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Fluid Mechanics MCQ Interview Questions and Answers
1.
Poise is the unit of
surface tension
capillarity
viscosity
shear stress in fluids
buoyancy.
2.
Pascal-second is the unit of
pressure
kinematic viscosity
dynamic viscosity
surface tension
3.
An ideal fluid is
one which obeys Newton’s law of viscosity
frictionless and incompressible
very viscous
frictionless and compressible
4.
The unit of kinematic viscosity is
gm/cm-sec2
dyne-sec/cm2
gm/cm2-sec
cm2/sec
5.
If the dynamic viscosity of a fluid is 0.5 poise and specific gravity is 0.5, then the kinematic viscosity of that fluid in stokes is
0.25
0.50
1.0
none of the above
6.
The viscosity of a gas
decreases with increase in temperature
increases with increase in temperature
is independent of temperature
is independent of pressure for very high pressure intensities
7.
Newton’s law of viscosity relates
intensity of pressure and rate of angular deformation
shear stress and rate of angular deformation
shear stress, viscosity and temperature
viscosity and rate of angular deformation
8.
An open tank contains 1 m deep water with 50 cm depth of oil of specific gravity 0.8 above it. The intensity of pressure at the bottom of tank will be
4 kN/m2
10 kN/m2
12 kN/m2
14 kN/m2
9.
The position of center of pressure on a plane surface immersed vertically in a static mass of fluid is
at the centroid of the submerged area
always above the centroid of the area
always below the centroid of the area
none of the above
10.
The total pressure on a plane surface inclined at an angle 9 with the horizontal is equal to where p is pressure intensity at centroid of area and A is area of plane surface.
PA
pA sin 9
pA cos 9
pA tan 9
11.
A vertical rectangular plane surface is submerged in water such that its top and bottom surfaces are 1.5 m and 6.0 m res-pectively below the free surface. The position of center of pressure below the free surface will be at a distance of
3.75 m
4.0 m
4.2m
4.5m
12.
Centre of buoyancy always
coincides with the centre of gravity
coincides with the centroid of the volume of fluid displaced
remains above the centre of gravity
remains below the centre of gravity
13.
If the weight of a body immersed in a fluid exceeds the buoyant force, then the body will
rise until its weight equals the buoyant force
tend to move downward and it may finally sink
float
none of the above
14.
Metacentric height for small values of angle of heel is the distance between the
centre of gravity and centre of buoy-ancy
centre of gravity and metacentre
centre of buoyancy and metacentre
free surface and centre of buoyancy
15.
A floating body is said to be in a state of stable equilibrium
when its metacentric height is zero
when the metacentre is above the centre of gravity
when the metacentre is below the centre of gravity
only when its centre of gravity is below its centre of buoyancy
16.
The increase in meta centric height i) increases stability ii) decreases stability iii) increases comfort for passengers iv) decreases comfort for passengers The correct answer is
(i) and (iii)
(i)and(iv)
(ii) and (iii)
(ii) and (iv)
17.
A rectangular block 2 m long, 1 m wide and 1 m deep floats in water, the depth of immersion being 0.5 m. If water weighs 10 kN/m3, then the weight of the block is
5kN
lOkN
15 kN
20 kN
18.
The point in the immersed body through which the resultant pressure of the liquid may be taken to act is known as
meta center
center of pressure
center of buoyancy
center of gravity
none of the above.
19.
If a vessel containing liquid moves downward with a constant acceleration equal to ‘g’ then
the pressure throughout the liquid mass is atmospheric
there will be vacuum in the liquid
the pressure in the liquid mass is greater than hydrostatic pressure
none of the above
20.
When a liquid rotates at a constant angular velocity about a vertical axis as a rigid body, the pressure intensity varies
linearly with radial distance
as the square of the radial distance
inversely as the square of the radial distance
inversely as the radial distance
21.
An open cubical tank of 2 m side is filled with water. If the tank is rotated with an acceleration such that half of the water spills out, then the acceleration is equal to
g/3
g/2
2g/3
g
22.
A right circular cylinder open at the top is filled with liquid and rotated about its vertical axis at such a speed that half the liquid spills out, then the pressure intensity at the center of bottom is
zero
one-fourth its value when cylinder was full
one-half its value when cylinder was full
cannot be predicted from the given data
23.
The horizontal component of force on a curved surface is equal to the
product of pressure intensity at its centroid and area
force on a vertical projection of the curved surface
weight of liquid vertically above the curved surface
force on the horizontal projection of the curved surface
24.
A closed tank containing water is moving in a horizontal direction along a straight line at a constant speed. The tank also contains a steel ball and a bubble of air. If the tank is decelerated horizontally, then i) the ball will move to the front ii) the bubble will move to the front iii) the ball will move to the rear iv) the bubble will move to the rear Find out which of the above statements are correct ?
(i) and (ii)
(i)and(iv)
(ii) and (iii)
(iii) and (iv)
25.
The eddy viscosity for turbulent flow is
a function of temperature only
a physical property of the fluid.
dependent on the flow
independent of the flow
26.
Flow at constant rate through a tapering pipe is i) steady flow ii) uniform flow iii) unsteady flow iv) non-uniform flow The correct answer is
(i) and (ii)
(i)and(iv)
(ii) and (iii)
(ii) and (iv)
27.
In a two dimensional incompressible steady flow around an airfoil, the stream lines are 2 cm apart at a great distance from the airfoil, where the velocity is 30 m/sec. The velocity near the airfoil, where the stream lines are 1.5 cm apart, is
22.5 m/sec.
33 m/sec.
40 m/sec.
90 m/sec.
28.
When the velocity distribution is uniform over the cross-section, the correction factor for momentum is
0
1
4/3
2
29.
Least possible value of correction factor for i) kinetic energy is zero ii) kinetic energy is 1 iii) momentum is zero iv) momentum is 1 The correct statements are
(i) and (iii)
(ii) and (iii)
(i) and (iv)
(ii) and (iv)
30.
If the velocity is zero over half of the cross-sectional area and is uniform over the remaining half, then the momentum correction factor is
1
4/3
2
4
31.
If velocity is zero over l/3rd of a cross-section and is uniform over remaining 2/3rd of the cross-section, then the correction factor for kinetic energy is
4/3
3/2
9/4
27/8
32.
The continuity equation pi V,A,= p2V2A2 is based on the following assumption regarding flow of fluid where pi and p2 are mass densities.
steady flow
uniform flow
incompressible flow
frictionless flow
33.
Which of the following velocity potentials satisfies continuity equation ?
x2y
x2-y2
cosx
x2 + y2
34.
The motion of air mass in a tornado is a
free vortex motion
forced vortex motion
free vortex at center and forced vortex outside
forced vortex at center and free vortex outside
35.
In a forced vortex motion, the velocity of flow is
directly proportional to its radial distance from axis of rotation
inversely proportional to its radial distance from the axis of rotation
inversely proportional to the square of its radial distance from the axis of rotation
directly proportional to the square of its radial distance from the axis of rotation
36.
Stream lines and path lines always coincide in case of
steady flow
laminar flow
uniform flow
turbulent flow
37.
Equation of continuity is based on the principle of conservation of
mass
energy
momentum
none of the above
38.
In steady flow of a fluid, the total accele ration of any fluid particle
can be zero
is never zero
is always zero
is independent of coordinates
39.
The pitot tube is used to measure
velocity at stagnation point
stagnation pressure
static pressure
dynamic pressure
40.
Hot wire anemometer is used to measure
discharge
velocity of gas
pressure intensity of gas
pressure intensity of liquid
41.
The theoretical value of coefficient of contraction of a sharp edged orifice is
0.611
0.85
0.98
1.00
42.
Which of the following is used to measure the discharge ?
current meter
venturimeter
pitot tube
hotwire anemometer
43.
Select the incorrect statement.
The pressure intensity at vena contracta is atmospheric.
Contraction is least at vena contracta.
Stream lines are parallel throughout the jet at vena contracta.
Coefficient of contraction is always less than one.
44.
Size of a venturimeter is specified by
pipe diameter
throat diameter
angle of diverging section
both pipe diameter as well as throat diameter
45.
Due to each end contraction, the discharge of rectangular sharp crested weir is reduced by
5%
10%
15%
20%
46.
The discharge through a V- notch varies as
H1/2
H3’2
H5/2
H5’4 where H is head.
47.
Which of the following is an incorrect statement ?
Coefficient of contraction of a venturimeter is unity.
Flow nozzle is cheaper than venturimeter but has higher energy loss.
Discharge is independent of orientation of venturimeter whether it is horizontal, vertical or inclined.
None of the above statement is correct.
48.
Coefficient of velocity of venturimeter
is independent of Reynolds number
decreases with higher Reynolds number
is equal to the coefficient of discharge of venturimeter
none of the above
49.
The pressure at the summit of a syphon is
equal to atmospheric
less than atmospheric
more than atmospheric
none of the above
50.
Ay between two stream lines represents
velocity
discharge
head
pressure
51.
Coefficient of velocity for Borda’s mouth piece running full is
0.611
0.707
0.855
1.00
52.
Coefficient of discharge for a totally submerged orifice as compared to that for an orifice discharging free is
slightly less
slightly more
nearly half
equal
53.
The major loss of energy in long pipes is due to
sudden enlargement
sudden contraction
gradual contraction or enlargement
friction
54.
Coefficient of contraction for an external cylindrical mouthpiece is
1.00
0.855
0.7H
0.611
55.
Which of the following has highest coefficient of discharge ?
sharp edged orifice
venturimeter
Borda’s mouthpiece running full
CipoUetti weir
56.
In a Sutro weir, the discharge is proportional to where H is head.
H1/2
H3/2
H5/2
H
57.
The discharge over a broad crested weir is maximum when the depth of flow is where H is the available head.
H/3
H/2
2 H/5
2 H/3
58.
Which of the following statements is correct?
Lower critical Reynolds number is of no practical significance in pipe flow problems.
Upper critical Reynolds number is significant in pipe flow problems.
Lower critical Reynolds number has the value 2000 in pipe flow
Upper critical Reynolds number is the number at which turbulent flow changes to laminar flow.
59.
For a sphere of radius 15 cm moving with a uniform velocity of 2 m/sec through a liquid of specific gravity 0.9 and dynamic viscosity 0.8 poise, the Reynolds number will be
300
337.5
600
675
60.
The shear stress distribution for a fluid flowing in between the parallel plates, both at rest, is
constant over the cross section
parabolic distribution across the section
zero at the mid plane and varies linearly with distance from mid plane
zero at plates and increases linearly to midpoint
61.
If x is the distance from leading edge, then the boundary layer thickness in laminar flow varies as
x
x
x
x/7
62.
Stanton diagram is a
log-log plot of friction factor against Reynolds number
log-log plot of relative roughness against Reynolds number
semi-log plot of friction factor against Reynolds number
semi-log plot of friction factor against relative roughness
63.
The depth ‘d’ below the free surface at which the point velocity is equal to the average velocity of flow for a uniform laminar flow with a free surface, will be where D is the depth of flow.
0.423 D
0.577 D
0.223 D
0.707 D
64.
The boundary layer thickness in turbulent flow varies as where x is the distance from leading edge.
x”7
x,/2
x4/5
x3/5
65.
The distance y from pipe boundary, at which the point velocity is equal to average velocity for turbulent flow, is where R is radius of pipe.
0.223 R
0.423 R
0.577 R
0.707 R
66.
If a sphere of diameter 1 cm falls in castor oil of kinematic viscosity 10 stokes, with a terminal velocity of 1.5 cm/sec, the coefficient of drag on the sphere is
less than 1
between 1 and 100
160
200
67.
In case of an airfoil, the separation of flow occurs
at the extreme rear of body
at the extreme front of body
midway between rear and front of body
any where between rear and front of body depending upon Reynolds number
68.
When an ideal fluid flows past a sphere,
highest intensity of pressure occurs around the circumference at right angles to flow
lowest pressure intensity occurs at front stagnation point
lowest pressure intensity occurs at rear stagnation point
total drag is zero
69.
With the same cross-sectional area and immersed in same turbulent flow, the largest total drag will be on
a circular disc of plate held normal to flow
a sphere
a cylinder
a streamlined body
70.
In which of the following the friction drag is generally larger than pressure drag?
a circular disc or plate held normal to flow
a sphere
a cylinder
an airfoil
71.
For hydro-dynamically smooth boundary, the friction coefficient for turbulent flow is
constant
dependent only on Reynolds number
a function of Reynolds number and relative roughness
dependent on relative roughness only
72.
The value of friction factor ‘f’ for smooth pipes for Reynolds number 106 is approximately equal to
0.1
0.01
0.001
0.0001
73.
For laminar flow in a pipe of circular cross-section, the Darcy’s friction factor f is
directly proportional to Reynolds number and independent of pipe wall roughness
directly proportional to pipe wall roughness and independent of Reynolds number
inversely proportional to Reynolds number and indpendent of pipe wall roughness
inversely proportional to Reynolds number and directly proportional to pipe wall roughness
74.
Separation of flow occurs when
the pressure intensity reaches a minimum
the cross-section of a channel is reduced
the boundary layer comes to rest
all of the above
75.
The ratio of average velocity to maximum velocity for steady laminar flow in circular pipes is
1/2
2/3
3/2
2
76.
The distance from pipe boundary, at which the turbulent shear stress is one-third die wall shear stress, is where R is the radius of pipe.
1/3 R
1/2 R
2/3 R
3/4R
77.
The discharge of a liquid of kinematic viscosity 4 cm2/sec through a 8 cm dia-meter pipe is 3200n cm7sec. The type of flow expected is
laminar flow
transition flow
turbulent flow
not predictable from the given data
78.
The Prartdtl mixing length is
zero at the pipe wall
maximum at the pipe wall
independent of shear stress
none of the above
79.
The velocity distribution for laminar flow through a circular tube
is constant over the cross-section
varies linearly from zero at walls to maximum at centre
varies parabolically with maximum at the centre
none of the above
80.
A fluid of kinematic viscosity 0.4 cm2/sec flows through a 8 cm diameter pipe. The maximum velocity for laminar flow will be
less than 1 m/sec
1 m/sec
1.5 m/sec
2 m/sec
81.
The losses are more in
laminar flow
transition flow
turbulent flow
critical flow
82.
The wake
always occurs before a separation point
always occurs after a separation point
is a region of high pressure intensity
none of the above
83.
The maximum thickness of boundary layer in a pipe of radius r is
0
r/2
r
2r
84.
The hydraulic grade line is
always above the centre line of pipe
never above the energy grade line
always sloping downward in the direction of flow
all of the above
85.
Two pipe systems are said to be equivalent when
head loss and discharge are same in two systems
length of pipe and discharge are same in two systems
friction factor and length are same in two systems
length and diameter are same in two systems
86.
In series-pipe problems
the head loss is same through each pipe
the discharge is same through each pipe
a trial solution is not necessary
the discharge through each pipe is added to obtain total discharge
87.
Select the correct statement.
The absolute roughness of a pipe de-creases with time.
A pipe becomes smooth after using for long time.
The friction factor decreases with time.
The absolute roughness increases with time.
88.
A valve is suddenly closed in a water main in wl.ich the velocity is 1 m/sec and velocity of pressure wave is 981 m/ sec. The inertia head at the valve will be
1 m
10m
100m
none of the above
89.
The speed of a pressure wave through a pipe depends upon
the length of pipe
the viscosity of fluid
the bulk modulus for the fluid
the original head
90.
When time of closure tc = L/v0 (where L is length of pipe and v0 is speed of pressure wave), the portion of pipe length subjected to maximum head is
L/4
L/3
L/2
L
91.
If the elevation of hydraulic grade line at the junction of three pipes is above the elevation of reservoirs B and C and below reservoir A, then the direction of flow will be
from reservoir A to reservoirs B and C
from reservoir B to reservoirs C and A
from reservoir C to reservoirs A and B
unpredictable
92.
The length of a pipe is 1 km and its diameter is 20 cm. If the diameter of an equivalent pipe is 40 cm, then its length is
32 km
20 km
8 km
4 km
93.
Two pipes of same length and diameters d and 2d respectively are connected in series. The diameter of an equivalent pipe of same length is
less than d
between d and 1.5 d
between 1.5 d and 2d
greater than 2d
94.
The horse power transmitted through a pipe is maximum when the ratio of loss of head due to friction and total head supplied is
1/3
1/4
1/2
2/3
95.
The boundary layer thickness at a distance of l m from the leading edge of a flat plate, kept at zero angle of incidence to the flow direction, is O.l cm. The velocity outside the boundary layer is 25 ml sec. The boundary layer thickness at a distance of 4 m is Assume that boundary layer is entirely laminar.
0.40 cm
0.20 cm
0.10 cm
0.05 cm
96.
Drag force is a function of i) projected area of the body ii) mass density of the fluid iii) velocity of the body The correct answer is
(i) and (ii)
(i) and (iii)
(ii) and (iii)
(i), (ii) and (iii)
97.
The correct relationship among displacement thickness d, momentum thickness m and energy thickness e is
d > m > e
d > e > m
e > m > d
e > d > m
98.
For laminar flow in circular pipes, the Darcy’s friction factor f is equal to
16/Re
32/ Re
64/ Re
none of the above where R,, is Reynolds number.
99.
. Surge wave in a rectangular channel is an example of i) steady flow ii) unsteady flow iii) uniform flow iv) non-uniform flow The correct answer is
(i) and (iii)
(ii) and (iii)
(i) and (:v)
(ii) and (iv)
100.
Fluid is a substance that
cannot be subjected to shear forces
always expands until it fills any container
has the same shear stress.at a point regardless of its motion
cannot remain at rest under action of any shear force
flows.
101.
Fluid is a substance which offers no resistance to change of
pressure
flow
shape
volume
temperature.
102.
Practical fluids
are viscous
possess surface tension
are compressible
possess all the above properties
possess none of the above properties.
103.
In a static fluid
resistance to shear stress is small
fluid pressure is zero
linear deformation is small
only normal stresses can exist
viscosity is nil.
104.
A fluid is said to be ideal, if it is
incompressible
inviscous
viscous and incompressible
inviscous and compressible
inviscous and incompressible.
105.
An ideal flow of any fluid must fulfill the following
Newton’s law of motion
Newton’s law of viscosity
Pascal’ law
Continuity equation
Boundary layer theory.
106.
If no resistance is encountered by displacement, such a substance is known as
fluid
water
gas
perfect solid
ideal fluid.
107.
The volumetric change of the fluid caused by a resistance is known as
volumetric strain
volumetric index
compressibility
adhesion
cohesion.
108.
Liquids
cannot be compressed
occupy definite volume
are not affected by change in pressure and temperature
are not viscous
none of the above.
109.
Density of water is maximum at
0°C
0°K
4°C
100°C
20°C.
110.
The value of mass density in kgsecVm4 for water at 0°C is
1
1000
100
101.9
91
111.
Property of a fluid by which its own molecules are attracted is called
adhesion
cohesion
viscosity
compressibility
surface tension.
112.
Mercury does not wet glass. This is due to property of liquid known as
adhesion
cohesion
surface tension
viscosity
compressibility.
113.
The property of a fluid which enables it to resist tensile stress is known as
compressibility
surface tension
cohesion
adhesion
viscosity.
114.
Property of a fluid by which molecules of different kinds of fluids are attracted to each other is called
adhesion
cohesion
viscosity
compressibility
surface tension.
115.
The specific weight of water is 1000 kg/m”
at normal pressure of 760 mm
at 4°C temperature
at mean sea level
all the above
none of the above.
116.
Specific weight of water in S.I. units is equal to
1000 N/m3
10000 N/m3
9.81 xlO3 N/m3
9.81 xlO6N/m3
9.81 N/m3.
117.
When the flow parameters at any given instant remain same at every point, then flow is said to be
quasi static
steady state
laminar
uniform
static.
118.
Which of the following is demensionless
specific weight
specific volume
specific speed
specific gravity
specific viscosity.
119.
The normal stress in a fluid will be constant in all directions at a point only if
it is incompressible
it has uniform viscosity
it has zero viscosity
it is frictionless
it is at rest.
120.
The pressure at a point in a fluid will not be same in all the directions when the fluid is
moving
viscous
viscous and static
inviscous and moving
viscous and moving.
121.
An object having 10 kg mass weighs 9.81kg on a spring balance. The value of ‘g’ at this place is
10m/sec2
9.81 m/sec2
10.2/m sec
9.75 m/sec2
9 m/sec .
122.
The tendency of a liquid surface to contract is due to the following property
cohesion
adhesion
viscosity
surface tension
elasticity.
123.
The surface tension of mercury at normal temperature compared to that of water is
more
less
same
more or less depending on size of glass tube
none of the above.
124.
A perfect gas
has constant viscosity
has zero viscosity
is in compressible
is of theoretical interest
none of the above.
125.
For very great pressures, viscosity of moss gases and liquids
remains same
increases
decreases
shows erratic behavior
none of the above.
126.
A fluid in equilibrium can’t sustain
tensile stress
compressive stress
shear stress
bending stress
all of the above.
127.
Viscosity of water in comparison to mercury is
higher
lower
same
higher/lower depending on temperature
unpredictable.
128.
The bulk modulus of elasticity with increase in pressure
increases
decreases
remains constant
increases first up to certain limit and then decreases
unpredictable.
129.
The bulk modulus of elasticity
has the dimensions of 1/pressure
increases with pressure
is large when fluid is more compressible
is independent of pressure and viscosity
is directly proportional to flow.
130.
A balloon lifting in air follows the following principle
law of gravitation
Archimedes principle
principle of buoyancy
all of the above
continuity equation.
131.
The value of the coefficient of compressibility for water at ordinary pressure and temperature in kg/cm is equal to
1000
2100
2700
10,000
21,000.
132.
The increase of temperature results in
increase in viscosity of gas
increase in viscosity of liquid
decrease in viscosity of gas
decrease in viscosity of liquid
(a) and (d) above.
133.
Surface tension has the units of
newtons/m
newtons/m
new tons/m
newtons
newton m.
134.
Surface tension
acts in the plane of the interface normal to any line in the surface
is also known as capillarity
is a function of the curvature of the interface
decreases with fall in temperature
has no units.
135.
The stress-strain relation of the newtoneon fluid is
linear
parabolic
hyperbolic
inverse type
none of the above.
136.
A liquid compressed in cylinder has a volume of 0.04 m3 at 50 kg/cm2 and a volume of 0.039 m3 at 150 kg/cm2. The bulk modulus of elasticity of liquid is
400 kg/cm2
4000 kg/cm2
40 x 105 kg/cm2
40 x 106 kg/cm2
none of the above.
137.
The units of viscosity are
metres2 per sec
kg sec/metre
newton-sec per metre2
newton-sec per meter
none of the above.
138.
Kinematic viscosity is dependent upon
pressure
distance
level
flow
density.
139.
Units of surface tension are
energy/unit area
distance
both of the above
it has no units
none of the above.
140.
Which of the following meters is not associated with viscosity
Red wood
Say bolt
Engler
Orsat
none of the above.
141.
Choose the correct relationship
specific gravity = gravity x density
dynamicviscosity = kinematicviscosity x density
gravity = specific gravity x density
kinematicviscosity = dynamicviscosity x density
hydrostaticforce = surface tension x gravity.
142.
Dimensions of surface tension are
MlL°T2
MlL°Tx
MlL r2
MlL2T2
MlL°t.
143.
For manometer, a better liquid combination is one having
higher surface tension
lower surface tension
surface tension is no criterion
high density and viscosity
low density and viscosity.
144.
If mercury in a barometer is replaced by water, the height of 3.75 cm of mercury will be following cm of water
51 cm
50 cm
52 cm
52.2 cm
51.7 cm.
145.
Choose the wrong statement. lcohol is used in manometer, because
its vapour pressure is low
it provides suitable meniscus for the inclined tube
its density is less
it provides longer length for a given pressure difference
it provides accurate readings.
146.
Increase in pressure at the outer edge of a drum of radius R due to rotation at corad/sec, full of liquid of density p will be
pco2/?2
pco2/?2/2
2pa2R2
pa2R/2
none of the above.
147.
The property of fluid by virtue of which it offers resistance to shear is called
surface tension
adhesion
cohesion
viscosity
all of the above.
148.
Choose the wrong statement
fluids are capable of flowing
fluids conform to the shape of the containing vessels
when in equilibrium, fluids cannot sustain tangential forces
when in equilibrium, fluids can sustain shear forces
fluids have some degree of comprehensibility and offer little resistance to form.
149.
The density of water is 1000 kg/m3 at
0°C
0°K
4°C (d) 20°C
all temperature.
150.
If w is the specific weight of liquid and k the depth of any point from the surface, then pressure intensity at that point will be
h
wh
w/h
h/w
h/wh.
151.
Choose the wrong statement
Viscosity of a fluid is that property which determines the amount of its resistance to a shearing force
Viscosity is due primarily to interaction between fluid molecules
Viscosity of liquids decreases with in-crease in temperature
Viscosity of liquids is appreciably affected by change in pressure
Viscosity is expressed as poise, stoke, or saybolt seconds.
152.
The units of kinematic viscosity are
metres2 per sec
kg sec/metre
newton-sec per metre
newton-sec per metre
none of the above.
153.
The ratio of absolute viscosity to mass density is known as
specific viscosity
viscosity index
kinematic viscosity
coefficient of viscosity
coefficient of compressibility.
154.
Kinematic viscosity is equal to
dynamic viscosity/density
dynamicviscosity x density
density/dynamic viscosity
1/dynamicviscosity x density
same as dynamic viscosity.
155.
Which of the following is the unit of kinematic viscosity
pascal
poise
stoke
faraday
none of the above.
156.
A one dimensional flow is one which
is uniform flow
is steady uniform flow
takes place in straight lines
involves zero transverse component of flow
takes place in one dimension.
157.
Alcohol is used in manometers because
it has low vapour pressure
it is clearly visible
it has low surface tension
it can provide longer column due to low density
is provides suitable meniscus.
158.
A pressure of 25 m of head of water is equal to
25 kN/m2
245 kN/m2
2500 kN/m2
2.5kN/m2
12.5 kN/m2.
159.
Specific weight of sea water is more that of pure water because it contains
dissolved air
dissolved salt
suspended matter
all of the above
heavy water.
160.
If 850 kg liquid occupies volume of one cubic meter, men 0.85 represents its
specific weight
specific mass
specific gravity
specific density
none of the above.
161.
Free surface of a liquid tends to contract to the smallest possible area due to force of
surface tension
viscosity
friction
cohesion
adhesion.
162.
A bucket of water is hanging from a spring balance. An iron piece is suspended into water without touching sides of bucket from another support. The spring balance reading will
increase
decrease
remain same
increase/decrease depending on depth of immersion
unpredictable.
163.
Falling drops of water become spheres due to the property of
adhesion
cohesion
surface tension
viscosity
compressibility.
164.
A liquid would wet the solid, if adhesion forces as compared to cohesion forces are
less
more
equal
less at low temperature and more at high temperature
there is no such criterion.
165.
If cohesion between molecules of a fluid is greater than adhesion between fluid and glass, then the free level of fluid in a dipped glass tube will be
higher than the surface of liquid
the same as the surface of liquid
lower than the surface of liquid
unpredictable
none of the above.
166.
The total pressure on the surface of a vertical sluice gate 2 m x 1 m with its top 2 m surface being 0.5 m below the water level will be
500 kg
1000 kg
1500 kg
2000 kg
4000 kg.
167.
The resultant upward pressure of a fluid on a floating body is equal to the weight of the fluid displaced by the body. This definition is according to
Buoyancy
Equilibrium of a floating body
Archimedes’ principle
Bernoulli’s theorem
Metacentric principle.
168.
The resultant upward pressure of the fluid on an immersed body is called
upthrust
buoyancy
center of pressure
all the above are correct
none of above is correct.
169.
The conditions for the stable equilibrium of a floating body are
the meta-center should lie above the center of gravity
the center of buoyancy and the center of gravity must lie on the same vertical line
a righting couple should be formed
all the above are correct
none of the above is correct.
170.
Metacentric height is given as the distance between
the center of gravity of the body and the meta center
the center of gravity of the body and the center of buoyancy
the center of gravity of the body and the center of pressure
center of buoyancy and metacentre
none of the above.
171.
The buoyancy depends on
mass of liquid displaced
viscosity of the liquid
pressure of the liquid displaced
depth of immersion
none of the above.
172.
The center of gravity of the volume of the liquid displaced by an immersed body is called
meta-center
center of pressure
center of buoyancy
center of gravity
none of the above.
173.
A piece of metal of specific gravity 13.6 is placed in mercury of specific gravity 13.6, what fraction of it volume is under mercury?
the metal piece will simply float over the mercury
the metal piece will be immersed in mercury by half
whole of the metal piece will be immersed with its top surface just at mercury level
metal piece will sink to the bottom
none of the above.
174.
The angle of contact in case of a liquid depends upon
the nature of the liquid and the solid
the material which exists above the free surface of the liquid
both of die above
any one of the above
none of die above.
175.
Free surface of a liquid behaves like a sheet and tends to contract to smallest possible area due to the
force of adhesion
force of cohesion
force of friction
force of diffusion
none of die above.
176.
Rain drops are spherical because of
viscosity
air resistance
surface tension forces
atmospheric pressure
none of the above.
177.
Surface energy per unit area of a surface is numerically equal to ..
atmospheric pressure
surface tension
force of adhesion
force of cohesion
viscosity.
178.
The capillary rise at 20°C in a clean glass tube of 1 mm bore containing water is approximately
1 mm
5 mm
10 mm
20 mm
30 mm.
179.
The difference of pressure between the inside and outside of a liquid drop is
= Txr
= T/r
p = T/2r
= 2T/r
none of the above.
180.
If the surface of liquid is convex, men
cohesion pressure is negligible
cohesion pressure is decreased
cohesion pressure is increased
there is no cohesion pressure
none of the above.
181.
To avoid vaporisation in the pipe line, the pipe line over the ridge is laid such that it is not more than
2.4 m above the hydraulic gradient
6.4 m above the hydraulic gradient
10.0 m above the hydraulic gradient
5.0 above the hydraulic gradient
none of the above.
182.
To avoid an interruption in the flow of a syphon, an air vessel is provided
at the inlet
at the outlet
at the summit
ay nay point between inlet and outlet
none of the above.
183.
The vapour pressure over the concave surface is
less man the vapour pressure over the plane surface
equal to the vapour pressure over the plane surface
greater than the vapour pressure over the plane surface
zero
none of the above.
184.
The property by virtue of which a liquid opposes relative motion between its different layers is called
surface tension
co-efficient of viscosity
viscosity
osmosis
cohesion.
185.
The process of diffusion of one liquid into the other through a semi-permeable membrane is called
viscosity
osmosis
surface tension
cohesion
diffusivity.
186.
The units of dynamic or absolute viscosity are
metres2 per sec
kg sec/meter
newton-sec per meter
newton-sec2 per meter
none of the above.
187.
The continuity equation is connected with
viscous/unviscous fluids
compressibility of fluids
conservation of mass
steady/unsteady flow
open channel/pipe flow.
188.
The rise or depression of liquid in a tube due to surface tensionwim increase in size of tube will
increase
remain unaffected
may increase or decrease depending on the characteristics of liquid
decrease
unpredictable.
189.
Liquids transmit pressure equally in all the directions. This is according to
Boyle’s law
Archimedes principle
Pascal’s law
Newton’s formula
Chezy’s equation.
190.
Capillary action is due to the
surface tension
cohesion of the liquid
adhesion of the liquid molecules and the molecules on the surface of a solid
all of the above
none of the above.
191.
Newton’s law of viscosity is a relationship between
shear stress anctthejiate of angular distortion
shear stress and viscosity
shear stress, velocity and viscosity
pressure, velocity and viscosity
shear stress, pressure and rate of angular distortion.
192.
The atmospheric pressure with rise in altitude decreases
linearly
first slowly and then steeply
first steeply and then gradually
unpredictable
none of the above.
193.
Pressure of the order of 10″‘ torr can be measured by
Bourdon tube
Pirani Gauge
micro-manometer
ionisastion gauge
McLeod gauge.
194.
Operation of McLeod gauge used for low pressure measurement is based on the principle of
gas law
Boyle’s law
Charle’s law
Pascal’s law
McLeod’s law.
195.
An odd shaped body weighing 7.5 kg and occupying 0.01 m3 volume will be completely submerged in a fluid having specific gravity of
1
1.2
0.8
0.75
1.25.
196.
In an isothermal atmosphere, the pressure
decreases linearly with elevation
remains constant
varies in the same way as the density
increases exponentially with elevation
unpredictable.
197.
. Mercury is often used in barometer because
it is the best liquid
the height of barometer will be less
its vapour pressure is so low that it may be neglected
both (b) and (c)
it moves easily.
198.
. Barometer is used to measure
pressure in pipes, channels etc.
atmospheric pressure
very low pressure
difference of pressure between two points
rain level.
199.
. Which of the following instrument can be used for measuring speed of a submarine moving in deep sea
Venturimeter
Orifice plate
hot wire anemometer
rotameter
pitot tube.
200.
. Which of the following instrument can be used for measuring speed of an aeroplane
Venturimeter
Orifice plate
hot wire anemometer
rotameter
pitot tube.
201.
. Piezometer is used to measure
pressure in pipe, channels etc.
atmospheric pressure
very low pressures
difference of pressure between two points
flow.
202.
. Which of the following instruments is used to measure flow on the application of Bernoulli’s theorem
Venturimeter
Orifice plate
nozzle
pitot tube
all of the above.
203.
. The speed of sound in a ideal gas varies directly as its
pressure
temperature
density
modulus of elasticity
absolute temperature,
204.
. Dynamic viscosity of most of the liquids with rise in temperature
increases
decreases
remains unaffected
unpredictable
none of the above.
205.
. Dynamic viscosity of most of the gases with rise in temperature
increases
decreases
remains unaffected
unpredictable
none of the above.
206.
. A metal with specific gravity of o floating in a fluid of same specific gravity a will
sink to bottom
float over fluid
partly immersed
be fully immersed with top surface at fluid surface
none of the above.
207.
. Euler’s dimensionless number relates the following
inertial force and gravity
viscous force and inertial force
viscous force and buoyancy force
pressure force and inertial force
pressure force and viscous force.
208.
. Manometer is used to measure
pressure in pipes, channels etc.
atmospheric pressure
very low pressure
difference of pressure between two points
velocity.
209.
. Which of the following manometer has highest sensitivity
U-tube with water
inclined U-tube
U-tube with mercury
micro-manometer with water
displacement type.
210.
. In order to increase sensitivity of U-tube manometer, one leg is usually inclined by angle 9. Sensitivity of inclined tube to sensitivity of U-tube is equal to
sin 9
sin 9
cas 9
cos 9
tan 9.
211.
. Working principle of dead weight pressure gauge tester is based on
Pascal’s law
Dalton’s law of partial pressure
Newton’s law of viscosity .
Avogadro’s hypothesis
Second law of thermodynamic.
212.
. The resultant of all normal pressures acts
at e.g. of body
at center of pressure
vertically upwards
at metacentre
vertically downwards.
213.
. Center of pressure compared to e.g. is
above it
below it.
at same point
above or below depending on area of body
none of the above.
214.
. Metacentric height is the distance between the metacentre and
water surface
center of pressure
center of gravity
center of buoyancy
none of the above.
215.
. The resultant upward pressure of the fluid on an immersed body due to its tendency to uplift the sub-merged body is called
upthrust
reaction
buoyancy
metacentre
center of pressure.
216.
. The center of pressure of a surface subjected to fluid pressure is the point
on the surface at which resultant pres-sure acts
on the surface at which gravitational force acis
at which all hydraulic forces meet
similar to metacentre
where pressure equivalent to hydraulic thrust will act.
217.
. Buoyant force is
resultant force acting on a floating body
equal to the volume of liquid displaced
force necessary to keep a body in equilibrium
the resultant force on a body due to the fluid surrounding it
none of the above.
218.
. The line of action of the buoyant force acts through the
centroid of the volume of fluid vertically above the body
centre of the volume of floating body
center of gravity of any submerged body
centriod of the displaced volume of fluid
none of the above.
219.
. Center of buoyancy is the
centroid of the displaced volume of fluid
center of pressure of displaced volume
e.g. of floating ‘body
does not exist
none of the above.
220.
. A body floats in stable equilibrium
when its meatcentric height is zero
when the metancentre is above e.g.
when its e.g. is below it’s center of buoyancy
metacentre has nothing to do with position of e.g. for determining stability
none of the above.
221.
. A piece weighing 3 kg in air was found to weigh 2.5 kg when submerged in water. Its specific gravity is
1
5
7
6
222.
. The total pressure force on a plane area is equal to the area multiplied by the intensity of pressure at the centriod, if
the area is horizontal
the area is vertical
the area is inclined
all of the above
none of the above.
223.
. A square surface 3 m x 3 m lies in a vertical line in water pipe its upper edge at water surface. The hydrostatic force on square surface is
9,000 kg
13,500 kg
18,000 kg
27,000 kg
30,000 kg.
224.
. The depth of the center of pressure on a vertical rectangular gate 8 m wide and 6 m high, when the water surface coincides with the top of the gate, is
2.4 m
3.0 m
4.0 m
2.5 m
5.0 m.
225.
. If the atmospheric pressure on the surface of an oil tank (sp. gr. 0.8) is 0.2 kg/cm”, the pressure at a depth of 50 m below the oil surface will be
2 meters of water column
3 meters of water column
5 meters of water column
6 meters of water Column
7 meters of water column.
226.
. Metacentre is the point of intersection of
vertical upward force through e.g. of body and center line of body
buoyant force and the center line of body
mid point between e.g. and center of buoyancy
all of the above
none of the above.
227.
. Choose the wrong statement
The horizontal component of the hydro-static force on any surface is equal to the normal force on the vertical projection of the surface
The horizontal component acts through the center of pressure for the vertical projection
The vertical component of the hydrostatic force on any surface is equal to the weight of the volume of the liquid above the area
he vertical component passes through the center of pressure of the volume
Center of pressure acts at a greater depth than center of gravity.
228.
. For a body floating in a liquid the normal pressure exerted by the liquid acts at
bottom surface of the body
e.g. of the body
metacentre
all points on the surface of the body
all of the above.
229.
. Choose the wrong statement (p) Buoyant force is equal to the weight of the liquid displaced
any weight, floating or immersed in a liquid, is acted upon by a buoyant force
The point through which buoyant force acts, is called the center of buoyancy
Center of buoyancy is located above the center of gravity of the displaced liquid v
Relative density of liquids can be determined by means of the depth of flotation of hydrometer.
230.
. According to the principle of buoyancy a body totally or partially immersed in a fluid will be lifted up by a force equal to
the weight of the body
more than the weight of the body
less than the weight of the body
weight of the fluid displaced by the body
weight of body plus the weight of the fluid displaced hy the body.
231.
. When a body floating in a liquid, is displaced slightly, it oscillates about
e.g. of body
center of pressure
center of buoyancy
metacentre
liquid surface.
232.
. Ratio of inertia force to surface Jension is known as
Mach number
Froude number
Reynold’s number
Weber’s number
none of the above.
233.
. A ship whose hull length is 100 m is to travel at 10 m/sec. For dynamic similarity, at what velocity should a 1:25 model be towed through water ?
10 m/sec
25 m/sec
2 m/sec
50 m/sec
250 m/sec.
234.
. A model of a reservior is drained in 4 mts by opening the sluice gate. The model scale is 1: 225. How long should it take to empty the prototype ?
900 minutes
4 minutes
4 x (225)3/2 minutes
4 (225)1/3 minutes
4 x V225 minutes.
235.
. A model of torpedo is tested in a towing tank at a velocity of 25 m/sec. The prototype is expected to attain a velocity of 5 m/sec. What model scale has been used ?
1 : 5
1 : 2.5
1 :25
1:V5″
1 : 53/2
236.
. Ratio of inertia force to elastic force is known as
Mach number
Froude number
Reynold’s number
Weber’s number
none of the above.
237.
. For a floating body to be in stable equilibrium, its metacentre should be
below the center of gravity
below the center of buoyancy
above the center of buoyancy
between e.g. and center of pressure
above the center of gravity.
238.
. For a floating body to be in equilibrium
meta centre should be above e.g.
centre of buoyancy and e.g. must lie on same vertical plane
a righting couple should be formed
all of the above
none of the above.
239.
. The two important forces for a floating body are
buoyancy, gravity
buoyancy, pressure
buoyancy, inertial
inertial, gravity
gravity, pressure.
240.
. Choose the wrong statement
The center of buoyancy is located at the center of gravity of the displaced liquid
For stability of a submerged body, the center of gravity of body must lie directly below the center of buoyancy
If e.g. and center of buoyancy coincide, the submerged body must lie at neutral equilibrium for all positions
For stability of floating cylinders or spheres, the e.g. of body must lie below the center of buoyancy
All floating bodies are stable.
241.
. Center of pressure on an inclined plane is
at the centroid
above the centroid
below the centroid
at metacentre
at center of pressure.
242.
. An open vessel of water is accelerated up an inclined plane. The free water surface will
be horizontal
make an angle in direction of inclination of inclined plane
make an angle in opposite direction to inclination of inclined plane
any one of above is possible
none of the above.
243.
. The line of action of the buoyant force acts through the centroid of the
submerged body
volume of the floating body
volume of the fluid vertically above the body
displaced volume of the fluid
none of the above.
244.
. Resultant pressure of the liquid in the case of an immersed body acts through
centre of gravity
centre of pressure
metacentre
centre of buoyancy
in between e.g. and centre of pressure.
245.
. The centre of gravity of the volume of the liquid displaced by an immersed body is called
centre of gravity
centre of pressure
metacentre
centre of buoyancy
centroid.
246.
. Differential monometer is used to measure
pressure in pipes, channels etc.
atmospheric pressure
very low pressure
difference of pressure between two points
velocity in pipes
247.
. The pressure in the air space above an oil (sp. gr. 0.8) surface in a tank is 0.1 kg/cm”. The pressure at 2.5 m below the oil surface will be
2 metres of water column
3 metres of water column
3.5 metres of water column
4 m of water column
none of the above.
248.
. The time oscillation of a floating body with increase in metacentric height will be
same
higher
lower
lower/higher depending on weight of body
unpredictable.
249.
. In an immersed body, centre of pressure is
at the centre of gravity
above the centre of gravity
below be centre of gravity
could be above or below e.g. depend¬ing on density of body and liquid
unpredictable.
250.
. The normal stress is same in all directions at a point in a fluid
only when the fluid is frictionless
only when the fluid is incompressible and has zero viscosity
when there is no motion of one fluid layer relative to an adjacent layer
irrespective of the motion of one fluid layer relative to an adjacent layer
in case of an ideal fluid.
251.
. Select the correct statement
Local atmospheric pressure depends upon elevation of locality only
Standard atmospheric pressure is the mean local atmospheric pressure a* sea level
Local atmospheric pressure is always below standard atmospheric pressure
A barometer reads the difference be-tween local and standard atmospheric pressure
Gauge piessure is equal to atmospheric pressure plus instrument reading.
252.
. For measuring flow by a venturimeter, if should be installed in
vertical line
horizontal line
inclined line with flow downward
inclined line with upward flow
in any direction and in any location.
253.
. Total pressure on a lmxlm gate immersed vertically at a depth of 2 m below the free water surface will be
1000 kg
4000 kg
2000 kg
8000 kg
16000 kg.
254.
. Hot wire anemometer is used to measure
pressure in gases
liquid discharge
pressure in liquids
gas velocities
temperature.
255.
. Rotameter is a device used to measure
absolute pressure
velocity of fluid
flow
rotation
velocity of air.
256.
Flow of water in a pipe about 3 metres in diameter can be measured by
orifice plate
venturi
rotameter
pitot tube
nozzle
257.
. True one-dimensional flow occurs when
the direction and magnitude of the veiocity at all points are identical
the velocity of successive fluid par-ticles, at any point, is the same at suc-cessive periods of time
the magnitude and direction of the velocity do not change from point to point in the fluid
the fluid particles move in plane or parallel planes and the streamline pat-terns are identical in each plane
velocity, depth, pressure etc. change from point to point in the fluid flow.
258.
. An ideal flow of any fluid must satisfy
Pascal law
Newton’s law of viscosity
boundary layer theory
continuity equation
Bernoulli’s theorem.
259.
. In the case of steady flow of a fluid, the acceleration of any fluid particle is
constant
variable
zero
zero under limiting conditions
never zero.
260.
. Non uniform flow occurs when
the direction and magnitude of the velocity at all points are identical
the velocity of successive fluid particles, at any point, is the same at successive periods of time
the magnitude aricf direction of the velocity do not change from point to point in the fluid
the fluid particles move in plane or parallel planes and the streamline pat-terns are identical in each plane
velocity, depth, pressure, etc. change from point to point in the fluid flow.
261.
. During the opening of a valve in a pipe line, the flow is
steady
unsteady
uniform
laminar
free vortex type.
262.
. Uniform flow occurs when
the flow is steady
the flow is streamline
size and shape of the cross section in a particular length remain constant
size and cross section change uniformly along length
flow occurs at constant fate.
263.
. Gradually varied flow is
steady uniform
non-steady non-uniform
non-steady uniform
steady non-uniform
true one-dimensional.
264.
. Steady flow occurs when
the direction and magnitude of the velocity at all points are identical
the velocity of successive fluid particles, at any point, is the same at successive periods of time
the magnitude and direction of the velocity do not change from point to point in the fluid
the fluid particles move in plane or parallel planes and the streamline pat-terns are identical in each plane
velocity, depth, pressure, etc. change from point to point in the fluid flow.
265.
. The flow which neglects changes in a transverse direction is known as
one dimensional flow
uniform flow
steady flow
turbulent flow
streamline flow.
266.
. The flow in which each liquid particle has a definite path and their paths do not cross each other is called
one dimensional flow
uniform flow
steady flow
turbulent flow
streamline flow.
267.
. The flow in which conditions do not change with time at any point, is known as
one dimensional flow
uniform flow
steady flow
turbulent flow
streamline flow.
268.
. The flow in which the velocity vector is identical in magnitude and direction at every point, for any given instant, is known as
one dimensional flow
uniform flow
steady flow
turbulent flow
streamline flow.
269.
. The flow in which the particles of a fluid attain such velocities that vary from point to point in magnitude and direction as well as from instant to instant, is known as
one dimensional flow
uniform flow
steady flow
turbulent flow
streamline flow.
270.
. Flow occurring in a pipeline when a valve is being opened is
steady
unsteady
laminar
vortex
rotational.
271.
. General energy equation holds for
steady flow
turbulent flow
laminar flow
non-uniform flow
all of the above.
272.
. A streamline is defined as the line
parallel to central axis flow
parallel to outer surface of pipe
of equal yelocity in a flow
along which the pressure drop is uniform
which occurs in all flows.
273.
. Two dimensional flow occurs when
the direction and magnitude of the velocity at all points are identical
the velocity of successive fluid particles, at any point, is the same at successive periods of time
the magnitude and direction of the velocity do not change from point to point in the fluid
the fluid particles move in plane or parallel planes and the streamline pat-terns are identical in each plane
velocity, depth, pressure, etc. change from point to point in the fluid flow.
274.
. A piece of metal of specific gravity 7 floats in mercury of specific gravity 13.6. What fraction of its volume is under mercury ?
0.5
0.4
0.515
0.5
none of the above.
275.
. A piece of wood having weight 5 kg floats in water with 60% of its volume under the liquid. The specific gravity of wood is
0.83
0.6
0.4
0.3
none of the above.
276.
. The velocity of jet of water travelling out of opening in a tank filled with water is proportional to
head of water (h)
h2
V/T
h2
h3/1.
277.
. In a free vortex motion, the radial component of velocity everywhere is
maximum
minimum
zero
non-zero and finite
unpredictable.
278.
. In a forced vortex, the velocity of flow everywhere within the fluid is
maximum
minimum
zero
non-zero finite
unpredictable.
279.
. The region between the separation streamline and the boundary surface of the solid body is known as
wake
drag
lift
boundary layer
aerofoil section.
280.
. For hypersonic flow, the Mach number is
unity
greater than unity
greater than 2
greater than 4
greater than 10.
281.
. The upper surface of a weir over which water flows is known is
crest
nappe
sill
weir top
contracta.
282.
. Normal depth in open channel flow is the depth of flow corresponding to
steady flow
unsteady flow
laminar flow
uniform flow
critical flow.
283.
. Uniform flow occurs when
the direction and magnitude of the velocity at all points are identical
the velocity of successive fluid paiticles, at any point, is the same at successive periods of time
the magnitude and direction of the velocity do not change from point to point in the fluid
the fluid particles move in plane or parallel planes and the streamline pat-terns are identical in each pleasure
velocity, depth, pressure, etc. change from point to point in the fluid flow.
284.
. Pitot tube is used for measurement of
pressure
flow
velocity
dsscharge
viscosity.
285.
. Hydrometer is used to determine
specific gravity of liquids
specific gravity of solids
specific gravity of gases
relative humidity
density.
286.
. The total energy of each particle at various places in the case of perfect incompres sible fluid flowing in continuous sream
keeps on increasing
keeps on decreasing
remains constant
may increase/decrease
unpredictable.
287.
. According to Bernoulli’s equation for steady ideal fluid flow
principle of conservation of mass holds
velocity and pressure are inversely proportional
total energy is constant throughout
the energy is constant along a stream-line but may vary across streamlines
none of the above.
288.
. The equation of continuity holds good when the flow
is steady
is one dimensional
velocity is uniform at all the cross sections
all of the above
none of the above.
289.
. Mach number is significant in
supersonics, as with projectiles and jet propulsion
full immersion or completely enclosed flow, as with pipes, aircraft wings, nozzles etc.
simultaneous motion through two fluids where there is a surface of dis-continuity, gravity force, and wave making effects, as with ship’s hulls
all of fhe above
none of the above.
290.
. Froude number is significant in
supersonics, as with projectile and jet propulsion
full immersion or completely enclosed flow, as with pipes, aircraft wings, nozzles etc.
simultaneous motion through two fluids where there is a surface of dis-continuity, gravity forces, and wave making effect, as with ship’s hulls
all of the above
none of the above
291.
. All the terms of energy in Bernoulli’s equation have dimension of
energy
work
mass
length
time.
292.
. Reynolds number is significant in
supersonics, as with projectile and jet propulsion
full immersion or completely enclosed flow, as with pipes, aircraft wings, nozzles etc.
simultaneous motion through two fluids where there is a surface of dis-continuity, gravity forces, and wave making effect, as with ship’s hulls
all of the above
none of the above.
293.
. The fluid forces considered in the Navier Stokes equation are
gravity, pressure and viscous
gravity, pressure and turbulent
pressure, viscous and turbulent
gravity, viscous and turbulent
none of the above.
294.
. A large Roynold number is indication of
smooth and streamline flow
laminar flow
steady flow
turbulent flow
highly turbulent flow.
295.
. For pipes, laminar flow occurs when Roynolds number is
less than 2000
between 2000 and 4000
more than 4000
less than 4000
none of the above.
296.
. In order that flow takes place between two points in a pipeline, the differential pressure between these points must be more than
frictional force
viscosity
surface friction
all of the above
none of the above.
297.
. At the center line of a pipe flowing under pressure where the velocity gradient is zero, the shear stress will be
minimum
maximum
zero
negative value
could be any value.
298.
. The pressure in Pascals at a depth of 1 m below the free surface of a body of water will be equal to
1 Pa
91 Pa
981 Pa
9810 Pa
98,100 Pa.
299.
. Two pipe systems can be said to be equivalent, when the following quantites are same
friction loss and flow
length and diameter
flow and length
friction factor and diameter
velocity and diameter.
300.
. For pipes, turbulent flow occurs when Reynolds number is
less than 2000
between 2000 and 4000
more than 4000
less than 4000
none of the above.
301.
. Bernoulli equation deals with the law of conservation of
mass
momentum
energy
work
force.
302.
. A hydraulic press has a ram of 15 cm diameter and plunger of 1.5 cm. It is required to lift a weight of 1 tonne. The force required on plunger is equal to
10 kg
100 kg
1000 kg
1 kg
10,000 kg.
303.
. Cavitation is caused by
high velocity
high pressure
weak material
low pressure
low viscosity.
304.
. Cavitation will begin when
the pressure at any location reaches an absolute pressure equal to the saturated vapour pressure of the liquid
pressure becomes more than critical pressure
flow is increased
pressure is increased
none of the above.
305.
. Principle of similitude forms the basis of
comparing two identical equipments
designing models so that the result can be converted to prototypes
comparing similarity between design and actual equipment
hydraulic designs
performing acceptance tests.
306.
. For similarity, in addition to models being geometrically similar to prototype, the following in both cases should also be equal
ratio of inertial force to force due to viscosity
ratio of inertial force to force due to gravitation
ratio of inertial force to force due to surface tension
all the four ratios of inertial force to force due to viscosity, gravitation, sur-face tension, and elasticity
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