the discharge at outlet is radial, determine (i) the speed of the turbine, (ii) the vane angle at outlet of the runner and (iii) hydraulic efficiency.

Q.5 Solve both questions :

Q5.1

Draw a schematic of a Francis turbine and explain briefly its construction and working.

Q5.2

A turbine is to operate under a head of 28 m at 200 r.p.m. The discharge and overall efficiency of the turbine are $ 8.5~m^3/s $ and 89%, simultaneously. Determine (i) specific speed of the turbine, (ii) power generated and (iii) types of turbine.

Q.6 Solve both questions :

Q6.1

What is cavitation? How can it be avoided in reaction turbines?

Q6.2

A turbine is to operate under a head of 23 m at 180 r.p.m. The discharge is $ 9~m^3/s $. If the overall efficiency is 90 percent, determine (i) power generated, (ii) specific speed of the turbine and (iii) types of turbine.

Q.7 Solve both questions :

Q7.1

List the main component parts of a centrifugal pump and explain them briefly.

Q7.2

The impeller of a centrifugal pump has an external diameter of 500 mm and internal diameter of 220 mm and it runs at 1400 r.p.m. Assuming a constant radial flow through the impeller at $ 2.4~m/s $ and that the vanes at exit are set back at an angle of $ 22^{\circ} $, determine- (i) the inlet vane angle; (ii) the angle, absolute velocity of water at exit makes with the tangent; (iii) the work done per N of water.

Q.8 Solve both questions :

Q8.1

A centrifugal pump impeller has diameters at inlet and outlet as 350 mm and 720 mm respectively. The flow velocity at outlet is $ 2.5~m/s $ and the vanes are set back at an angle of $ 45^{\circ} $ at the outlet. If the manometric efficiency is 70%, calculate the minimum starting speed of the pump.

Q8.2

In order to predict the performance of a large centrifugal pump, a scale model of one-sixth size was made with the following specifications: Power $ P = 25~kW $, Head $ H_{mano} = 7~m $, Speed $ N = 1000~r.p.m $. If the prototype pump has to work against a head of 22 m, calculate its (i) working speed, (ii) the power required to drive it and (iii) the ratio of the flow rates handled by the two pumps.

Q.9 Solve both questions :

Q9.1

What is a reciprocating pump? Describe the principle and working of a reciprocating pump with a neat sketch. Why is a reciprocating pump not coupled directly to the motor? Discuss the reason in detail.

Q9.2

What is negative slip in reciprocating pump? Explain with neat sketches the function of air vessels in a reciprocating pump.


2020 V4 102501

B.Tech 5th Semester Exam., 2020 (New Course)

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct option of the following (any seven):

Q1.1

In hydraulic turbines,

a)

inlet energy is greater than the outlet energy

b)

outlet energy is greater than the inlet energy

c)

inlet energy is equal to the outlet energy

d)

None of the above

Q1.2

Which principle is used in hydraulic turbines?

a)

Faraday's law

b)

Newton's second law

c)

Charles' law

d)

Bragg's law

Q1.3

Which among the following is not a unit quantity of turbine?

a)

Unit speed

b)

Unit discharge

c)

Unit power

d)

Unit temperature

Q1.4

The overall efficiency of a reaction turbine is the ratio of

a)

actual work available at the turbine to the energy imparted to the wheel

b)

work done on the wheel to the energy (or head of water) actually supplied to the turbine

c)

power produced by the turbine to the energy actually supplied by the turbine

d)

None of the above

Q1.5

How many valves are there in rotary pump?

a)

3

b)

4

c)

5

d)

6

Q1.6

The ratio of power at the shaft of turbine and power delivered by water to runner is known as

a)

overall efficiency

b)

volumetric efficiency

c)

hydraulic efficiency

d)

mechanical efficiency

Q1.7

Which of the following turbines has least efficiency?

a)

Pelton turbine

b)

Kaplan turbine

c)

Francis turbine

d)

Propeller turbine

Q1.8

The hydraulic efficiency of Pelton turbine will be maximum when the blade velocity is equal to

a)

V/6V/6

b)

V/3V/3

c)

V/2V/2

d)

V/4V/4

Q1.9

When the casing in a centrifugal pump decelerates the flow, what does increase?

a)

Temperature

b)

Pressure

c)

Volume

d)

Flow rate

Q1.10

Centrifugal pump works by imparting

a)

potential energy

b)

kinetic energy

c)

heat energy

d)

electrical energy

Q.2 Solve both questions :

Q2.1

A jet of water strikes with a velocity of $ 35~m/s $ a flat plate inclined at $ 30^{\circ} $ with the axis of the jet. If the cross-sectional area of the jet is $ 25~cm^2 $, determine- (i) the force exerted by the jet on the plate; (ii) the components of the force in the direction normal to the jet; (iii) the ratio in which the discharge gets divided after striking the plate.

Q2.2

A jet of water of diameter 60 mm moving with a velocity of $ 40~m/s $, strikes a curved fixed plate tangentially at one end at an angle of $ 30^{\circ} $ to horizontal. The jet leaves the plate at an angle of $ 20^{\circ} $ to the horizontal. Find the force exerted by the jet on the plate in the horizontal and vertical directions.

Q.3 Solve both questions :

Q3.1

A Pelton wheel, having a mean bucket diameter of 1.2 m, is running at 1000 r.p.m. The net head on the Pelton wheel is 840 m. If the side clearance angle is $ 15^{\circ} $ and discharge through the nozzle is $ 0.12~m^3/s $ determine (i) power available at the nozzle, and (ii) hydraulic efficiency of the turbine.

Q3.2

Describe, with the help of sketches, the working of an impulse turbine.

Q.4 Solve both questions :

Q4.1

What is a hydraulic turbine? How will you classify them?

Q4.2

In an inward flow reaction turbine, the head on the turbine is 32 m. The external and internal diameters are 1.43 m and 0.71 m respectively. The velocity of flow through the runner is constant and equal to $ 3.2~m/s $. The guide blade angle is $ 10^{\circ} $ and the runner vanes are rigid at inlet. If the discharge at outlet is radial, determine (i) the speed of the turbine, (ii) the vane angle at outlet of the runner and (iii) hydraulic efficiency.

Q.5 Solve both questions :

Q5.1

Draw a schematic of a Francis turbine and explain briefly its construction and working.

Q5.2

A turbine is to operate under a head of 28 m at 200 r.p.m. The discharge and overall efficiency of the turbine are $ 8.5~m^3/s $ and 89%, simultaneously. Determine (i) specific speed of the turbine, (ii) power generated and (iii) types of turbine.

Q.6 Solve both questions :

Q6.1

What is cavitation? How can it be avoided in reaction turbines?

Q6.2

A turbine is to operate under a head of 23 m at 180 r.p.m. The discharge is $ 9~m^3/s $. If the overall efficiency is 90 percent, determine (i) power generated, (ii) specific speed of the turbine and (iii) types of turbine.

Q.7 Solve both questions :

Q7.1

List the main component parts of a centrifugal pump and explain them briefly.

Q7.2

The impeller of a centrifugal pump has an external diameter of 500 mm and internal diameter of 220 mm and it runs at 1400 r.p.m. Assuming a constant radial flow through the impeller at $ 2.4~m/s $ and that the vanes at exit are set back at an angle of $ 22^{\circ} $, determine- (i) the inlet vane angle; (ii) the angle, absolute velocity of water at exit makes with the tangent; (iii) the work done per N of water.

Q.8 Solve both questions :

Q8.1

A centrifugal pump impeller has diameters at inlet and outlet as 350 mm and 720 mm respectively. The flow velocity at outlet is $ 2.5~m/s $ and the vanes are set back at an angle of $ 45^{\circ} $ at the outlet. If the manometric efficiency is 70%, calculate the minimum starting speed of the pump.

Q8.2

In order to predict the performance of a large centrifugal pump, a scale model of one-sixth size was made with the following specifications: Power $ P = 25~kW $, Head $ H_{mano} = 7~m $, Speed $ N = 1000~r.p.m $. If the prototype pump has to work against a head of 22 m, calculate its (i) working speed, (ii) the power required to drive it and (iii) the ratio of the flow rates handled by the two pumps.

Q.9 Solve both questions :

Q9.1

What is a reciprocating pump? Describe the principle and working of a reciprocating pump with a neat sketch. Why is a reciprocating pump not coupled directly to the motor? Discuss the reason in detail.

Q9.2

What is negative slip in reciprocating pump? Explain with neat sketches the function of air vessels in a reciprocating pump.


2019 021510

B.Tech 5th Semester Exam., 2019

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer from the following (any seven):

Q1.1

Where is a water hammer developed?

a)

Reservoir

b)

Penstock

c)

Turbine blades

d)

Pipeline

Q1.2

Reciprocating pump has _____ efficiency compared to centrifugal pump.

a)

lower

b)

higher

c)

equal

d)

exponential

Q1.3

The fluid coming into the centrifugal pump is accelerated by

a)

throttle

b)

impeller

c)

nozzle

d)

governor

Q1.4

Which of the following turbines will have the lowest number of blades in it?

a)

Pelton turbine

b)

Steam turbine

c)

Francis turbine

d)

Kaplan turbine

Q1.5

What is the head of water available at turbine inlet in hydro-electric power plant called?

a)

Head race

b)

Tail race

c)

Gross head

d)

Net head

Q1.6

Impulse turbine requires

a)

high head and low discharge

b)

high head and high discharge

c)

low head and low discharge

d)

low head and high discharge

Q1.7

The ratio of actual whirl velocity to the ideal whirl velocity in the centrifugal compressor is called as

a)

velocity factor

b)

slip factor

c)

work factor

d)

None of the above

Q1.8

The mass flow rate of air compressed in axial flow compressor is _____ centrifugal compressor.

a)

lower than

b)

higher than

c)

same as

d)

Unpredictable

Q1.9

Compression efficiency is compared against

a)

isothermal compression

b)

isentropic compression

c)

adiabatic compression

d)

both isothermal and adiabatic compression

Q1.10

Jet propulsion works on the principle of

a)

Newton's first law

b)

Newton's second law

c)

Newton's third law

d)

Thermodynamic properties

Q.2 Solve both questions :

Q2.1

A jet of water of diameter 10 cm strikes flat plate normally with velocity of 15 $ m/s $. The plate is moving with a velocity of 6 $ m/s $ in the direction of the jet and away from the jet. Find- (i) the force exerted by the jet on the plate; (ii) work done by the jet on the plate per second.

Q2.2

Obtain an expression for the force exerted by a jet of water (strikes at the centre) on a stationary curved plate.

Q.3 Solve both questions :

Q3.1

Show that the force exerted by a jet of water on moving inclined plane in the direction of jet is given by $ F_x = \rho a (V - u)^2 \sin^2 \theta $ where, $ a = $ area of jet, $ \theta = $ inclination of the plate with the jet and $ v = $ velocity of jet.

Q3.2

Show the general layout of a hydro-electric power plant and explain each component in brief.

Q.4 Solve both questions :

Q4.1

What do you mean by gross head, net head and efficiency of turbine? Explain the different types of efficiency of a turbine.

Q4.2

Prove that the work done per second per unit weight of water in a reaction turbine is given as $ \frac{1}{g}(V_{u_1}u_1 \pm V_{u_2}u_2) $ where, $ V_{u_1} $ and $ V_{u_2} $ are velocities of whirl at inlet and outlet; $ u_1 $ and $ u_2 $ are peripheral velocities at inlet and outlet.

Q.5 Solve both questions :

Q5.1

A Francis turbine working under a head of 30 m has a wheel diameter of 1.2 m at the entrance and 0.6 m at the exit. The vane angle at the entrance is $ 90^{\circ} $ and guide blade angle is $ 15^{\circ} $. The water at the exit leaves the vanes without any tangential velocity and the velocity of flow in the runner is constant. Neglecting the effect of draft tube and losses in the guide and runner passages, determine the speed of wheel in rpm and vane angle at the exit. State whether the speed calculated is synchronous or not. If not, what speed would you recommend to couple the turbine with an alternator of 50 cycles?

Q5.2

What is cavitation? How can it be avoided in reaction turbine?

Q.6 Solve both questions :

Q6.1

A turbine develops 3000 kW under head of 300 m. The overall efficiency of the turbine is 83%. If speed ratio = 0.46, $ C_v = 0.98 $ and specific speed is 165, then find the (i) type of turbine, (ii) diameter of the turbine and (iii) diameter of the jet.

Q6.2

Define slip, percentage slip and negative slip of a reciprocating pump.

Q6.3

How will you classify the reciprocating pumps?

Q.7 Solve both questions :

Q7.1

A double-acting reciprocating pump, running at 40 r.p.m., is discharging $ 1~m^3 $ of water per minute. The pump has a stroke of 400 mm. The diameter of the piston is 200 mm. The delivery and suction head are 20 m and 5 m respectively. Find the slip of the pump and power required to deliver the pump.

Q7.2

A centrifugal pump has the dimensions-inlet radius 80 mm, outlet radius 160 mm, width of impeller at the inlet = 50 mm, $ \beta_1 = 0.45 $ radian, $ \beta_2 = 0.25 $ radian, width of impeller at the outlet = 50 mm. Assuming shockless entry, determine the discharge and the head developed by the pump when the impeller rotates at 90 radian/second.

Q.8 Solve all three questions :

Q8.1

How will you obtain an expression for the minimum speed for starting a centrifugal pump?

Q8.2

What is the effect of atmospheric condition on the output of compressor?

Q8.3

Air is to be compressed in a single-stage reciprocating compressor from 1.013 bar and $ 15^{\circ}C $ to 7 bar. Calculate the indicated power required for a free air delivery of $ 0.3~m^3/min $, when the compression process is isentropic.

Q.9 Solve both questions :

Q9.1

Explain with a neat sketch actual $ p-V $ diagram for a two-stage reciprocating compressor.

Q9.2

A single-sided centrifugal compressor is to deliver 14 kg of air per second, when operating at a pressure ratio 4:1 and a speed of 12000 r.p.m. The total head inlet conditions may be taken as 288 K and 1.033 $ kgf/cm^2 $. Assuming a slip factor as 0.9, a power input factor 1.04 and an isentropic efficiency (based on total head) of 80%, estimate the overall diameter of the impeller. If the Mach number is not to exceed unity at the impeller tip and 50% of the losses are assumed to occur in the impeller, find the minimum possible depth of the diffuser.


2019 V4 021510

B.Tech 5th Semester Exam., 2019

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer from the following (any seven):

Q1.1

Where is a water hammer developed?

a)

Reservoir

b)

Penstock

c)

Turbine blades

d)

Pipeline

Q1.2

Reciprocating pump has _____ efficiency compared to centrifugal pump.

a)

lower

b)

higher

c)

equal

d)

exponential

Q1.3

The fluid coming into the centrifugal pump is accelerated by

a)

throttle

b)

impeller

c)

nozzle

d)

governor

Q1.4

Which of the following turbines will have the lowest number of blades in it?

a)

Pelton turbine

b)

Steam turbine

c)

Francis turbine

d)

Kaplan turbine

Q1.5

What is the head of water available at turbine inlet in hydro-electric power plant called?

a)

Head race

b)

Tail race

c)

Gross head

d)

Net head

Q1.6

Impulse turbine requires

a)

high head and low discharge

b)

high head and high discharge

c)

low head and low discharge

d)

low head and high discharge

Q1.7

The ratio of actual whirl velocity to the ideal whirl velocity in the centrifugal compressor is called as

a)

velocity factor

b)

slip factor

c)

work factor

d)

None of the above

Q1.8

The mass flow rate of air compressed in axial flow compressor is _____ centrifugal compressor.

a)

lower than

b)

higher than

c)

same as

d)

Unpredictable

Q1.9

Compression efficiency is compared against

a)

isothermal compression

b)

isentropic compression

c)

adiabatic compression

d)

both isothermal and adiabatic compression

Q1.10

Jet propulsion works on the principle of

a)

Newton's first law

b)

Newton's second law

c)

Newton's third law

d)

Thermodynamic properties

Q.2 Solve both questions :

Q2.1

A jet of water of diameter 10 cm strikes flat plate normally with velocity of 15 $ m/s $. The plate is moving with a velocity of 6 $ m/s $ in the direction of the jet and away from the jet. Find- (i) the force exerted by the jet on the plate; (ii) work done by the jet on the plate per second.

Q2.2

Obtain an expression for the force exerted by a jet of water (strikes at the centre) on a stationary curved plate.

Q.3 Solve both questions :

Q3.1

Show that the force exerted by a jet of water on moving inclined plane in the direction of jet is given by $ F_x = \rho a (V - u)^2 \sin^2 \theta $ where, $ a = $ area of jet, $ \theta = $ inclination of the plate with the jet and $ v = $ velocity of jet.

Q3.2

Show the general layout of a hydro-electric power plant and explain each component in brief.

Q.4 Solve both questions :

Q4.1

What do you mean by gross head, net head and efficiency of turbine? Explain the different types of efficiency of a turbine.

Q4.2

Prove that the work done per second per unit weight of water in a reaction turbine is given as $ \frac{1}{g}(V_{u_1}u_1 \pm V_{u_2}u_2) $ where, $ V_{u_1} $ and $ V_{u_2} $ are velocities of whirl at inlet and outlet; $ u_1 $ and $ u_2 $ are peripheral velocities at inlet and outlet.

Q.5 Solve both questions :

Q5.1

A Francis turbine working under a head of 30 m has a wheel diameter of 1.2 m at the entrance and 0.6 m at the exit. The vane angle at the entrance is $ 90^{\circ} $ and guide blade angle is $ 15^{\circ} $. The water at the exit leaves the vanes without any tangential velocity and the velocity of flow in the runner is constant. Neglecting the effect of draft tube and losses in the guide and runner passages, determine the speed of wheel in rpm and vane angle at the exit. State whether the speed calculated is synchronous or not. If not, what speed would you recommend to couple the turbine with an alternator of 50 cycles?

Q5.2

What is cavitation? How can it be avoided in reaction turbine?

Q.6 Solve both questions :

Q6.1

A turbine develops 3000 kW under head of 300 m. The overall efficiency of the turbine is 83%. If speed ratio = 0.46, $ C_v = 0.98 $ and specific speed is 165, then find the (i) type of turbine, (ii) diameter of the turbine and (iii) diameter of the jet.

Q6.2

Define slip, percentage slip and negative slip of a reciprocating pump.

Q6.3

How will you classify the reciprocating pumps?

Q.7 Solve both questions :

Q7.1

A double-acting reciprocating pump, running at 40 r.p.m., is discharging $ 1~m^3 $ of water per minute. The pump has a stroke of 400 mm. The diameter of the piston is 200 mm. The delivery and suction head are 20 m and 5 m respectively. Find the slip of the pump and power required to deliver the pump.

Q7.2

A centrifugal pump has the dimensions-inlet radius 80 mm, outlet radius 160 mm, width of impeller at the inlet = 50 mm, $ \beta_1 = 0.45 $ radian, $ \beta_2 = 0.25 $ radian, width of impeller at the outlet = 50 mm. Assuming shockless entry, determine the discharge and the head developed by the pump when the impeller rotates at 90 radian/second.

Q.8 Solve all three questions :

Q8.1

How will you obtain an expression for the minimum speed for starting a centrifugal pump?

Q8.2

What is the effect of atmospheric condition on the output of compressor?

Q8.3

Air is to be compressed in a single-stage reciprocating compressor from 1.013 bar and $ 15^{\circ}C $ to 7 bar. Calculate the indicated power required for a free air delivery of $ 0.3~m^3/min $, when the compression process is isentropic.

Q.9 Solve both questions :

Q9.1

Explain with a neat sketch actual $ p-V $ diagram for a two-stage reciprocating compressor.

Q9.2

A single-sided centrifugal compressor is to deliver 14 kg of air per second, when operating at a pressure ratio 4:1 and a speed of 12000 r.p.m. The total head inlet conditions may be taken as 288 K and 1.033 $ kgf/cm^2 $. Assuming a slip factor as 0.9, a power input factor 1.04 and an isentropic efficiency (based on total head) of 80%, estimate the overall diameter of the impeller. If the Mach number is not to exceed unity at the impeller tip and 50% of the losses are assumed to occur in the impeller, find the minimum possible depth of the diffuser.


2018 021510

B.Tech 5th Semester Exam., 2018

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer from the following (any seven):

Q1.1

The force of impingement of a jet on a vane increases, if

a)

the vane angle is increased

b)

the vane angle is decreased

c)

the pressure is reduced

d)

the vane is moved against the jet

Q1.2

A jet of water issues from a nozzle with a velocity of 20 m/s and it impinges normally on a flat plate moving away from it at $ 10~m/s $. If the cross-sectional area of the jet is $ 0.02~m^2 $ and the density of water is taken as $ 1000~kg/m^3 $, then the force developed on the plate will be

a)

10 N

b)

100 N

c)

1000 N

d)

2000 N

Q1.3

Kaplan turbine is

a)

a high head mixed flow turbine

b)

a low axial flow turbine

c)

an outward flow reaction turbine

d)

an impulse inward flow turbine

Q1.4

Cavitation in a hydraulic turbine is most likely to occur at the turbine

a)

entry

b)

exit

c)

stator exit

d)

rotor exit

Q1.5

Euler equation for water turbine is derived on the basis of

a)

conservation of mass

b)

rate of change of linear momentum

c)

rate of change of angular momentum

d)

rate of change of velocity

Q1.6

A Francis turbine is coupled to an alternator to generate electricity with a frequency of 50 Hz. If the alternator has 12 poles, then the turbine should be regulated to run at which one of the following constant speeds?

a)

250 r.p.m.

b)

500 r.p.m.

c)

600 r.p.m.

d)

1000 r.p.m.

Q1.7

Consider the following types of water turbines: 1. Bulb, 2. Francis, 3. Kaplan, 4. Pelton. One correct sequence of order in which the operating head decreases while developing the same power is

a)

4-2-3-1

b)

3-4-1-2

c)

2-1-4-3

d)

1-3-2-4

Q1.8

When the speed of a centrifugal pump is doubled, the power required to drive the pump will

a)

increase 8 times

b)

increase 4 times

c)

double

d)

remain the same

Q1.9

A centrifugal pump driven by a directly coupled 3 kW motor of 1450 r.p.m. speed is proposed to be connected to another motor of 2900 r.p.m. speed. The power of the motor should be

a)

6 kW

b)

12 kW

c)

18 kW

d)

24 kW

Q1.10

Air vessel is used in a reciprocating pump to obtain

a)

reduction of suction heat

b)

rise in delivery head

c)

continuous supply of water at uniform rate

d)

increase in supply of water

Q.2 Solve both questions :

Q2.1

Differentiate between impact of jet and jet propulsion. Show that the force exerted by a jet of water on moving inclined plate in the direction of jet is given by $ F_x = \rho a (V-u)^2 \sin^2 \theta $ where a is area of jet, V is velocity of jet and $ \theta $ is inclination of the plate with the jet.

Q2.2

A 75 mm diameter jet having a velocity of $ 30~m/s $ strikes a flat plate, the normal of which is inclined at $ 45^{\circ} $ to the axis of the jet. Find the normal pressure on the plate when the plate is stationary, when the plate is moving with a velocity of $ 15~m/s $ in the direction of jet, away from the jet and also determine the efficiency of the jet when the plate is moving.

Q.3 Solve both questions :

Q3.1

Derive Euler's equation of motion. Also derive Bernoulli's equation with the help of Euler's equation.

Q3.2

A pipe 200 m long slopes down at 1 in 100 and tapers from 600 mm diameter at the higher end to 300 mm diameter at the lower end, and carries $ 100~litres/s $ of oil (specific gravity 0.8). If the pressure gauge at the higher end reads $ 60~kN/m^2 $, calculate velocities at the two ends and pressure at the lower end neglecting all the losses.

Q.4 Solve both questions :

Q4.1

What is a hydraulic turbine? How are they classified? With the help of neat sketch, explain the construction and working of a Pelton wheel turbine.

Q4.2

An inward flow reaction turbine has external and internal diameters as 1 m and 0.5 m respectively. The turbine is running at 200 r.p.m. and width of turbine at inlet is 200 mm. The velocity of flow through the runner is constant and is equal to $ 1.8~m/s $. The guide blades make an angle of $ 10^{\circ} $ to the tangent of the wheel and the discharge at the outlet of the turbine is radial. Calculate all velocity vectors and draw the inlet and outlet velocity triangles. Also calculate mass flow through the runner/second, power developed and hydraulic efficiency.

Q.5 Solve both questions :

Q5.1

What is model analysis? What are the advantages and applications of model testing?

Q5.2

A 1:8 model of a 12 ft diameter turbine is operated at 600 r.p.m. under a net head of 54.0 ft. Under this mode of operation, the bhp and Q of the model were observed, to be 332 hp and 62 cfs, respectively. From the above data, compute (i) the specific speed of the model and the value of $ \sigma $, (ii) the efficiency and shaft torque of the model, (iii) the efficiency of the prototype, (iv) the flow rate and horsepower of the prototype if it is operated at 450 r.p.m. under a net head of 200 ft.

Q.6 Solve both questions :

Q6.1

What is negative slip in a reciprocating pump? Explain with neat sketches the functions of air vessels in a reciprocating pump.

Q6.2

The diameter and stroke length of a single-acting reciprocating pump are 75 mm and 150 mm respectively. It takes its supply of water from a sump 3 m below the pump through a pipe 5 m long and 40 mm in diameter. It delivers water to a tank 12 m above the pump through a pipe 30 mm in diameter and 15 m long. If separation occurs 75 kN/$ m^2 $ below the atmospheric pressure, find the maximum speed at which pump may be operated without separation. Assume that the piston has a simple harmonic motion.

Q.7 Solve both questions :

Q7.1

With the help of neat sketch, discuss various components and working of a volute type centrifugal pump.

Q7.2

A centrifugal pump is running at 1000 r.p.m. The outlet vane angle of the impeller is $ 30^{\circ} $ and the velocity of flow at outlet is $ 3~m/s $. The pump is working against a total head of 30 m and the discharge through the pump is $ 0.3~m^3/s $. If the manometric efficiency of the pump is 75%, determine (i) the diameter of the impeller and (ii) width of the impeller at the outlet.

Q.8 Solve both questions :

Q8.1

What are reciprocating compressors? Calculate the isothermal and adiabatic work and efficiency of a single-stage reciprocating compressor.

Q8.2

A two-stage single reciprocating compressor takes in air at the rate of $ 2~m^3/s $. The intake temperature and pressure of air are 0.1 MPa and $ 16^{\circ}C $. The air is compressed to a final pressure of 0.7 MPa. The intermediate pressure is ideal and cooling is perfect. The compression index in both the stages is 1.25 and the compressor runs at 600 r.p.m. Neglect clearance. Determine intermediate pressure, total volume of each cylinder, power required to drive the compressor and rate of heat rejection in the intercooler.

Q.9 Solve both questions :

Q9.1

What are centrifugal compressors? With the help of velocity diagram, deduce the expression of work done and pressure rise in centrifugal compressor.

Q9.2

A centrifugal compressor runs at a speed of 15000 r.p.m. and delivers 30 kg of air per second. Exit radius is 0.35 m, relative velocity at exit is $ 100~m/s $ at an exit angle of $ 75^{\circ} $. Assume axial inlet and $ T_{01}=300~K $ and $ P_{01}=1~bar $. Calculate (i) the torque, (ii) the power required to drive the compressor, (iii) the ideal head developed (iv) the work done and (v) the exit total pressure.


2018 V4 021510

B.Tech 5th Semester Exam., 2018

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Q.1 Choose the correct answer from the following (any seven):

Q1.1

The force of impingement of a jet on a vane increases, if

a)

the vane angle is increased

b)

the vane angle is decreased

c)

the pressure is reduced

d)

the vane is moved against the jet

Q1.2

A jet of water issues from a nozzle with a velocity of 20 m/s and it impinges normally on a flat plate moving away from it at $ 10~m/s $. If the cross-sectional area of the jet is $ 0.02~m^2 $ and the density of water is taken as $ 1000~kg/m^3 $, then the force developed on the plate will be

a)

10 N

b)

100 N

c)

1000 N

d)

2000 N

Q1.3

Kaplan turbine is

a)

a high head mixed flow turbine

b)

a low axial flow turbine

c)

an outward flow reaction turbine

d)

an impulse inward flow turbine

Q1.4

Cavitation in a hydraulic turbine is most likely to occur at the turbine

a)

entry

b)

exit

c)

stator exit

d)

rotor exit

Q1.5

Euler equation for water turbine is derived on the basis of

a)

conservation of mass

b)

rate of change of linear momentum

c)

rate of change of angular momentum

d)

rate of change of velocity

Q1.6

A Francis turbine is coupled to an alternator to generate electricity with a frequency of 50 Hz. If the alternator has 12 poles, then the turbine should be regulated to run at which one of the following constant speeds?

a)

250 r.p.m.

b)

500 r.p.m.

c)

600 r.p.m.

d)

1000 r.p.m.

Q1.7

Consider the following types of water turbines: 1. Bulb, 2. Francis, 3. Kaplan, 4. Pelton. One correct sequence of order in which the operating head decreases while developing the same power is

a)

4-2-3-1

b)

3-4-1-2

c)

2-1-4-3

d)

1-3-2-4

Q1.8

When the speed of a centrifugal pump is doubled, the power required to drive the pump will

a)

increase 8 times

b)

increase 4 times

c)

double

d)

remain the same

Q1.9

A centrifugal pump driven by a directly coupled 3 kW motor of 1450 r.p.m. speed is proposed to be connected to another motor of 2900 r.p.m. speed. The power of the motor should be

a)

6 kW

b)

12 kW

c)

18 kW

d)

24 kW

Q1.10

Air vessel is used in a reciprocating pump to obtain

a)

reduction of suction heat

b)

rise in delivery head

c)

continuous supply of water at uniform rate

d)

increase in supply of water

Q.2 Solve both questions :

Q2.1

Differentiate between impact of jet and jet propulsion. Show that the force exerted by a jet of water on moving inclined plate in the direction of jet is given by $ F_x = \rho a (V-u)^2 \sin^2 \theta $ where a is area of jet, V is velocity of jet and $ \theta $ is inclination of the plate with the jet.

Q2.2

A 75 mm diameter jet having a velocity of $ 30~m/s $ strikes a flat plate, the normal of which is inclined at $ 45^{\circ} $ to the axis of the jet. Find the normal pressure on the plate when the plate is stationary, when the plate is moving with a velocity of $ 15~m/s $ in the direction of jet, away from the jet and also determine the efficiency of the jet when the plate is moving.

Q.3 Solve both questions :

Q3.1

Derive Euler's equation of motion. Also derive Bernoulli's equation with the help of Euler's equation.

Q3.2

A pipe 200 m long slopes down at 1 in 100 and tapers from 600 mm diameter at the higher end to 300 mm diameter at the lower end, and carries $ 100~litres/s $ of oil (specific gravity 0.8). If the pressure gauge at the higher end reads $ 60~kN/m^2 $, calculate velocities at the two ends and pressure at the lower end neglecting all the losses.

Q.4 Solve both questions :

Q4.1

What is a hydraulic turbine? How are they classified? With the help of neat sketch, explain the construction and working of a Pelton wheel turbine.

Q4.2

An inward flow reaction turbine has external and internal diameters as 1 m and 0.5 m respectively. The turbine is running at 200 r.p.m. and width of turbine at inlet is 200 mm. The velocity of flow through the runner is constant and is equal to $ 1.8~m/s $. The guide blades make an angle of $ 10^{\circ} $ to the tangent of the wheel and the discharge at the outlet of the turbine is radial. Calculate all velocity vectors and draw the inlet and outlet velocity triangles. Also calculate mass flow through the runner/second, power developed and hydraulic efficiency.

Q.5 Solve both questions :

Q5.1

What is model analysis? What are the advantages and applications of model testing?

Q5.2

A 1:8 model of a 12 ft diameter turbine is operated at 600 r.p.m. under a net head of 54.0 ft. Under this mode of operation, the bhp and Q of the model were observed, to be 332 hp and 62 cfs, respectively. From the above data, compute (i) the specific speed of the model and the value of $ \sigma $, (ii) the efficiency and shaft torque of the model, (iii) the efficiency of the prototype, (iv) the flow rate and horsepower of the prototype if it is operated at 450 r.p.m. under a net head of 200 ft.

Q.6 Solve both questions :

Q6.1

What is negative slip in a reciprocating pump? Explain with neat sketches the functions of air vessels in a reciprocating pump.

Q6.2

The diameter and stroke length of a single-acting reciprocating pump are 75 mm and 150 mm respectively. It takes its supply of water from a sump 3 m below the pump through a pipe 5 m long and 40 mm in diameter. It delivers water to a tank 12 m above the pump through a pipe 30 mm in diameter and 15 m long. If separation occurs 75 kN/$ m^2 $ below the atmospheric pressure, find the maximum speed at which pump may be operated without separation. Assume that the piston has a simple harmonic motion.

Q.7 Solve both questions :

Q7.1

With the help of neat sketch, discuss various components and working of a volute type centrifugal pump.

Q7.2

A centrifugal pump is running at 1000 r.p.m. The outlet vane angle of the impeller is $ 30^{\circ} $ and the velocity of flow at outlet is $ 3~m/s $. The pump is working against a total head of 30 m and the discharge through the pump is $ 0.3~m^3/s $. If the manometric efficiency of the pump is 75%, determine (i) the diameter of the impeller and (ii) width of the impeller at the outlet.

Q.8 Solve both questions :

Q8.1

What are reciprocating compressors? Calculate the isothermal and adiabatic work and efficiency of a single-stage reciprocating compressor.

Q8.2

A two-stage single reciprocating compressor takes in air at the rate of $ 2~m^3/s $. The intake temperature and pressure of air are 0.1 MPa and $ 16^{\circ}C $. The air is compressed to a final pressure of 0.7 MPa. The intermediate pressure is ideal and cooling is perfect. The compression index in both the stages is 1.25 and the compressor runs at 600 r.p.m. Neglect clearance. Determine intermediate pressure, total volume of each cylinder, power required to drive the compressor and rate of heat rejection in the intercooler.

Q.9 Solve both questions :

Q9.1

What are centrifugal compressors? With the help of velocity diagram, deduce the expression of work done and pressure rise in centrifugal compressor.

Q9.2

A centrifugal compressor runs at a speed of 15000 r.p.m. and delivers 30 kg of air per second. Exit radius is 0.35 m, relative velocity at exit is $ 100~m/s $ at an exit angle of $ 75^{\circ} $. Assume axial inlet and $ T_{01}=300~K $ and $ P_{01}=1~bar $. Calculate (i) the torque, (ii) the power required to drive the compressor, (iii) the ideal head developed (iv) the work done and (v) the exit total pressure.


2017 021510

B.Tech Examination, 2017

Time 3 hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Questions

Q1

Choose the correct answer of the following (any seven) :

a)

A free water jet acts upon a water wheel that has semi-circular vanes fitted on its periphery. The theoretical maximum efficiency of this wheel system is

a)

(i) 50%50\%

b)

(ii) 67%67\%

c)

(iii) 75%75\%

d)

(iv) 100%100\%

b)

The unit speed NuN_u of a turbine having a rotational speed of NN and head HH is equal to

a)

(i) NH0.5N H^{0.5}

b)

(ii) N/H0.5N / H^{0.5}

c)

(iii) H0.5/NH^{0.5} / N

d)

(iv) (H/N)0.5(H / N)^{0.5}

c)

Specific speed of a turbine is defined as the speed of a member of same homologous series of such a size that it

a)

(i) delivers unit discharge at unit head

b)

(ii) delivers unit discharge at unit power

c)

(iii) delivers unit power at unit discharge

d)

(iv) produces unit power under unit head

d)

What does Euler's equation of turbo machines relate to?

a)

(i) Discharge and head

b)

(ii) Discharge and velocities

c)

(iii) Head and power

d)

(iv) Head and velocities

e)

In a Francis turbine, the runner blades are radial at the inlet and the discharge leaves the runner radially at the exit. For this turbine

a)

(i) relative velocity is radial at the outlet

b)

(ii) absolute velocity is radial at the outlet

c)

(iii) guide-vane angle is 9090^\circ at inlet

d)

(iv) velocity of flow is constant

f)

Without residual whirl in the flow at the entrance to a draft tube, the best cone angle is

a)

(i) <10< 10^\circ

b)

(ii) 1212^\circ

c)

(iii) 1818^\circ

d)

(iv) 2424^\circ

g)

A Kaplan turbine is

a)

(i) a high-head mixed-flow turbine

b)

(ii) a low-head axial-flow turbine

c)

(iii) an outward-flow reaction turbine

d)

(iv) an inward-flow impulse turbine

h)

A centrifugal pump is started with its delivery valve kept

a)

(i) fully open

b)

(ii) fully shut

c)

(iii) partially open

d)

(iv) 50%50\% open

i)

The indicator diagram of a reciprocating pump is a plot of

a)

(i) work done vs stroke length

b)

(ii) acceleration head vs stroke length

c)

(iii) pressure head vs stroke length

d)

(iv) crank speed vs power developed

j)

A centrifugal jet pump is classified as

a)

(i) positive displacement pump

b)

(ii) rotary pump

c)

(iii) hydrostatic pump

d)

(iv) None of the above

[14 Marks]
Q2

Answer the following:

a)

Explain the similarity laws for turbines.

[5 Marks]
b)

A 10 cm10\text{ cm} diameter jet of water strikes a curved vane with a velocity of 25 m/s25\text{ m/s}. The inlet angle of the vane is zero and the outlet angle is 150150^\circ measured with respect to the impinging jet direction. Determine the resultant force on the vane when the vane is stationary.

[9 Marks]
Q3

An inward-flow reaction turbine has an inlet guide vane angle of 3030^\circ and inward edges of the runner blade at 115115^\circ to the direction of rotation. The breadth of the runner at the inlet is a quarter of the inlet diameter and there is no whirl velocity at the outlet. The gross head is 20 m20\text{ m} and the speed is 1000 r.p.m.1000\text{ r.p.m.} The hydraulic and overall efficiencies may be assumed to be 88%88\% and 85%85\% respectively. Estimate the runner diameter at inlet and the power developed.

[14 Marks]
Q4

Answer the following:

a)

What are the different characteristics of Francis turbine? Discuss any one of them.

[6 Marks]
b)

A Francis turbine develops 800 kW800\text{ kW} at an efficiency of 90%90\% under a net head of 12 m12\text{ m}. The draft tube used in this setup is a vertical cylindrical pipe of 2 m2\text{ m} diameter. (a) What increase in power could be expected if a tapering vertical draft tube having an outlet diameter of 2.5 m2.5\text{ m} replaces the existing cylindrical draft tube? (b) What would be the increase in the overall efficiency? Assume that the head, speed and discharge remain the same and there are no additional friction losses due to the new draft tube.

[8 Marks]
Q5

Answer the following:

a)

Explain different component parts of a centrifugal pump.

[6 Marks]
b)

A centrifugal pump delivers water at the rate of 40 litres/sec40\text{ litres/sec} for a total head of 30 m30\text{ m}. Find the output of the pump. If the overall efficiency of the set consisting of the pump and the electric motor is 75%75\%, find the power required to drive the motor.

[8 Marks]
Q6

A centrifugal pump is required to discharge 600 litres/sec600\text{ litres/sec} of water and develop a head of 15 m15\text{ m} when the impeller rotates at 750 r.p.m.750\text{ r.p.m.} The manometric efficiency is 0.800.80. The loss of head in the pump due to fluid resistance can be assumed to be 0.027V20.027V^2 where, V=V = velocity with which the water leaves the impeller. Water enters the impeller without shock and whirl and the velocity of flow is 3.2 m/s3.2\text{ m/s}. Determine the (a) impeller diameter, (b) blade angle at outlet and (c) outlet area.

[14 Marks]
Q7

Answer the following:

a)

Define slip in a reciprocating pump. Explain the phenomenon of negative slip.

[6 Marks]
b)

A single-acting reciprocating pump has a plunger of diameter of 250 mm250\text{ mm} and stroke of 350 mm350\text{ mm}. If the speed of the pump is 60 r.p.m.60\text{ r.p.m.} and if it delivers 16.5 litres/sec16.5\text{ litres/sec} of water against a suction head of 5 m5\text{ m} and a delivery head of 20 m20\text{ m}, find the theoretical discharge, coefficient of discharge, slip, the percentage slip of the pump and the power required to drive the pump.

[8 Marks]
Q8

A 1/51/5 scale model of a prototype air compressor consuming 225 kW225\text{ kW} and running at a speed of 1000 r.p.m.1000\text{ r.p.m.} delivers a flow rate of 9 kg/s9\text{ kg/s} through a pressure ratio of 55. At dynamically and kinematically similar conditions, what would the operating speed, mass flow rate and power consumption be for the full-scale prototype?

[14 Marks]
Q9

Write short notes on any two of the following :

a)

Draft tube

b)

Turbine

c)

Specific speed of pump

d)

Priming of a pump

[14 Marks]

2016 021510

B.Tech Examination, 2016

Time 3 hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Questions

Q1

Define the following terms (any seven) :

a)

Jet Impingement

b)

Nozzle

c)

Penstock

d)

Propeller Turbine

e)

Head Race

f)

Unit Discharge

g)

Scroll Casing

h)

Runner

i)

Mechanical Efficiency of a Pump

j)

Guide Vane Angle

[14 Marks]
Q2

Answer the following:

a)

A jet of water, 5 cm5\text{ cm} in diameter, issues with a velocity of 20 m/s20\text{ m/s} and impinges on a series of vanes. The vanes are so arranged that each vane appears successively before that jet in the same position and always moves with velocity of 5 m/s5\text{ m/s}. Find force on the plate, work done and the efficiency of system.

[5 Marks]
b)

A jet of water having a velocity of 45 m/s45\text{ m/s} impinges without shock on a series of vanes moving at 15 m/s15\text{ m/s}. The direction of motion of the vanes is inclined at 2020^\circ to that of the jet, the relative velocity at outlet is 0.90.9 of that at inlet, and the absolute velocity of the water at the exit is to be normal to the motion of vanes, find (i) vane angles at entrance and exit; (ii) work done on vanes per kg of water supplied by the jet; and (iii) hydraulic efficiency.

[9 Marks]
Q3

Answer the following:

a)

What is the basis of selection of a turbine at a particular place?

[5 Marks]
b)

A turbine develops 3000 kW3000\text{ kW} under a head of 300 m300\text{ m}. The overall efficiency of the turbine is 83%83\%. If speed ratio = 0.460.46, Cv=0.98C_v = 0.98 and specific speed is 16.516.5, then find the (i) Type of turbine, (ii) Diameter of the turbine, and (iii) Diameter of the jet.

[9 Marks]
Q4

Answer the following:

a)

Define the specific speed of a Turbine. Derive an expression for the specific speed.

[7 Marks]
b)

Prove that the work done per second per unit weight of water in a reaction turbine is given as: $$\frac{1}{g}(V_{w1} u_1 \pm V_{w2} u_2)$$ Where, Vw1V_{w1} and Vw2=V_{w2} = velocities of whirl at inlet and outlet.

[7 Marks]
Q5

Answer the following:

a)

What is a Draft tube? Explain with neat sketch.

[4 Marks]
b)

A Francis turbine working under a head of 30 m30\text{ m} has a wheel diameter of 1.2 m1.2\text{ m} at the entrance and 0.6 m0.6\text{ m} at the exit. The vane angle at the entrance is 9090^\circ and guide blade angle is 1515^\circ. The water at the exit leaves the vanes without any tangential velocity and the velocity of flow in the runner is constant. neglecting the effect of draft tube and losses in the guide and runner passages, determine the speed of wheel in r.p.m. and vane angle at the exit. State whether the speed calculated is synchronous or not. If not, what speed would you recommend to couple the turbine with an alternator of 50 cycles50\text{ cycles}?

[10 Marks]
Q6

Answer the following:

a)

What do you understand by characteristics curves of a pump? Explain with sketch.

[6 Marks]
b)

A centrifugal pump has the following dimensions: inlet radius = 80 mm80\text{ mm}, outlet radius = 160 mm160\text{ mm}, width of impeller at the inlet = 50 mm50\text{ mm}, β1=0.45 radians\beta_1 = 0.45\text{ radians}, β2=0.25 radians\beta_2 = 0.25\text{ radians}. Width of impeller at the outlet = 50 mm50\text{ mm}. Assuming shockless entry and determine the discharge and the head developed by the pump when the impeller rotates at 90 radians/second90\text{ radians/second}.

[8 Marks]
Q7

Answer the following:

a)

What are the causes of cavitation? How will you prevent the cavitation in hydraulic Machines?

[7 Marks]
b)

Define Indicator diagram. How will you prove that area of indicator diagram is proportional to the work done by the reciprocating pump?

[7 Marks]
Q8

Answer the following:

a)

How will you classify the reciprocating pump?

[4 Marks]
b)

The cylinder bore diameter of a single acting reciprocating pump is 150 mm150\text{ mm} and its stroke is 300 mm300\text{ mm}. The pump runs at 50 rpm50\text{ rpm} and lifts water through a height of 25 m25\text{ m}. the delivery pipe is 22 m22\text{ m} long and 100 mm100\text{ mm} in diameter. Find the theoretical discharge and the theoretical power required to run the pump. If the actual discharge is 4.2 litres/s4.2\text{ litres/s}, find the percentage slip. Also, determine the acceleration head at the beginning and middle of the delivery stroke.

[10 Marks]
Q9

Answer the following:

a)

A single inlet-type centrifugal compressor handles 528 kg/min528\text{ kg/min} of air. The ambient air condition are 1 bar1\text{ bar} and 20C20^\circ\text{C}. The compressor runs at 20000 rpm20000\text{ rpm} with isentropic efficiency of 80%80\%. The air is compressed in the compressor from 1 bar1\text{ bar} static pressure to 4 bar4\text{ bar} total pressure. The air enters the impeller eye with a velocity of 145 m/s145\text{ m/s} with no prewhirl. Assuming that the ratio of whirl speed to tip speed is 0.900.90, calculate: (i) Rise in total temperature during compression if the change in K.E. is negligible (ii) The tip diameter of the impeller (iii) Power required (iv) Eye diameter if the hub diameter is 12 cm12\text{ cm}.

[9 Marks]
b)

What is a centrifugal compressor? How does it differ from an axial flow compressor?

[5 Marks]

2015 021510

B.Tech Examination, 2015

Time 3 hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Questions

Q1

Define the following terms (any seven) :

a)

Gross head

b)

Net head

c)

Inward radial flow turbine

d)

Outward radial flow turbine

e)

Unit speed

f)

Unit discharge

g)

Draft tube

h)

Manometric efficiency

i)

Air vessel

j)

Slip

[14 Marks]
Q2

Answer the following:

a)

Obtain an expression for the force exerted by a jet of water on a fixed vertical plate in the direction of jet.

[4 Marks]
b)

A jet of water of diameter 75 mm75\text{ mm} moving with a velocity of 25 m/s25\text{ m/s} strikes a fixed plate in such a way that the angle between the jet and plate is 6060^\circ. Find the force exerted by jet on the plate— (i) in the direction normal to the plate; (ii) in the direction of jet.

[5 Marks]
c)

A jet of water of diameter 10 cm10\text{ cm} strikes a flat plate normally with a velocity of 15 m/s15\text{ m/s}. The plate is moving with a velocity of 6 m/s6\text{ m/s} in the direction of jet and away from the jet. Find— (i) force exerted by jet on the plate; (ii) work done by jet on the plate per second.

[5 Marks]
Q3

Answer the following:

a)

Describe briefly the function of various components of Pelton turbine with neat sketches.

[5 Marks]
b)

A Pelton wheel has mean bucket speed of 10 m/s10\text{ m/s} with a jet of water flowing at the rate of 700 l/s700\text{ l/s} under a head of 30 m30\text{ m}. The buckets deflect the jet through an angle of 160160^\circ. Calculate the power given by water to the runner and hydraulic efficiency of the turbine. Assume coefficient of velocity as 0.980.98.

[9 Marks]
Q4

Answer the following:

a)

How is hydraulic turbine classified?

[5 Marks]
b)

A Francis turbine with an overall efficiency of 75%75\% is required to produce 148.25 kW148.25\text{ kW} power. It is working under a head of 7.62 m7.62\text{ m}. The peripheral velocity is 0.262gH0.26\sqrt{2gH} and radial velocity of flow at inlet is 0.962gH0.96\sqrt{2gH}. The wheel runs at 150 r.p.m.150\text{ r.p.m.} and the hydraulic losses in the turbine are 22%22\% of the available energy. Assuming radial discharge, determine— (i) guide blade angle; (ii) the wheel vane angle at inlet; (iii) diameter of wheel at inlet; (iv) width of wheel at inlet.

[9 Marks]
Q5

Answer the following:

a)

Define the term 'unit power'. Also derive the expression for this term.

[5 Marks]
b)

A turbine is to operate under a head of 25 m25\text{ m} at 200 r.p.m.200\text{ r.p.m.} The discharge is 9 m3/sec9\text{ m}^3\text{/sec}. If the efficiency is 90%90\%, determine the performance of the turbine under a head of 20 m20\text{ m}.

[9 Marks]
Q6

Answer the following:

a)

Describe the working of a single-acting reciprocating pump with neat sketch.

[5 Marks]
b)

A single-acting reciprocating pump, running at 50 r.p.m.50\text{ r.p.m.}, delivers 0.01 m3/s0.01\text{ m}^3\text{/s} of water. The diameter of piston is 200 mm200\text{ mm} and stroke length is 400 mm400\text{ mm}. Determine— (i) theoretical discharge; (ii) coefficient of discharge; (iii) slip and the percentage slip of the pump.

[9 Marks]
Q7

Answer the following:

a)

Describe multistage centrifugal pump with (i) impellers in parallel and (ii) impellers in series.

[5 Marks]
b)

A centrifugal pump having outer diameter equal to two times the inner diameter and running at 1000 r.p.m.1000\text{ r.p.m.}, works against a total head of 40 m40\text{ m}. The velocity of flow through the impeller is constant and equal to 2.5 m/s2.5\text{ m/s}. The vanes are set back at angle of 4040^\circ at outlet if the outer diameter of the impeller is 500 mm500\text{ mm} and width at outlet is 50 mm50\text{ mm}. Determine— (i) vane angle at inlet; (ii) work done by impeller on water per second; (iii) manometric efficiency.

[9 Marks]
Q8

Answer the following:

a)

Describe the working of a single-stage reciprocating air compressor.

[5 Marks]
b)

Estimate the work done by a two-stage reciprocating single-acting air compressor to compress 2.8 m32.8\text{ m}^3 of air per min at 1.05 bar1.05\text{ bar} and 10C10^\circ\text{C} to a final pressure of 35 bar35\text{ bar}. The intermediate receiver cools the air to 30C30^\circ\text{C} and 5.6 barpressure5.6\text{ bar} pressure. For air, take n=1.4n = 1.4.

[9 Marks]
Q9

Write short notes on the following :

a)

Governing of water turbine

b)

Indicator diagram

[14 Marks]

2014 021510

B.Tech Examination, 2014

Time 3 hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.

Questions

Q1

Write on the following in short, preferably one or two sentences each (any seven) :

a)

Suction head

b)

Delivery head

c)

Static head

d)

Priming

e)

Multistage pump

f)

Stay ring

g)

Mechanical efficiency

h)

Fluid

i)

Power required to drive pump

j)

Manometric efficiency

[14 Marks]
Q2

Answer the following:

a)

Explain the function of Francis turbine.

[5 Marks]
b)

A Francis turbine works under a head of 260 m260\text{ m} and develops 21900 MHP21900\text{ MHP} at a speed of 600 r.p.m.600\text{ r.p.m.} The volume flow rate through the machine is 7000 l/s7000\text{ l/s}. If the outside wheel diameter is 1.5 m1.5\text{ m} and the axial wheel width at the inlet is 135 mm135\text{ mm}, find the overall efficiency of the turbine, its hydraulic efficiency, ($\eta_h$), and the inlet angles of the guide blades and the rotor blades. Assume a volumetric efficiency of 0.980.98 and the velocity at the draft tube exit to be 17.7 m/s17.7\text{ m/s}. The whirl velocity component at the wheel exit is zero.

[9 Marks]
Q3

Answer the following:

a)

Differentiate between inward-flow and outward-flow reaction turbines.

[5 Marks]
b)

The total resistance offered to the motion of a jet-propelled boat is 500 kg500\text{ kg}. The boat is moving with a velocity of 6 m/s6\text{ m/s} and draws water amid ship. The water is discharged through two jets provided at the back of the ship. The diameter of each jet is 150 mm150\text{ mm}. Determine the efficiency of jet propulsion.

[9 Marks]
Q4

Answer the following:

a)

Obtain an expression for unit speed, unit discharge and unit power for a turbine.

[5 Marks]
b)

An inward-flow reaction turbine having an overall efficiency of 80%80\% is required to deliver 136 kW136\text{ kW}. The head (H$) is $16\text{ m} and the peripheral velocity is 3.3(H)0.53.3 \cdot (H)^{0.5}. The radial velocity of flow at inlet is 1.1(H)0.51.1 \cdot (H)^{0.5}. The runner rotates at 120 r.p.m.120\text{ r.p.m.} The hydraulic losses in the turbine are 15%15\% of the available energy. Determine (i) the diameter of the runner, (ii) the guide vane angle, and (iii) the runner blade angle at inlet and through the turbine. Assume the discharge from the runner is radial.

[9 Marks]
Q5

Answer the following:

a)

Explain the purposes of providing (i) scroll casing, (ii) stay vanes, and (iii) guide vanes for a reaction turbine.

[4 Marks]
b)

Dimensions of a centrifugal pump impeller are given below :

Parameter Inlet section Outlet section
Radius, r (mm)r\text{ (mm)} 200200 600600
Blade width, b (mm)b\text{ (mm)} 6060 4040
Blade angle, β (deg)\beta\text{ (deg)} 5050 7070

The pump handles water and is driven at 850 r.p.m.850\text{ r.p.m.} Calculate the theoretical head and mechanical power input if the flow rate is 0.5 m3/second0.5\text{ m}^3\text{/second}.

[10 Marks]
Q6

Answer the following:

a)

What is cavitation? Why and how can it be avoided? Where does it occur? Also explain net positive suction head (NPSH). Explain, in detail, in the context of a pump.

[5 Marks]
b)

A Francis turbine with an overall efficiency of 75%75\% is required to produce 149.26 kW149.26\text{ kW}. It is working under a head of 7.62 m7.62\text{ m}. The peripheral velocity is 0.262gh0.26\sqrt{2gh} and the radial velocity of flow at inlet is 0.962gh0.96\sqrt{2gh}. The wheel runs at 150 r.p.m.150\text{ r.p.m.} and the hydraulic losses in the turbine are 22%22\% of the available energy. Assuming radial discharge, determine the guide blade angle, the wheel vane angle at inlet, diameter of the wheel at inlet, and width of the wheel at inlet.

[9 Marks]
Q7

Answer the following:

a)

Derive an expression for the starting speed of the centrifugal pump.

[6 Marks]
b)

A centrifugal pump lifts water against a static head of 35 m35\text{ m} of which 4 m4\text{ m} is suction. The suction and delivery pipes are both 15 cm15\text{ cm} in diameter. The head loss in the suction pipe is 2 m2\text{ m} and in the delivery pipe is 7.0 m7.0\text{ m}. The impeller is 40 cm40\text{ cm} in diameter and 2.5 cm2.5\text{ cm} wide and runs at 1150 r.p.m.1150\text{ r.p.m.} The blade angle at exit is 3030^\circ. If the manometric efficiency is 80%80\% and mechanical efficiency is 70%70\%, determine the power required to drive the pump and discharge.

[8 Marks]
Q8

A centrifugal compressor is desired to have a total pressure ratio of 44. The inlet eye of the compressor impeller is 30 cm30\text{ cm} in diameter. The axial velocity at inlet is 120 m/s120\text{ m/s} and the mass flow is 10 kg/s10\text{ kg/s}. The velocity in the delivery duct is 115 m/s115\text{ m/s}. The tip speed of the impeller is 450 m/s450\text{ m/s} and runs at 15000 r.p.m.15000\text{ r.p.m.} with total head isentropic efficiency of 78%78\% and pressure coefficient 0.720.72. The ambient conditions are 1.013 bar1.013\text{ bar} and 15C15^\circ\text{C}. Calculate— (a) static pressure ratio; (b) static pressure and temperature at outlet of the compressor; (c) work of the compressor per kg of air; (d) theoretical power required to drive the compressor.

[14 Marks]
Q9

Write short notes on any two of the following :

a)

Draft tube

b)

Turbine

c)

Specific speed

d)

Centrifugal pump

[14 Marks]

2013 021510

B. Tech 5th Semester Examination, 2013

Time 03 Hours
Full Marks 70
Instructions:
  • The marks are indicated in the right-hand margin.
  • There are NINE questions in this paper.
  • Attempt FIVE questions in all.
  • Question No. 1 is compulsory.
  • Assume any suitable data, if required.

Q.1 Define the following in short, preferably one or two sentences each (any seven) :

Q1.a

Fluid

Q1.b

Guide vanes

Q1.c

Draft tube

Q1.d

Turbo means

Q1.e

Hydraulic turbine

Q1.f

Stay ring

Q1.g

Mechanical efficiency

Q1.h

Specific speed

Q1.i

Centrifugal pump

Q1.j

Manometric head

Q.2 Solve both questions :

Q2.a

Explain the classification of fluid machineries.

[5 Marks]
Q2.b

Establish the ratio of forces exerted by a water jet when it is made to strike— (i) a stationary flat plate held normal to it; (ii) a flat plate moving in the direction of jet at one-third the velocity of jet; (iii) a series of flat plates mounted on a wheel and moving at one-third the velocity of jet.

[9 Marks]

Q.3 Solve both questions :

Q3.a

Briefly explain the different types of turbine and write the advantages of each.

[5 Marks]
Q3.b

A 40 m/s40\text{ m/s} velocity jet of water strikes without shock a series of vanes moving at 10 m/s10\text{ m/s}. The jet is inclined at an angle of 2020^\circ to the direction of motion of vanes. The relative velocity of jet at outlet is 0.9 times of the value at inlet and the absolute velocity of water at exit is to be normal to the motion of vanes. Determine (i) the vane angles at entrance and exit, (ii) the work done on vanes per second per N of water supplied by the jet and (iii) the hydraulic efficiency.

[9 Marks]

Q.4 Solve both questions :

Q4.a

Show that the efficiency of a Pelton wheel will be maximum when the velocity of the wheel is half the velocity of the jet of water at inlet.

[5 Marks]
Q4.b

An inward flow reaction turbine having an overall efficiency of 80% is required to deliver 136 kW136\text{ kW}. The head HH is 16 m16\text{ m} and the peripheral velocity is 3.3(H)0.53.3(H)^{0.5}. The radial velocity of flow at inlet is 1.1(H)0.51.1(H)^{0.5}. The runner rotates at 120 r.p.m.120\text{ r.p.m.} The hydraulic losses in the turbine are 15% of the available energy. Determine (i) the diameter of the runner, (ii) the guide vane angle, (iii) the runner blade angle at inlet and through the turbine. Assume the discharge from the runner is radial.

[9 Marks]

Q.5 Solve both questions :

Q5.a

Explain the purpose of providing (i) scroll casing, (ii) stay vanes and (iii) guide vanes for a reaction turbine.

[4 Marks]
Q5.b

A Pelton wheel has to develop 13230 kW13230\text{ kW} under a net head of 800 m800\text{ m} while running at a speed of 600 r.p.m.600\text{ r.p.m.} If the coefficient of the jet Cv=0.97C_v = 0.97, speed ratio ϕ=0.46\phi = 0.46 and the ratio of the jet diameter is 116\frac{1}{16} of the wheel diameter, calculate the number of jets required for the Pelton wheel. Also calculate (i) the diameter of jet, (ii) the diameter of pitch circle and (iii) the quantity of water supplied to the wheel.

[10 Marks]

Q.6 Solve both questions :

Q6.a

Differentiate between centrifugal and reciprocating pump.

[4 Marks]
Q6.b

A centrifugal pump having an impeller 30 cm30\text{ cm} outside diameter rotates at 1050 r.p.m.1050\text{ r.p.m.} The vanes are radial at exit and 7.5 cm7.5\text{ cm} wide. The velocity of radial flow through the impeller is 3 m/s3\text{ m/s}. The velocities in the suction and delivery pipes are 2.5 m/s2.5\text{ m/s} and 1.5 m/s1.5\text{ m/s} respectively. Neglecting frictional losses, determine the height through which the pump lifts, and the horsepower of the pump. Assume radial entry.

[10 Marks]

Q.7 Solve both questions :

Q7.a

Explain the different efficiencies used in centrifugal pump.

[6 Marks]
Q7.b

A centrifugal pump lifts water against a static head of 40 m40\text{ m} of which 4 m4\text{ m} is suction. The suction and delivery pipes are both 15 cm15\text{ cm} in diameter. The head loss in the suction pipe is 2 m2\text{ m} and in the delivery pipe 7.5 m7.5\text{ m}. The impeller is 40 cm40\text{ cm} in diameter, 2.5 cm2.5\text{ cm} wide and runs at 1250 r.p.m.1250\text{ r.p.m.} The blade angle at exit is 3030^\circ. If the manometric efficiency is 80% and mechanical efficiency 70%, determine the power required to drive the pump and discharge.

[8 Marks]

Q.8 Solve the following question :

Q8

A centrifugal compressor is desired to have a total pressure ratio of 4. The inlet eye of the compressor impeller is 30 cm30\text{ cm} in diameter. The axial velocity at inlet is 130 m/s130\text{ m/s} and the mass flow is 10 kg/s10\text{ kg/s}. The velocity in the delivery duct is 115 m/s115\text{ m/s}. The tip speed of the impeller is 450 m/s450\text{ m/s} and runs at 16000 r.p.m.16000\text{ r.p.m.} with total head isentropic efficiency of 78% and pressure coefficient 0.72. The ambient conditions are 1.013 bar1.013\text{ bar} and 15C15^\circ\text{C}. Calculate— (a) the static pressure ratio; (b) the static pressure and temperature at outlet of compressor; (c) the work of compressor per kg of air; (d) the theoretical power required to drive compressor.

Q.9 Write short notes on any two of the following :

Q9.a

Relief valve

Q9.b

Electrohydraulic governor

Q9.c

Priming of a pump


0 102308

B.Tech Examination, 0

Time 3 hours
Full Marks 70
Instructions:
  • All questions carry equal marks.
  • There are TEN questions in this paper.
  • Attempt any FIVE questions.

Questions

Q1

Write a note on the application of the moment of momentum equation to flow through hydraulic machinery. Also explain Euler's fundamental equation.

Q2

The following data is given for a Francis turbine: Net head = 70 m Speed = 600 r.p.m. Shaft power = 367.875 kW $\eta_o = 85%$ $\eta_h = 95%$ Flow ratio = 0.25 Breadth ratio = 0.1 Outer diameter of the runner = 2 x inner diameter of the runner The thickness of vanes occupy 10% of the circumferential area of the runner Velocity of flow is constant at inlet and outlet and discharge is radial at outlet Determine— (a) guide blade angle; (b) runner vane angles at inlet and outlet; (c) diameter of runner at inlet and outlet; (d) width of wheel at inlet.

Q3

A Kaplan turbine working under a head of 30 m develops 1290 kW SP. If the— speed ratio = 2.1 flow ratio = 0.62 diameter of boss = 0.34 times the diameter of the runner overall efficiency of the turbine = 89% find the diameter of the runner and the speed of the turbine.

Q4

A Pelton wheel is revolving at a speed of 200 r.p.m. and develops 5886 kW SP when working under a head of 200 m with an overall efficiency of 80%. Determine unit speed, unit discharge and unit power. The speed ratio of the turbine is given as 0.48. Find the speed, discharge and power when this turbine is working under a head of 150 m.

Q5

Write a note on performance characteristics and testing of models and selection of water turbines.

Q6

Write a note on surging, choking and stalling in rotary compressors.

Q7

The diameter of an impeller of a centrifugal pump at inlet and outlet are 300 mm and 600 mm respectively. The velocity of flow at outlet is 2.5 m/s and vanes are set back at an angle of 4545^\circ at outlet. Determine the minimum starting speed of the pump if the manometric efficiency is 80%.

Q8

A centrifugal pump is running at 1000 r.p.m. The outlet vane angle of the impeller is 3030^\circ and velocity of flow at outlet is 3 m/s. The pump is working against a total head of 30 m and the discharge through the pump is 0.3 m3/s0.3\text{ m}^3\text{/s}. If the manometric efficiency of the pump is 75%, determine the— (a) diameter of the impeller; (b) width of the impeller at outlet.

Q9

A double acting reciprocating pump, running at 50 r.p.m. is discharging 900 litres of water per minute. The pump has stroke of 400 mm. The diameter of piston is 250 mm. The delivery and suction heads are 25 m and 4 m respectively. Find the slip of the pump and power required to drive the pump.

Q10

Write a note on the theory of hydraulic couplings and torque converters, operating characteristics and common uses.


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