HYDRAULIC MACHINES - Mechanical Engineering Multiple choice Questions Answers

HYDRAULIC MACHINES

Mechanical Engineering Multiple choice Questions Answers


“HYDRAULIC MACHINES”

Mechanical Engineering MCQS

HYDRAULIC MACHINES Questions Answers


  1. Reciprocating pumps are no more to be seen in industrial applications (in comparison to centrifugal pumps) because of
    (a) high initial and maintenance cost
    (b) lower discharge
    (c) lower speed of operation
    (d) necessity of air vessel
    (e) all of the above.
    Ans: a
  2. In a centrifugal pump casing, the flow of water leaving the impeller, is
    (a) rectilinear flow
    (b) radial flow
    (c) free vortex motion
    (d) forced vortex
    (e) none of the above.
    Ans: c
  3. Head developed by a centrifugal pump depends on
    (a) impeller diameter
    (b) speed
    (c) fluid density
    (d) type of casing
    (e) (a) and (b) above.
    Ans: e
  4. For starting an axial flow pump, its delivery valve should be
    (a) closed
    (b) open
    (c) depends on starting condition and flow desired
    (d) could be either open or closed
    (e) partly open and partly closed.
    Ans: b
  5. The efficiency of a centrifugal pump is maximum when its blades are
    (a) straight
    (b) bent forward
    (c) bent backward
    (d) bent forward first and then backward
    (e) bent backward first and then forward.
    Ans: c
  6. In a centrifugal pump casing, the flow of water leaving the
    (a) radial
    (b) radial
    (c) centrifugal
    (d) rectilinear
    (e) vortex.
    Ans: e
  7. Centrifugal pump is started with its delivery valve
    (a) kept fully closed
    (b) kept fully open
    (c) irrespective of any position
    (d) kept 50% open
    (e) none of the above.
    Ans: a
  8. Axial flow pump is started with its delivery valve
    (a) kept fully closed
    (b) kept fully open
    (c) irrespective of any position
    (d) kept 50% open
    (e) none of the above.
    Ans: b
  9. When a piping system is made up primarily of vertical lift and very little pipe friction, the pump characteristics should be
    (a) horizontal
    (b) nearly horizontal
    (c) steep
    (d) first rise and then fall
    (e) none of the above.
    Ans: c
  10. One horsepower is equal to
    (a) 102 watts
    (b) 75 watts
    (c) 550 watts
    (d) 735 watts
    (e) 33000 watts.
    Ans: d
  11. Multistage centrifugal pumps are used to obtain
    (a) high discharge
    (b) high head
    (c) pumping of viscous fluids
    (d) high head and high discharge
    (e) high efficiency.
    Ans: b
  12. When a piping system is made up primarily of friction head and very little of vertical lift, then pump characteristics should be
    (a) horizontal
    (b) nearly horizontal
    (c) steep
    (d) first rise and then fall
    (e) none of the above.
    Ans: b
  13. In a single casing, multistage pump running at constant speed, the capacity rating is to be slightly lowered. It can be done by
    (a) designing new impeller
    (b) trimming the impeller size to the required size by machining
    (c) not possible
    (d) some other alterations in the impeller
    (e) none of the above.
    Ans: b
  14. If a pump is handling water and is discharging a certain flow Q at a constant total dynamic head requiring a definite B.H.P., the same pump when handling a liquid of specific gravity 0.75 and viscosity nearly same as of water would discharge
    (a) same quantity of liquid
    (b) 0.75 Q
    (c) Q/0.75
    (d) 1.5 Q
    (e) none of the above.
    Ans: a
  15. The horse power required in above case will be
    (a) same
    (b) 0.75 B.H.P.
    (c) B.H.P./0.75
    (d) 1.5 B.H.P.
    (e) none of the above.
    Ans: b
  16. Low specific speed of a pump implies it is
    (a) centrifugal pump
    (b) mixed flow pump
    (c) axial flow pump
    (d) any one of the above
    (e) none of the above.
    Ans: a
  17. The optimum value of vane exit angle for a centrifugal pump impeller is
    (a) 10-15°
    (b) 20-25°
    (c) 30-40°
    (d) 50-60°
    (e) 80-90°.
    Ans: b
  18. In a centrifugal pump, the liquid enters the pump
    (a) at the top
    (b) at the bottom
    (c) at the center
    (d) from sides
    (e) none of the above.
    Ans: c
  19. For small discharge at high pressure, following pump is preferred
    (a) centrifugal
    (b) axial flow
    (c) mixed flow
    (d) propeller
    (e) reciprocating.
    Ans: e
  20. In centrifugal pumps, maximum efficiency is obtained when the blades are
    (a) straight
    (b) bent forward
    (c) bent backward
    (d) radial
    (e) given aerofoil section.
    Ans: c
  21. Motion of a liquid in a volute casing of a centrifugal pump is an example of
    (a) rotational flow
    (b) radial
    (c) forced spiral vortex flow
    (d) forced cylindrical vortex flow
    (e) spiral vortex flow.
    Ans: e
  22. For very high discharge at low pressure such as for flood control and irrigation applications, following type of pump is preferred
    (a) centrifugal
    (b) axial flow
    (c) reciprocating
    (d) mixed flow
    (e) none of the above.
    Ans: b
  23. Medium specific speed of a pump implies it is
    (a) centrifugal pump
    (b) mixed flow pump
    (c) axial flow pump
    (d) any one of the above
    (e) none of the above.
    Ans: b
  24. High specific speed of a pump implies it is
    (a) centrifugal pump
    (b) mixed flow pump
    (c) axial flow pump
    (d) any one of the above
    (e) none of the above.
    Ans: c
  25. Indicator diagram of a reciprocating pump is a graph between
    (a) flow vs swept volume
    (b) pressure in cylinder vs swept volume
    (c) flow vs speed
    (d) pressure vs speed
    (e) swept volume vs speed.
    Ans: b
  26. Low specific speed of turbine implies it is
    (a) propeller turbine
    (b) Francis turbine
    (c) impulse turbine
    (d) any one of the above
    (e) none of the above.
    Ans: c
  27. Any change in load is adjusted by adjusting following parameter on turbine
    (a) net head
    (b) absolute velocity
    (c) blade velocity
    (d) flow
    (e) relative velocity of flow at inlet.
    Ans: d
  28. Runaway speed of a hydraulic turbine is
    (a) full load speed
    (b) the speed at which turbine runner will be damaged
    (c) the speed if the turbine runner is allowed to revolve freely without load and with the wicket gates wide open
    (d) the speed corresponding to maximum overload permissible
    (e) none of the above.
    Ans: c
  29. The maximum number of jets generally employed in impulse turbine without jet interference is
    (a) 4
    (b) 6
    (c) 8
    (d) 12
    (e) 16.
    Ans: b
  30. Medium specific speea of turbine implies it is
    (a) propeller turbine
    (b) Francis turbine
    (c) impulse turbine
    (d) any one of the above
    (e) none of the above.
    Ans: b
Hydraulic Machines Interview Questions and Answers pdf :-
  1. High specific speed of turbine implies it is
    (a) propeller turbine
    (b) Francis turbine
    (c) impulse turbine
    (d) any one of the above
    (e) none of the above.
    Ans: a
  2. The specific speed of turbine is defined as the speed of a unit
    (a) of such a size that it delivers unit dis-charge at unit head
    (b) of such a size that it delivers unit dis-charge at unit power
    (c) of such a size that it requires unit power per unit head
    (d) of such a size that it produces unit horse power with unit head
    (e) none of the above.
    Ans: d
  3. Puck up the wrong statement about centrifugal pump
    (a) discharge a diameter
    (b) head a speed2
    (c) head a diameter
    (d) Power a speed3
    (e) none of the above is wrong.
    Ans: a
  4. A turbine pump is basically a centrifugal pump equipped additionally with
    (a) adjustable blades
    (b) backward curved blades
    (c) vaned diffusion casing
    (d) inlet guide blades
    (e) totally submerged operation facility.
    Ans: c
  5. Casting of a centrifugal pump is designed so as to minimize
    (a) friction loss
    (b) cavitation
    (c) static head
    (d) loss of kinetic energy
    (e) starting time.
    Ans: d
  6. In reaction turbine, draft tube is used
    (a) to transport water downstream without eddies
    (b) to convert the kinetic energy to flow energy by a gradual expansion of the flow cross-section
    (c) for safety of turbine
    (d) to increase flow rate
    (e) none of the above.
    Ans: b
  7. Guide angle as per the aerofoil theory of Kaplan turbine blade design is defined as the angle between
    (a) lift and resultant force
    (b) drag and resultant force
    (c) lift and tangential force
    (d) lift and drag
    (e) resultant force and tangential force.
    Ans: a
  8. Francis turbine is best suited for
    (a) medium head application from 24 to 180 m
    (b) low head installation up to 30 m
    (c) high head installation above 180 m
    (d) all types of heads
    (e) none of the above.
    Ans: a
  9. The flow rate in gear pump
    (a) increases with increase in pressure
    (b) decreases with increase in pressure
    (c) more or less remains constant with in-crease in pressure
    (d) unpredictable
    (e) none of the above.
    Ans: c
  10. Impulse turbine is generally fitted
    (a) at the level of tail race
    (b) little above the tail race
    (c) slightly below the tail race
    (d) about 2.5 m above the tail race to avoid cavitation
    (e) about 2.5 m below the tail race to avoid cavitation.
    Ans: b
  11. Francis, Kaplan and propeller turbines fall under the category of
    (a) Impulse turbines
    (b) Reaction turbines
    (c) Axial flow turbines
    (d) Mixed flow turbines
    (e) Reaction-cum-impulse turbines.
    Ans: b
  12. Reaction turbines are used for
    (a) low head
    (b) high head
    (c) high head and low discharge
    (d) high head and high discharge
    (e) low head and high discharge.
    Ans: e
  13. The discharge through a reaction turbine with increase in unit speed
    (a) increases
    (b) decreases
    (c) remains unaffected
    (d) first increases and then decreases
    (e) first decreases and then increases.
    Ans: b
  14. The angle of taper on draft tube is
    (a) greater than 15°
    (b) greater than 8°
    (c) greater than 5°
    (d) less than 8°
    (e) less than 3°.
    Ans: d
  15. Specific speed for reaction turbines ranges from
    (a) 0 to 4.5
    (b) 10 to 100
    (c) 80 to 200
    (d) 250 to 300
    (e) none of the above.
    Ans: b
  16. In axial flow fans and turbines, fluid enters and leaves as follows
    (a) radially, axially
    (b) axially, radially
    (c) axially, axially
    (d) radially, radially
    (e) combination of axial and radial.
    Ans: c
  17. Which place in hydraulic turbine is most susceptible for cavitation
    (a) inlet of draft rube
    (b) blade inlet
    (c) guide blade
    (d) penstock
    (e) draft tube exit.
    Ans: a
  18. Air vessels in reciprocating pump are used to
    (a) smoothen flow
    (b) reduce acceleration to minimum
    (c) increase pump efficiency
    (d) save pump from cavitation
    (e) increase pump head.
    Ans: b
  19. Saving of work done and power by fitting an air vessel to single acting reciprocating pump is of the order of
    (a) 39.2%
    (b) 49.2%
    (c) 68.8%
    (d) 84.8%
    (e) 91.6%.
    Ans: d
  20. Saving of work done and power by fitting an air vessel to double acting reciprocating pump is of the order of
    (a) 39.2%
    (b) 49.2%
    (c) 68.8%
    (d) 84.8%
    (e) 91.6%.
    Ans: a
  21. According to fan laws, for fans having constant wheel diameter, the air or gas capacity varies
    (a) directly as fan speed
    (b) square of fan speed
    (c) cube of fan speed
    (d) square root of fan speed
    (e) none of the above.
    Ans: a
  22. According to fan laws, for fans having constant wheel diameter, the pressure varies
    (a) directly as fan speed
    (b) square of fan speed
    (c) cube of fan speed
    (d) square root of fan speed
    (e) none of the above.
    Ans: b
  23. According to fan laws, for the fans having constant wheel diameters, the power demand varies
    (a) directly as fan speed
    (b) square of fan speed
    (c) cube of fan speed
    (d) square root of fan speed
    (e) none of the above.
    Ans: c
  24. According to fan laws, at constant speed and capacity, the pressure and power vary
    (a) directly as the air or gas density
    (b) inversely as square root of density
    (c) inversely as density
    (d) as square of density
    (e) as square root of density.
    Ans: a
  25. According to fan laws, at constant pressure, the speed capacity and power vary
    (a) directly as the air or gas density
    (b) inversely as square root of density
    (c) inversely as density
    (d) as square of density
    (e) as square root of density.
    Ans: b
  26. According to fan laws, at constant weight of air or gas, the speed, capacity and pressure vary
    (a) directly as the air or gas density
    (b) inversely as square root of density
    (c) inversely as density
    (d) as square of density
    (e) as square root of density.
    Ans: c
  27. Pressure intensifier increases the pressure in proportion to
    (a) ratio of diameters
    (b) square of ratio of diameters
    (c) inverse ratio of diameters
    (d) square of inverse ratio of diameters
    (e) fourth power of ratio of diameters.
    Ans: b
  28. A hydraulic accumulator normally consists of
    (a) two cylinders, two rams and a storage device
    (b) a cylinder and a ram
    (c) two co-axial rams and two cylinders
    (d) a cylinder, a piston, storage tank and control valve
    (e) special type of pump with storage device and a pressure regulator.
    Ans: b
  29. A hydraulic intensifier normally consists of
    (a) two cylinders, two rams and a storage device
    (b) a cylinder and a ram
    (c) two co-axial rams and two cylinders
    (d) a cylinder, a piston, storage tank and control valve
    (e) special type of pump with storage device and a pressure regulator.
    Ans: c
  30. Hydraulic accumulator is used for
    (a) accumulating oil
    (b) supplying large quantities of oil for very short duration
    (c) generally high pressures to operate hydraulic machines
    (d) supplying energy when main supply fails
    (e) accumulating hydraulic energy.
    Ans: d
  31. Maximum impulse will be developed in hydraulic ram when
    (a) waste valve closes suddenly
    (b) supply pipe is long
    (c) supply pipe is short
    (d) ram chamber is large
    (e) supply pipe has critical diameter,
    Ans: a
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Open Channel Flow LAB REPORT



Aim
TO study the open channel flow in a rectangular perspex channel

Objectives
1. Investigate the uniform flow condition in open channel flow
2. Verify the manning’s equation


Theory
According to Dr. Khalil M. ALASTAL (n.d) an open channel is like a duck with flowing fluid and whose surface is exposed to atmosphere. As the atmospheric pressure remains constant through the length of duct so the fluid flows only due to the difference in potential energy.

According to Ivan Gramatikov (n.d) flow rate of water in a channel is the product of its area with the velocity of water through that area Q=A×V. Where A is area of cross section and V is velocity of the fluid. Volumetric flow rate is the ratio of volume of flowing fluid to the time takenQ=∆V/t. Area of the rectangular channel is the product of its width with the depth of the water flowing through that areaA=b ×y_o. Where b is the width of the rectangular channel and y_o is the depth of the flow.

According to David Knighton Wetted perimeter is the perimeter used for the wet cross section area. In an open channel flow it can be define as the sum of the sides of channels those are in direct contact with the flowing fluid. With the increase in wetted perimeter the friction losses increase resulting in the decrease in heat.

P=b+yo+yo

P=b+2 ×yo  

According to Bernard Le Méhauté channel flow efficiency of an open channel flow in measured in the term of hydraulic radius some time also called hydraulic mean depth. It is ratio of the channel cross section area to the wetted perimeter. Hydraulic radius is the function of shape of the channel not the half of the hydraulic diameter. 
R=A/P

According to Manning R. (1891) manning equation is used to find the theoretical flow rate of the fluid flowing under the action of gravity also called the open channel. 

Q=  A/n  × R^(2/3)  × So^(1/2)

Here So is the slope of the bed of the channel which enable the water to flow under the action of gravity. 

Procedure
Following is the procedure to perform the experiment according to Dr. Khalil M. ALASTAL (n.d)

1. Set up the flow channel apparatus

2. Adjust the support frame feet so that the flow channel does not rock

3. Reset the clock dial to zero 

4. Check the water depth along the length of channel, it should be constant to prove that the initial slope of bed is zero

5. With the help of a jack at the back of channel, set the slope of the channel to a gradient of 1/500 that is 0.002

6. Start the pump and introduce water into the channel by operating valves

7. Use the flow control valve to set the flow rate of water at 2.5 liter/sec 

8. Allow the flow in the channel to settle and then take the measurement of depth of water with the help of scales placed at their respective position

9. Note that the space between the scales should not be greater than 2 mm

10. Now adjust the flow control valve three times to set the flow rate to three different values of 2.0, 1.5 and 1.0 liter/sec and note the depth of water for all three flow rates.

11. Repeat the complete above procedure for the slope of gradient 0.005 and note the values in the below given tables

12. Calculate the value for Area, Wetted perimeter, Hydraulic Radius and Theoretical Flow rate.

13. Also convert the measured flow rate from liter per second to cubic meter per second

Observations
Numbers of experiments were performed according to above mention procedure, with different flow rates and with different slopes and data was recorded in the following table.

Table 1 Observation for So = 1/200
So
y1 mm
y2  mm
volume liter
Time sec
1/200
42.5
42
20
9.93
1/200
42.8
41.8
20
9.1
1/200
42.8
40.8
20
9.57
1/200
44.1
43.2
20
9.4


Table 2 Observation for So = 1/500
So
y1 mm
y2  mm
volume liter
Time sec
1/500
55.6
54.2
20
10.85
1/500
55.5
54.3
20
9.5
1/500
54.9
54
20
9.48
1/500
54.4
53.8
20
9.8


Analysis

Using the data gathered as the result of experiment performed, to get the values of mean depth, Area, wetted perimeter, hydraulic radius and theoretical flow rate with the help of formulas mention above.  

Table 3 Calculation for So = 0.005
QM  /sec
yo    (m)
A ()
P (m)
R   (m)
So
QT /sec
0.0025
0.04225
0.003211
0.1605
0.020006
0.005
0.001859201
0.002
0.0423
0.003215
0.1606
0.020017
0.005
0.001862096
0.0015
0.0418
0.003177
0.1596
0.019905
0.005
0.001833174
0.001
0.04365
0.003317
0.1633
0.020315
0.005
0.001940505

Table 4 Calculation for So = 0.0.002
QM  /sec
yo   (m)
A ()
P (m)
R  (m)
So
QT  /sec
0.0025
0.0549
0.004172
0.1858
0.022456
0.002
0.001650258
0.002
0.0549
0.004172
0.1858
0.022456
0.002
0.001650258
0.0015
0.05445
0.004138
0.1849
0.022381
0.002
0.001633053
0.001
0.0541
0.004112
0.1842
0.022321
0.002
0.001619686


Conclusion

Values for the measure flow rate were recorded using flow meter and value of theoretical flow rate was calculated by using manning equation. Difference between the values of these two flow rates is because the theoretical flow rate depends on the slope of the channel bed and also on the other factory like manning roughness coefficient but the measure flow rate depends only on the area and velocity of the fluid through that area.

Applying the same flow rate at different slopes has shown that the change in the slope of bed change the theoretical flow rate value as it depends on the depth of the flow. Value of theoretical flow rate at 0.002 gradient is less than the value at the 0.005 gradient, this show that increasing the gradient increase the theoretical flow rate while the measured flow rate remain the same. 

HYDRAULIC MACHINES - Mechanical Engineering Multiple choice Questions Answers

HYDRAULIC MACHINES


Mechanical Engineering Multiple choice Questions Answers


hydraulic machine objective questions, hydraulic machines objective questions pdf,  hydraulic machine mcq, hydraulic machines mcq

“HYDRAULIC MACHINES”


Mechanical Engineering MCQS


from FreePDfbook.com



HYDRAULIC MACHINES Questions Answers



  1. Reciprocating pumps are no more to be seen in industrial applications (in comparison to centrifugal pumps) because of
    (a) high initial and maintenance cost
    (b) lower discharge
    (c) lower speed of operation
    (d) necessity of air vessel
    (e) all of the above.
    Ans: a

  2. In a centrifugal pump casing, the flow of water leaving the impeller, is
    (a) rectilinear flow
    (b) radial flow
    (c) free vortex motion
    (d) forced vortex
    (e) none of the above.
    Ans: c

  3. Head developed by a centrifugal pump depends on
    (a) impeller diameter
    (b) speed
    (c) fluid density
    (d) type of casing
    (e) (a) and (b) above.
    Ans: e

  4. For starting an axial flow pump, its delivery valve should be
    (a) closed
    (b) open
    (c) depends on starting condition and flow desired
    (d) could be either open or closed
    (e) partly open and partly closed.
    Ans: b

  5. The efficiency of a centrifugal pump is maximum when its blades are
    (a) straight
    (b) bent forward
    (c) bent backward
    (d) bent forward first and then backward
    (e) bent backward first and then forward.
    Ans: c


 

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HEAT TRANSFER - Mechanical Engineering Multiple choice Questions Answers

HEAT TRANSFER


Mechanical Engineering Multiple choice Questions Answers


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“HEAT TRANSFER”


Mechanical Engineering MCQS


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HEAT TRANSFER Questions Answers


 

1. Unit of thermal conductivity in M.K.S. units is
(a) kcal/kg m2 °C
(b) kcal-m/hr m2 °C
(c) kcal/hr m2 °C
(d) kcal-m/hr °C
(e) kcal-m/m2 °C.
Ans: b

2. Unit of thermal conductivity in S.I. units is
(a) J/m2 sec
(b) J/m °K sec
(c) W/m °K
(d) (a) and (c) above
(e) (b) and (c) above.
Ans: e

3. Thermal conductivity of solid metals with rise in temperature normally
(a) increases
(b) decreases
(c) remains constant
(d) may increase or decrease depending on temperature
(e) unpredictable.
Ans: b

4. Thermal conductivity of non-metallic amorphous solids with decrease in temperature
(a) increases
(b) decreases
(c) remains constant
(d) may increase or decrease depending on temperature
(e) unpredictable.
Ans: b

5. Heat transfer takes place as per –
(a) zeroth law of thermodynamics
(b) first law of thermodynamic
(c) second law of the thermodynamics
(d) Kirchoff’s law (e) Stefan’s law.
Ans: c

6.
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120. A grey body is one whose absorptivity
(a) varies with temperature
(b) varies with the wave length of incident ray
(c) varies with both
(d) does not vary with temperature and wave length of the incident ray
(e) there is no such criterion.
Ans: d

 

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FLUID MECHANICS - Mechanical Engineering Multiple choice Questions Answers

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FLUID MECHANICS


Mechanical Engineering Multiple choice Questions Answers


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fluid mechanics mcq pdf 



“FLUID MECHANICS”


Mechanical Engineering MCQS


from FreePDfbook.com



FLUID MECHANICS Questions Answers


1. Fluid is a substance that
(a) cannot be subjected to shear forces
(b) always expands until it fills any container
(c) has the same shear stress.at a point regardless of its motion
(d) cannot remain at rest under action of any shear force
(e) flows.
Ans: d

2. Fluid is a substance which offers no resistance to change of
(a) pressure
(b) flow
(c) shape
(d) volume
(e) temperature.
Ans: c

3. Practical fluids
(a) are viscous
(b) possess surface tension
(c) are compressible
(d) possess all the above properties
(e) possess none of the above properties.
Ans: d

4. In a static fluid
(a) resistance to shear stress is small
(b) fluid pressure is zero
(c) linear deformation is small
(d) only normal stresses can exist
(e) viscosity is nil.
Ans: d

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251. For similarity, in addition to models being geometrically similar to prototype, the following in both cases should also be equal
(a) ratio of inertial force to force due to viscosity
(b) ratio of inertial force to force due to gravitation
(c) ratio of inertial force to force due to surface tension
(d) all the four ratios of inertial force to force due to viscosity, gravitation, sur-face tension, and elasticity
Ans: d


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fluid mechanics objective questions