Quasi-static
Steady state
Laminar
Uniform
D. Uniform
dQ/Q = 3/2 × (dH/H)
dQ/Q = 2 × (dH/H)
dQ/Q = 5/2 × (dH/H)
dQ/Q = 3 × (dH/H)
Mach number
Froude number
Reynolds number
Weber's number
(v₁ - v₂)²/g
(v₁² - v₂²)/g
(v₁ - v₂)²/2g
(v₁² - v₂²)/2g
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
Low pressure
High pressure
Low velocity
High velocity
Gravitational force is equal to the up-thrust of the liquid
Gravitational force is less than the up-thrust of the liquid
Gravitational force is more than the up-thrust of the liquid
None of the above
Straight line
Parabolic curve
Hyperbolic curve
Elliptical
Orifice
Notch
Weir
Dam
Pressure
Velocity
Square of velocity
Cube of velocity
The nature of the liquid and the solid
The material which exists above the free surface of the liquid
Both of die above
Any one of the above
It is easier to see through the glass tube
Glass tube is cheaper than a metallic tube
It is not possible to conduct this experiment with any other tube
All of the above
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
Width of channel at the top is equal to twice the width at the bottom
Depth of channel is equal to the width at the bottom
The sloping side is equal to half the width at the top
The sloping side is equal to the width at the bottom
K.ρ
K/ρ
ρ/K
None of these
Double
Four times
Eight times
Sixteen times
Less than
More than
Equal to
None of these
Horizontal line
Inclined line with flow upwards
Inclined line with flow downwards
Any direction and in any location
Path line
Stream line
Steak line
Potential line
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
(μπ²N/60t) × (R₁ - R₂)
(μπ²N/60t) × (R₁² - R₂²)
(μπ²N/60t) × (R₁³ - R₂³)
(μπ²N/60t) × (R₁⁴ - R₂⁴)
0.0116 stoke
0.116 stoke
0.0611 stoke
0.611 stoke
Atmospheric pressure
Gauge pressure
Absolute pressure
Mean pressure
Sub-sonic flow
Sonic flow
Super-sonic flow
Hyper-sonic flow
Narrow crested weir
Broad crested weir
Ogee weir
Submerged weir
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
Q = (2/3) Cd × b × √(2g) × (H2 - H1)
Q = (2/3) Cd × b × √(2g) × (H2 1/2 - H1 1/2)
Q = (2/3) Cd × b × √(2g) × (H2 3/2 - H1 3/2)
Q = (2/3) Cd × b × √(2g) × (H2 2 - H1 2)
π w ω² r²/4g
π w ω² r³/4g
π w ω² r⁴/4g
π w ω² r²/2g
Less than
More than
Equal to
None of these
Surface tension
Cohesion of the liquid
Adhesion of the liquid molecules and the molecules on the surface of a solid
All of the above
Unity
Greater than unity
Greater than 2
Greater than 4