Actual velocity of jet at vena-contracta to the theoretical velocity
Area of jet at vena-contracta to the area of orifice
Loss of head in the orifice to the head of water available at the exit of the orifice
Actual discharge through an orifice to the theoretical discharge
C. Loss of head in the orifice to the head of water available at the exit of the orifice
10 m/sec
25 m/sec
2 m/sec
50 m/sec
Real fluid
Ideal fluid
Newtonian fluid
Non-Newtonian fluid
Sum
Different
Product
Ratio
Equal to
Less than
More than
None of these
1
5
7
6
ML°T⁻²
ML°T
ML r²
ML²T²
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
Effects
Does not effect
Both A and B
None of these
Wake
Drag
Lift
Boundary layer
Pressure
Discharge
Velocity
Volume
The bodies A and B have equal stability
The body A is more stable than body B
The body B is more stable than body A
The bodies A and B are unstable
K.ρ
K/ρ
ρ/K
None of these
Resistance to shear stress is small
Fluid pressure is zero
Linear deformation is small
Only normal stresses can exist
Total energy per unit discharge
Total energy measured with respect to the datum passing through the bottom of the channel
Total energy measured above the horizontal datum
Kinetic energy plotted above the free surface of water
Pascal
Poise
Stoke
Faraday
Varies as the square of the radial distance
Increases linearly as its radial distance
Increases as the square of the radial distance
Decreases as the square of the radial distance
Up-thrust
Buoyancy
Center of pressure
All the above are correct
Equal to
One-fourth
One-third
One-half
Mach number
Froude number
Reynoldss number
Weber's number
Law of gravitation
Archimedes principle
Principle of buoyancy
All of the above
Inertia force
Viscous force
Gravity force
All of these
To control the pressure variations due to rapid changes in the pipe line flow
To eliminate water hammer possibilities
To regulate flow of water to turbines by providing necessary retarding head of water
All of the above
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
Kinematic viscosity in C. G. S. units
Kinematic viscosity in M. K. S. units
Dynamic viscosity in M. K. S. units
Dynamic viscosity in S. I. units
Pressure force
Elastic force
Gravity force
Surface tension force
Double
Four times
Eight times
Sixteen times
At the inlet
At the outlet
At the summit
At any point between inlet and outlet
At the centre of gravity
Above the centre of gravity
Below be centre of gravity
Could be above or below e.g. depending on density of body and liquid
Higher
Lower
Same as
None of these
w1a1 = w2a2
w1v1 = w2v2
a1v1 = a2v2
a1/v1 = a2/v2