Surface tension
Compressibility
Capillarity
Viscosity
A. Surface tension
Low pressure
High pressure
Moderate pressure
Vacuum pressure
103 kN/m2
10.3 m of water
760 mm of mercury
All of these
Remains constant
Increases
Decreases
Depends upon mass of liquid
1.84 (L - 0.1nH)H3/2
1.84 (L - nH)H2
1.84 (L - 0.1nH)H5/2
1.84 (L - nH)H3
Gas law
Boyle's law
Charles law
Pascal's law
Metres² per sec
kg-sec/metre
Newton-sec per metre²
Newton-sec per meter
Notch
Weir
Mouthpiece
Nozzle
Compressibility
Surface tension
Cohesion
Adhesion
0.0116 stoke
0.116 stoke
0.0611 stoke
0.611 stoke
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
Has constant viscosity
Has zero viscosity
Is in compressible
None of the above
One-dimensional flow
Two-dimensional flow
Three-dimensional flow
Four-dimensional flow
Shear stress and the rate of angular distortion
Shear stress and viscosity
Shear stress, velocity and viscosity
Pressure, velocity and viscosity
Real fluid
Ideal fluid
Newtonian fluid
Non-Newtonian fluid
Velocity of flow is very high
Discharge is difficult to measure
Mach number is between 1 and 6
None of these
100 litres
250 litres
500 litres
1000 litres
Higher
Lower
Same as
None of these
Sum
Different
Product
Ratio
Centre of gravity
Centre of depth
Centre of pressure
Centre of immersed surface
(2A√H₁)/(Cd × a√2g)
(2AH₁)/(Cd × a√2g)
(2AH₁3/2)/(Cd × a√2g)
(2AH₁²)/(Cd × a√2g)
0.375
0.5
0.707
0.855
Viscosity of a fluid is that property which determines the amount of its resistance to a shearing force
Viscosity is due primarily to interaction between fluid molecules
Viscosity of liquids decreases with increase in temperature
Viscosity of liquids is appreciably affected by change in pressure
Steady uniform
Non-steady non-uniform
Non-steady uniform
Steady non-uniform
One-fourth of the total supply head
One-third of the total supply head
One-half of the total supply head
Two-third of the total supply head
Remains constant
Increases
Decreases
Depends upon mass of liquid
One dimensional flow
Streamline flow
Steady flow
Turbulent flow
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
wA
wx
wAx
wAx/sinθ
Equal to
Less than
More than
None of these
Higher
Lower
Same
Higher/lower depending on temperature