Flow of Fluids Flashcards
A fluid is one which
A. Cannot remain at rest under the action of shear force
B. COntinuously expands till it fills any container
C. Is incompressible
D. Permanently resists distortion
A. Cannot remain at rest under the action of shear force
In an incompressible fluid density
A. Is greatly affected by moderate changes in pressure
B. Is greatly affected only by moderate changes in temperature
C. Remains unaffected with moderate change in temperature and pressure
D. Is sensible to changes in both temperature and pressure
C. Remains unaffected with moderate change in temperature and pressure
Potential flow is the flow of
A. Compressible fluids with shear
B. Compressible fluids with no shear
C. Incompressible fluids with shear
D. Incompressible flds with no shear
D. Incompressible flds with no shear
Potential flow is characterized by
A. Irrotational and frictioless flow
B. Irrotational and frictional flow
C. One in which dissipation of mechanical energy into heat occurs
D. The formation of eddies within the stream
A. Irrotational and frictionless flow
Newton’s law of viscosity relates
A. Shear stress and velocity
B. Velocity gradient and pressure intensity
C. Shear stress and rate of angular deformation in a fluid
D. Pressure gradient and rate of angular deformation
C. Shear stress and rate of angular deformation in a fluid
Dimension of viscosity is
A. M/LT
B. ML/T
C. MLT/T
D. MLT
A. M/LT
Poise is converted into stoke by
A. Multiplying with density (g/cc)
B. Dividing with density (g/cc)
C. Multiplying with specific gravity
D. Dividing with specific gravity
B. Dividing with density (g/cc)
Dimension of kinematic viscosity is
A. M/L²
B. L²/T
C. L²T
D. L²T²
B. L²/T
With increase in the temperature, viscosity of a liquid
A. Increases
B. Decreases
C. Remains constant
D. First decreases and then increases
B. Decreases
For water, when the pressure increases, the viscosity
A. Also increases
B. Decreases
C. Remains constant
D. First decreases and then increases
D. First decreases and then increases
The pressure intensity is the same in all direction at a point in a fluid
A. Only when the fluid is frictioless
B. Only when the fluid is at rest having zero velocity
C. When there is no motion of one fluid layer relative to an adjacent layer
D. Regardless of the motion of one fluid layer relative to an adjacent layer
C. When there is no motion of one fluid layer relative to an adjacent layer
Choose the set of pressure intensities that are equivalent.
A. 4.33 psi, 10 ft H2O, 8.83 inHg
B. 4.33 psi, 10 ft H2O, 20.7 inHg
C. 10 psi, 19.7 ft H2O, 23.3 inHg
D. 10 psi, 19.7 ft H2O, 5.3 inHg
A. 4.33 psi, 10 ft H2O, 8.83 inHg
For a fluid rotating at constant angular velocity about vertical axis as a rigid body, the pressure intensity varies as the
A. Square of the radial distance
B. Radial distance linearly
C.Averse of the radial distance
D. Elevation along vertical direction
A. Square of the radial distance
The center of pressure is
A. Always below the centroid of the area
B. Always above the centroid of the arrea
C. A point on the line of action of the resultant force
D. At the centroid of the submerge area
C. A point on he line of action of the resultant force
A rectangular surace 3’ x 4’ has the lower 3 edge horizontal and 6’ below a free oil surface (sp. gr. 0.8). The surface inclination is 300 with the horizontal. The force in one side of the surace is (y = specific weight of water):
A. 39.6y
B. 48y
C. 49.2y
D. 58y
B. 48y
A stream tube is that which has ______ cross-section entirely bounded by a stream lines.
A. A circular
B. Any convenient
C. A small
D. A large
B. Any convenient
Mass velocity is independent of temperature and pressure when the flow is
A. Unsteady through uncharged corss-section
B. Steady through changing cross-section
C. Steady and the cross-section is unchanged
D. Usteady and the cross-section is changed
C. Steady and the cross-section is unchanged
In turbulent flow,
A. The fluid paricles move in an orderly manner
B. Momentum transfer is on molecular scale only
C. Shear stress is cause more efectively by cohesion than momentum transfer
D. Shear stresses are generally larger than in a similar laminar flow
D. Shear stresses are generally larger than in a similar laminar flow
Turbulent flow generally occurs for cases involving
A. Highly viscous fluid
B. Very narrow passages
C. Very slow motion
D. None of these
D. None of these
An ideal fluid is
A. Frictionless and incompressible
B. One which obeys Newton’s law of viscosity
C. Highly viscous
D None of these
A. Frictionless and incompressible
Steady flow occurs when
A. Conditions change steadily with time
B. Conditios are the same at the adjacent points at any instant
C. Conditions do not change with time at any point
D. Rate of change of velocity is constant
C. Conditions do not change with time at any point
Which of the following must be followed by the flw of fluid (real or ideal)?
I. Newton’s law of viscosity
II. Newton’s second law of motion
III. The continuity equation
IV. Velocity of boundary must be zero relative to boundary
V. Fluid cannot penetrate a boundary
A. I, II, III
B. II, III, V
C. I, II, V
D. II, III, V
B. II, III, V
Discharge (ft³/sec) from a 24-inch pipe of water at 10 ft/sec will be
A. 7.65
B. 32.36
C. 48.22
D.125.6
D. 125.6
The unit velocity head is
A. ft-lb/sec
B. ft-lb/ft³
C. ft-lbf/lbm
D. ft-lbf/sec
C. ft-lbf/lbm
Bernoulli’s equation describes
A. Mechanical energy balance in potetial flow
B. Kinetic energy balance in laminar flow
C. Mechanical energy balance in turbulent flow
D. Mechanical energy balance in boundary layer
A. Mechanical energy balance in potential flow
The kinetic energy correction factor for velocity distribution of laminar flow is
A. 0.5
B. 1.66
C. 1
D. 2
B. 1.66
The momentum correction factor for the velocity distrbution of laminar flow is
A. 1.3
B. 1.66
C. 2.5
D. None of these
D. None of these
The loss due to sudden expansion is
A. V1²-V2²/2gc
B. (V1-V2)³/2gc
C. V1-V2/2gc
D. None of these
B. (V1-V2)³/2gc
The loss due to sudden contraction is proportional to
A. Velocity
B. Velocity head
C. Turbulence
D. None of these
B. Velocity head
The value of critical Reynolds number for pipe flow is
A. 1300
B. 10,000
C. 100,000
D. None of these
A. 1300
Reynolds number flow of wate at room temperature through 2 cm diameter pipe at average velocity of 5 cm/s is around
A. 2000
B. 10
C. 100
D. 1000
D. 1000
Shear stress in a fluid flowing in a round pipe
A. Varies parabolically across the cross-section
B. Remains constant over the cross-section
C. Is zero at the center and varies linearly with the radius
D. Is zero at the wall and increase linearly to the center
C. Is zero at the center and varies linearly with the radius
Discharge in laminar flow through a pipe varies
A. As the square of the radius
B. Inversely as the pressure drop
C. Inversely as the velocity
D. As the square of the diameter
A. As the square of the radius
Boundary layer separation is caused by
A. Reduction of pressure below vapor pressure
B. Reduction of pressure gradient to zero
C. An adverse pressure gradient
D. Reduction of boundary layer thickness to zero
C. An adverse pressure gradient
The friction factor for turbulent flow in a hydraulically smooth pipe
A. Depends only on Reynolds number
B. Does not depend on Reynolds number
C. Depends on the roughness
D. None of these
A. Depends only on Reynolds number
For a given Reynolds number, in hydraulically smooth pipe, further smoothing
A. Brings about no further reduction of friction factor
B. Increases the friction factor
C. Decreases the friction factor
D. None of these
A. Brings about no further reduction of friction factor
Hydraulic radius is the ratio of
A. Wetted perimeter to flow area
B. Flow area to wetted perimeter
C. Flow area to square of wetted perimeter
D. Square root of flow area to wetted perimeter
B. Flow area to wetted perimeter
Hydraulic radius of 6” x 12” c/s is
A. 2”
B. 0.5”
C. 1.5”
D. None of these
A. 2”
Reynolds number is the ratio of
A. Viscous forces to gravity forces
B. Inertial forces to viscous forces
C. Viscous force to inertial forces
D. Inertial forces to gravity forces
B. Inertial forces to viscous forces