Option A: The absolute roughness of a pipe de-creases with time
Option B: A pipe becomes smooth after using for long time
Option C: The friction factor decreases with time
Option D: The absolute roughness increases with time
Correct Answer: The absolute roughness increases with time ✔
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Option A: gm/cm-sec2
Option B: dyne-sec/cm2
Option C: gm/cm2-sec
Option D: cm2/sec
Correct Answer: cm2/sec ✔
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Option A: pressure
Option B: kinematic viscosity
Option C: dynamic viscosity
Option D: surface tension
Correct Answer: dynamic viscosity ✔
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Option A: one which obeys Newton’s law of viscosity
Option B: frictionless and incompressible
Option C: very viscous
Option D: frictionless and compressible
Correct Answer: frictionless and incompressible ✔
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Option A: 0.25
Option B: 0.50
Option C: 1.0
Option D: none of the above
Correct Answer: 1.0 ✔
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Option A: decreases with increase in temperature
Option B: increases with increase in temperature
Option C: is independent of temperature
Option D: is independent of pressure for very high pressure intensities
Correct Answer: increases with increase in temperature ✔
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Option A: intensity of pressure and rate of angular deformation
Option B: shear stress and rate of angular deformation
Option C: shear stress, viscosity and temperature
Option D: viscosity and rate of angular deformation
Correct Answer: shear stress and rate of angular deformation ✔
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Option A: at the centroid of the submerged area
Option B: always above the centroid of the area
Option C: always below the centroid of the area
Option D: none of the above
Correct Answer: always below the centroid of the area ✔
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Option A: 3.75 m
Option B: 4.0 m
Option C: 4.2m
Option D: 4.5m
Correct Answer: 4.2m ✔
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Option A: when its metacentric height is zero
Option B: when the metacentre is above the centre of gravity
Option C: when the metacentre is below the centre of gravity
Option D: only when its centre of gravity is below its centre of buoyancy
Correct Answer: when the metacentre is above the centre of gravity ✔
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If the weight of a body immersed in a fluid exceeds the buoyant force, then the body will__________?
Option A: rise until its weight equals the buoyant force
Option B: tend to move downward and it may finally sink
Option C: float
Option D: none of the above
Correct Answer: tend to move downward and it may finally sink ✔
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Option A: (1) and (3)
Option B: (1)and(iv)
Option C: (2) and (3)
Option D: (2) and (4)
Correct Answer: (1)and(iv) ✔
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Option A: center of gravity
Option B: center of buoyancy
Option C: center of pressure
Option D: metacentre
Correct Answer: center of pressure ✔
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Option A: linearly with radial distance
Option B: as the square of the radial distance
Option C: inversely as the square of the radial distance
Option D: inversely as the radial distance
Correct Answer: as the square of the radial distance ✔
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Option A: zero
Option B: one-fourth its value when cylinder was full
Option C: one-half its value when cylinder was full
Option D: cannot be predicted from the given data
Correct Answer: zero ✔
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Option A: Coefficient of contraction of a venturimeter is unity
Option B: Flow nozzle is cheaper than venturimeter but has higher energy loss
Option C: Discharge is independent of orientation of venturimeter whether it is horizontal, vertical or inclined
Option D: None of the above statement is correct.
Correct Answer: None of the above statement is correct. ✔
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Option A: (1) and (2)
Option B: (1)and(4)
Option C: (2) and (3)
Option D: (3) and (4)
Correct Answer: (1)and(4) ✔
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Option A: The pressure intensity at vena contracta is atmospheric
Option B: Contraction is least at vena contracta
Option C: Stream lines are parallel throughout the jet at vena contracta
Option D: Coefficient of contraction is always less than one
Correct Answer: Stream lines are parallel throughout the jet at vena contracta ✔
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Option A: (1) and (2)
Option B: (1)and(iv)
Option C: (2) and (3)
Option D: (2) and (4)
Correct Answer: (1)and(iv) ✔
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Option A: (1) and (3)
Option B: (2) and (3)
Option C: (1) and (4)
Option D: (2) and (4)
Correct Answer: (2) and (4) ✔
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Option A: 4/3
Option B: 3/2
Option C: 9/4
Option D: 27/8
Correct Answer: 9/4 ✔
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Option A: x2y
Option B: x2-y2
Option C: cosx
Option D: x2 + y2
Correct Answer: x2-y2 ✔
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Option A: directly proportional to its radial distance from axis of rotation
Option B: inversely proportional to its radial distance from the axis of rotation
Option C: inversely proportional to the square of its radial distance from the axis of rotation
Option D: directly proportional to the square of its radial distance from the axis of rotation
Correct Answer: directly proportional to its radial distance from axis of rotation ✔
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Option A: mass
Option B: energy
Option C: momentum
Option D: none of the above
Correct Answer: mass ✔
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Option A: velocity at stagnation point
Option B: stagnation pressure
Option C: static pressure
Option D: dynamic pressure
Correct Answer: stagnation pressure ✔
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Option A: 0.611
Option B: 0.85
Option C: 0.98
Option D: 1.00
Correct Answer: 0.611 ✔
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Option A: equal to atmospheric
Option B: less than atmospheric
Option C: more than atmospheric
Option D: none of the above
Correct Answer: less than atmospheric ✔
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Option A: 0.611
Option B: 0.707
Option C: 0.855
Option D: 1.00
Correct Answer: 0.707 ✔
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Option A: sudden enlargement
Option B: sudden contraction
Option C: gradual contraction or enlargement
Option D: friction
Correct Answer: friction ✔
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Option A: sharp edged orifice
Option B: venturimeter
Option C: Borda’s mouthpiece running full
Option D: CipoUetti weir
Correct Answer: venturimeter ✔
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Option A: H/3
Option B: H/2
Option C: 2 H/5
Option D: 2 H/3
Correct Answer: H/3 ✔
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Option A: 300
Option B: 337.5
Option C: 600
Option D: 675
Correct Answer: 675 ✔
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Option A: 0.423 D
Option B: 0.577 D
Option C: 0.223 D
Option D: 0.707 D
Correct Answer: 0.577 D ✔
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Option A: at the extreme rear of body
Option B: at the extreme front of body
Option C: midway between rear and front of body
Option D: any where between rear and front of body depending upon Reynolds number
Correct Answer: at the extreme rear of body ✔
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Option A: 0.223 R
Option B: 0.423 R
Option C: 0.577 R
Option D: 0.707 R
Correct Answer: 0.223 R ✔
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Option A: a circular disc of plate held normal to flow
Option B: a sphere
Option C: a cylinder
Option D: a streamlined body
Correct Answer: a circular disc of plate held normal to flow ✔
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Option A: constant
Option B: dependent only on Reynolds number
Option C: a function of Reynolds number and relative roughness
Option D: dependent on relative roughness only
Correct Answer: dependent only on Reynolds number ✔
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For laminar flow in a pipe of circular cross-section, the Darcy’s friction factor f is__________?
Option A: directly proportional to Reynolds number and independent of pipe wall roughness
Option B: directly proportional to pipe wall roughness and independent of Reynolds number
Option C: inversely proportional to Reynolds number and indpendent of pipe wall roughness
Option D: inversely proportional to Reynolds number and directly proportional to pipe wall roughness
Correct Answer: inversely proportional to Reynolds number and indpendent of pipe wall roughness ✔
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Option A: laminar flow
Option B: transition flow
Option C: turbulent flow
Option D: not predictable from the given data
Correct Answer: laminar flow ✔
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Option A: is constant over the cross-section
Option B: varies linearly from zero at walls to maximum at centre
Option C: varies parabolically with maximum at the centre
Option D: none of the above
Correct Answer: varies parabolically with maximum at the centre ✔
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Option A: laminar flow
Option B: transition flow
Option C: turbulent flow
Option D: critical flow
Correct Answer: turbulent flow ✔
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Option A: head loss and discharge are same in two systems
Option B: length of pipe and discharge are same in two systems
Option C: friction factor and length are same in two systems
Option D: length and diameter are same in two systems
Correct Answer: head loss and discharge are same in two systems ✔
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Option A: the length of pipe
Option B: the viscosity of fluid
Option C: the bulk modulus for the fluid
Option D: the original head
Correct Answer: the bulk modulus for the fluid ✔
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Option A: (1) and (2)
Option B: (1) and (3)
Option C: (2) and (3)
Option D: (1), (2) and (3)
Correct Answer: (2) and (3) ✔
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Option A: 16/Re
Option B: 32/ Re
Option C: 64/ Re
Option D: none of the above where R,, is Reynolds number
Correct Answer: 64/ Re ✔
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Option A: 1/3
Option B: 1/4
Option C: 1/2
Option D: 2/3
Correct Answer: 1/3 ✔
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Option A: from reservoir A to reservoirs B and C
Option B: from reservoir B to reservoirs C and A
Option C: from reservoir C to reservoirs A and B
Option D: unpredictable
Correct Answer: from reservoir C to reservoirs A and B ✔
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Option A: (1) and (3)
Option B: (2) and (3)
Option C: (1) and (4)
Option D: (2) and (4)
Correct Answer: (2) and (4) ✔
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Option A: d > m > e
Option B: d > e > m
Option C: e > m > d
Option D: e > d > m
Correct Answer: e > d > m ✔
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Option A: 0.40 cm
Option B: 0.20 cm
Option C: 0.10 cm
Option D: 0.05 cm
Correct Answer: 0.20 cm ✔
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Option A: less than d
Option B: between d and 1.5 d
Option C: between 1.5 d and 2d
Option D: greater than 2d
Correct Answer: less than d ✔
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Option A: 32 km
Option B: 20 km
Option C: 8 km
Option D: 4 km
Correct Answer: 32 km ✔
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Option A: 1 m
Option B: 10m
Option C: 100m
Option D: none of the above
Correct Answer: 100m ✔
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Option A: the head loss is same through each pipe
Option B: the discharge is same through each pipe
Option C: a trial solution is not necessary
Option D: the discharge through each pipe is added to obtain total discharge
Correct Answer: the discharge is same through each pipe ✔
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Option A: less than 1
Option B: between 1 and 100
Option C: 160
Option D: 200
Correct Answer: 160 ✔
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Option A: always above the centre line of pipe
Option B: never above the energy grade line
Option C: always sloping downward in the direction of flow
Option D: all of the above
Correct Answer: never above the energy grade line ✔
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Option A: always occurs before a separation point
Option B: always occurs after a separation point
Option C: is a region of high pressure intensity
Option D: none of the above
Correct Answer: always occurs after a separation point ✔
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Option A: less than 1 m/sec
Option B: 1 m/sec
Option C: 1.5 m/sec
Option D: 2 m/sec
Correct Answer: 1 m/sec ✔
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Option A: zero at the pipe wall
Option B: maximum at the pipe wall
Option C: independent of shear stress
Option D: none of the above
Correct Answer: zero at the pipe wall ✔
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Option A: 1/3 R
Option B: 1/2 R
Option C: 2/3 R
Option D: 3/4R
Correct Answer: 1/3 R ✔
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Option A: the pressure intensity reaches a minimum
Option B: the cross-section of a channel is reduced
Option C: the boundary layer comes to rest
Option D: all of the above
Correct Answer: the boundary layer comes to rest ✔
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Option A: 0.1
Option B: 0.01
Option C: 0.001
Option D: 0.0001
Correct Answer: 0.01 ✔
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Option A: a circular disc or plate held normal to flow
Option B: a sphere
Option C: a cylinder
Option D: an airfoil
Correct Answer: an airfoil ✔
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Option A: highest intensity of pressure occurs around the circumference at right angles to flow
Option B: lowest pressure intensity occurs at front stagnation point
Option C: lowest pressure intensity occurs at rear stagnation point
Option D: total drag is zero
Correct Answer: total drag is zero ✔
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Option A: log-log plot of friction factor against Reynolds number
Option B: log-log plot of relative roughness against Reynolds number
Option C: semi-log plot of friction factor against Reynolds number
Option D: semi-log plot of friction factor against relative roughness
Correct Answer: log-log plot of friction factor against Reynolds number ✔
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Option A: velocity
Option B: discharge
Option C: head
Option D: pressure
Correct Answer: discharge ✔
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Option A: x”7
Option B: x,/2
Option C: x4/5
Option D: x3/5
Correct Answer: x4/5 ✔
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Option A: constant over the cross section
Option B: parabolic distribution across the section
Option C: zero at the mid plane and varies linearly with distance from mid plane
Option D: zero at plates and increases linearly to midpoint
Correct Answer: zero at the mid plane and varies linearly with distance from mid plane ✔
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Option A: Lower critical Reynolds number is of no practical significance in pipe flow problems.
Option B: Upper critical Reynolds number is significant in pipe flow problems.
Option C: Lower critical Reynolds number has the value 2000 in pipe flow
Option D: Upper critical Reynolds number is the number at which turbulent flow changes to laminar flow
Correct Answer: A. Lower critical Reynolds number is of no practical significance in pipe flow problems ✔
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Option A: 1.00
Option B: 0.855
Option C: 0.7H
Option D: 0.611
Correct Answer: 1.00 ✔
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Option A: slightly less
Option B: slightly more
Option C: nearly half
Option D: equal
Correct Answer: slightly less ✔
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Option A: is independent of Reynolds number
Option B: decreases with higher Reynolds number
Option C: is equal to the coefficient of discharge of venturimeter
Option D: none of the above
Correct Answer: is equal to the coefficient of discharge of venturimeter ✔
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Option A: H1/2
Option B: H3’2
Option C: H5/2
Option D: H5’4 where H is head
Correct Answer: H5/2 ✔
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Option A: pipe diameter
Option B: throat diameter
Option C: angle of diverging section
Option D: both pipe diameter as well as throat diameter
Correct Answer: pipe diameter ✔
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Option A: current meter
Option B: venturimeter
Option C: pitot tube
Option D: hotwire anemometer
Correct Answer: venturimeter ✔
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Option A: discharge
Option B: velocity of gas
Option C: pressure intensity of gas
Option D: pressure intensity of liquid
Correct Answer: velocity of gas ✔
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Option A: can be zero
Option B: is never zero
Option C: is always zero
Option D: is independent of coordinates
Correct Answer: can be zero ✔
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Option A: steady flow
Option B: laminar flow
Option C: uniform flow
Option D: turbulent flow
Correct Answer: steady flow ✔
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Option A: free vortex motion
Option B: forced vortex motion
Option C: free vortex at center and forced vortex outside
Option D: forced vortex at center and free vortex outside
Correct Answer: forced vortex at center and free vortex outside ✔
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Option A: steady flow
Option B: uniform flow
Option C: incompressible flow
Option D: frictionless flow
Correct Answer: steady flow ✔
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Option A: 22.5 m/sec
Option B: 33 m/sec
Option C: 40 m/sec
Option D: 90 m/sec
Correct Answer: 40 m/sec ✔
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Option A: a function of temperature only
Option B: a physical property of the fluid.
Option C: dependent on the flow
Option D: independent of the flow
Correct Answer: dependent on the flow ✔
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Option A: product of pressure intensity at its centroid and area
Option B: force on a vertical projection of the curved surface
Option C: weight of liquid vertically above the curved surface
Option D: force on the horizontal projection of the curved surface
Correct Answer: force on a vertical projection of the curved surface ✔
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Option A: the pressure throughout the liquid mass is atmospheric
Option B: there will be vacuum in the liquid
Option C: the pressure in the liquid mass is greater than hydrostatic pressure
Option D: none of the above
Correct Answer: the pressure throughout the liquid mass is atmospheric ✔
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Option A: 5kN
Option B: lOkN
Option C: 15 kN
Option D: 20 kN
Correct Answer: lOkN ✔
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Option A: centre of gravity and centre of buoy-ancy
Option B: centre of gravity and metacentre
Option C: centre of buoyancy and metacentre
Option D: free surface and centre of buoyancy
Correct Answer: centre of gravity and metacentre ✔
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Option A: coincides with the centre of gravity
Option B: coincides with the centroid of the volume of fluid displaced
Option C: remains above the centre of gravity
Option D: remains below the centre of gravity
Correct Answer: coincides with the centroid of the volume of fluid displaced ✔
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Option A: PA
Option B: pA sin 9
Option C: pA cos 9
Option D: pA tan 9
Correct Answer: PA ✔
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Option A: 4 kN/m2
Option B: 10 kN/m2
Option C: 12 kN/m2
Option D: 14 kN/m2
Correct Answer: 4 kN/m2 ✔
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