Length of both the pipes is same
Diameter of both the pipes is same
Loss of head and discharge of both the pipes is same
Loss of head and velocity of flow in both the pipes is same
C. Loss of head and discharge of both the pipes is same
1
1.2
0.8
0.75
Is steady and uniform
Takes place in straight line
Takes place in curve
Takes place in one direction
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
Centre of gravity
Centre of pressure
Metacentre
Centre of buoyancy
Higher than the surface of liquid
The same as the surface of liquid
Lower than the surface of liquid
Unpredictable
v²/2g
0.5v²/2g
0.375v²/2g
0.75v²/2g
Pressure in pipes, channels etc.
Atmospheric pressure
Very low pressure
Difference of pressure between two points
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
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 discontinuity, gravity forces, and wave making effect, as with ship's hulls
All of the above
tanθ = a/g
tanθ = 2 a/g
tanθ = a/2g
tanθ = a2/2g
Actual velocity of jet at vena contracta to the theoretical velocity
Area of jet at vena contracta to the area of orifice
Actual discharge through an orifice to the theoretical discharge
None of the above
Pressure in gases
Liquid discharge
Pressure in liquids
Gas velocities
High velocity
High pressure
Weak material
Low pressure
One-dimensional flow
Two-dimensional flow
Three-dimensional flow
Four-dimensional flow
It is incompressible
It has uniform viscosity
It has zero viscosity
It is at rest
Critical velocity
Velocity of approach
Sub-sonic velocity
Super-sonic velocity
When its meatcentric height is zero
When the metacentre is above C.G.
When its e.g. is below its center of buoyancy
Metacentre has nothing to do with position of e.g. for determining stability
Directly proportional to density of fluid
Inversely proportional to density of fluid
Directly proportional to (density)1/2 of fluid
Inversely proportional to (density)1/2 of fluid
9,000 kg
13,500 kg
18,000 kg
27,000 kg
Viscosity
Osmosis
Surface tension
Cohesion
51 cm
50 cm
52 cm
52.2 cm
0.384 Cd × L × H1/2
0.384 Cd × L × H3/2
1.71 Cd × L × H1/2
1.71 Cd × L × H3/2
Steady flow
Uniform flow
Free vortex
Forced vortex
Velocity of flow at the required point in a pipe
Pressure difference between two points in a pipe
Total pressure of liquid flowing in a pipe
Discharge through a pipe
At the Centroid
Above the Centroid
Below the Centroid
At metacentre
ML°T⁻²
ML°T
ML r²
ML²T²
Sub-sonic velocity
Super-sonic velocity
Lower critical velocity
Higher critical velocity
Sinθ
1/Sinθ
Cosθ
1/Cosθ
Increase in viscosity of gas
Increase in viscosity of liquid
Decrease in viscosity of gas
Decrease in viscosity of liquid
Pascal law
Newton's law of viscosity
Boundary layer theory
Continuity equation