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
C. The sloping side is equal to half the width at the top
2A × √H₁/Cd × a × √(2g)
2A × √H₂/Cd × a × √(2g)
2A × (√H₁ - √H₂)/Cd × a × √(2g)
2A × (√H3/2 - √H3/2)/Cd × a × √(2g)
Increases
Decreases
Remain unaffected
Unpredictable
ρ ω2 r2
2ρ ω2 r2
ρ ω2 r2/2
ρ ω2 r2/4
One dimensional flow
Streamline flow
Steady flow
Turbulent flow
Effects
Does not effect
Both A and B
None of these
1.84 LH1/2
1.84 LH
1.84 LH3/2
1.84 LH5/2
Pascal law
Newton's law of viscosity
Boundary layer theory
Continuity equation
0° C
0° K
4° C
20° C
Metres² per sec
kg sec/meter
Newton-sec per meter
Newton-sec² per meter
K.ρ
K/ρ
ρ/K
None of these
Buoyancy
Equilibrium of a floating body
Archimedes' principle
Bernoulli's theorem
C.G. of body
Center of pressure
Center of buoyancy
Metacentre
The resultant force acting on a floating body
The resultant force on a body due to the fluid surrounding it
Equal to the volume of liquid displaced
The force necessary to maintain equilibrium of a submerged body
Circular
Square
Rectangular
Trapezoidal
The pressure below the nappe is atmospheric
The pressure below the nappe is negative
The pressure above the nappe is atmospheric
The pressure above the nappe is negative
It has low vapour pressure
It is clearly visible
It has low surface tension
It can provide longer column due to low density
0.34 times
0.67 times
0.81 times
0.95 times
w1a1 = w2a2
w1v1 = w2v2
a1v1 = a2v2
a1/v1 = a2/v2
Pressure in pipe, channels etc.
Atmospheric pressure
Very low pressures
Difference of pressure between two points
2 meters of water column
3 meters of water column
5 meters of water column
6 meters of water Column
Atmospheric pressure
Pressure in pipes and channels
Pressure in Venturimeter
Difference of pressures between two points in a pipe
N/m
N/m2
N/m3
N-m
Venturimeter
Orifice plate
Pitot tube
Rotameter
Directly proportional to (radius)2
Inversely proportional to (radius)2
Directly proportional to (radius)4
Inversely proportional to (radius)4
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
Maximum at the centre and minimum near the walls
Minimum at the centre and maximum near the walls
Zero at the centre and maximum near the walls
Maximum at the centre and zero near the walls
1 %
1.5 %
2 %
2.5 %
1/2 × depth
1/2 × breadth
1/2 × sloping side
1/4 × (depth + breadth)
Centre of gravity
Centre of pressure
Metacentre
Centre of buoyancy
wA
wx
wAx
wA/x