Decrease
Increase
Remain unchanged
Depend upon the characteristics of liquid
A. Decrease
0.62
0.76
0.84
0.97
Steady flow
Turbulent flow
Vortex flow
Uniform flow
Sub-sonic velocity
Super-sonic velocity
Lower critical velocity
Higher critical velocity
Planes of the body are completely smooth
Space around the body is completely filled with the fluid
Fluid particles do not exert any influence on one another
All of the above
0.384 Cd × L × H1/2
0.384 Cd × L × H3/2
1.71 Cd × L × H1/2
1.71 Cd × L × H3/2
A flow whose streamline is represented by a curve is called two dimensional flow.
The total energy of a liquid particle is the sum of potential energy, kinetic energy and pressure energy.
The length of divergent portion in a Venturimeter is equal to the convergent portion.
A pitot tube is used to measure the velocity of flow at the required point in a pipe.
Wake
Drag
Lift
Boundary layer
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 patterns are identical in each plane
Atmospheric pressure
Pressure in pipes and channels
Pressure in Venturimeter
Difference of pressures between two points in a pipe
Velocity of approach
Lower critical velocity
Higher critical velocity
None of these
2gH
H × √(2g)
2g × √H
√(2gh)
Decreases
Increases
Remain same
None of these
At the Centroid
Above the Centroid
Below the Centroid
At metacentre
Friction loss and flow
Length and diameter
Flow and length
Friction factor and diameter
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 patterns are identical in each pleasure
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
1
1000
100
101.9
Specific weight
Specific volume
Specific speed
Specific gravity
Adhesion
Cohesion
Viscosity
Compressibility
Less than
More than
Equal
None of these
Is steady and uniform
Takes place in straight line
Takes place in curve
Takes place in one direction
Principle of conservation of mass holds
Velocity and pressure are inversely proportional
Total energy is constant throughout
The energy is constant along a streamline but may vary across streamlines
Velocity of liquid
Pressure of liquid
Area of mouthpiece
Length of mouthpiece
Sub-sonic velocity
Super-sonic velocity
Lower critical velocity
Higher critical velocity
Shear stress and the rate of angular distortion
Shear stress and viscosity
Shear stress, velocity and viscosity
Pressure, velocity and viscosity
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
Surface tension
Compressibility
Capillarity
Viscosity
1.84 LH1/2
1.84 LH
1.84 LH3/2
1.84 LH5/2
1 %
1.5 %
2 %
2.5 %
It is incompressible
It has uniform viscosity
It has zero viscosity
It is at rest