Triangular
Rectangular
Square
Trapezoidal
D. Trapezoidal
The head loss for all the pipes is same
The total discharge is equal to the sum of discharges in the various pipes
The total head loss is the sum of head losses in the various pipes
Both (A) and (B)
Equal to
Less than
More than
None of these
Head of water (h)
h²
V/T
h/2
The center of gravity of the body and the metacentre
The center of gravity of the body and the center of buoyancy
The center of gravity of the body and the center of pressure
Center of buoyancy and metacentre
It gives maximum discharge for a given cross-sectional area and bed slope
It has minimum wetted perimeter
It involves lesser excavation for the designed amount of discharge
All of the above
Pressure
Flow
Shape
Volume
Remains constant
Increases
Decreases
Depends upon mass of liquid
Dissolved air
Dissolved salt
Suspended matter
All of the above
Actual velocity of jet at vena contracta to the theoretical velocity
Loss of head in the orifice to the head of water available at the exit of the orifice
Loss of head in the orifice to the head of water available at the exit of the orifice
Area of jet at vena-contracta to the area of orifice
A triangle
A paraboloid
An ellipse
None of these
Less than
More than
Equal to
None of these
Less than
More than
Equal to
None of these
Steady flow
Uniform flow
Streamline flow
Turbulent flow
Velocity of approach
Lower critical velocity
Higher critical velocity
None of these
Vertical upward force through e.g. of body and center line of body
Buoyant force and the center line of body
Midpoint between e.g. and center of buoyancy
All of the above
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
Ratio of absolute viscosity to the density of the liquid
Ratio of density of the liquid to the absolute viscosity
Product of absolute viscosity and density of the liquid
Product of absolute viscosity and mass of the liquid
Constant
Variable
Zero
Zero under limiting conditions
w1a1 = w2a2
w1v1 = w2v2
a1v1 = a2v2
a1/v1 = a2/v2
Same as
Less than
More than
None of these
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
1/RN
4/RN
16/RN
64/RN
Less than 2000
Between 2000 and 4000
More than 4000
Less than 4000
A compressible
An incompressible
Both A and B
None of these
Z + p/w + v²/2g = constant
Z + p/w - v²/2g = constant
Z - p/w + v²/2g = constant
Z - p/w - v²/2g = constant
Adhesion
Cohesion
Surface tension
Viscosity
0.417 H5/2
1.417 H5/2
4.171 H5/2
7.141 H5/2
Quasi-static
Steady state
Laminar
Uniform
(q/g)1/2
(q²/g)1/3
(q³/g)1/4
(q⁴/g)1/5
100 litres
250 litres
500 litres
1000 litres