Reynold's number
Froude's number
Weber's number
Mach number
D. Mach number
Sinθ
1/Sinθ
Cosθ
1/Cosθ
Directly proportional to (radius)2
Inversely proportional to (radius)2
Directly proportional to (radius)4
Inversely proportional to (radius)4
Q = Cd × bH₁ × √(2gh)
Q = Cd × bH2 × √(2gh)
Q = Cd × b (H2 - H1) × √(2gh)
Q = Cd × bH × √(2gh)
Sub-sonic flow
Sonic flow
Super-sonic flow
Hyper-sonic flow
Less man the vapour pressure over the plane surface
Equal to the vapour pressure over the plane surface
Greater than the vapour pressure over the plane surface
Zero
Maximum
Minimum
Zero
Nonzero finite
Pressure of liquid
Discharge of liquid
Pressure difference between two points in a channel
Pressure difference between two points in a pipe
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
Venturimeter
Orifice plate
Hot wire anemometer
Pitot tube
Steady
Unsteady
Laminar
Vortex
Equal to
Less than
More than
None of these
Quasi-static
Steady state
Laminar
Uniform
U-tube with water
Inclined U-tube
U-tube with mercury
Micro-manometer with water
Increase in viscosity of gas
Increase in viscosity of liquid
Decrease in viscosity of gas
Decrease in viscosity of liquid
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
Gravity, pressure and viscous
Gravity, pressure and turbulent
Pressure, viscous and turbulent
Gravity, viscous and turbulent
Pressure
Flow
Shape
Volume
Velocity of liquid
Pressure of liquid
Area of mouthpiece
Length of mouthpiece
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
The direction and magnitude of the velocity at all points are identical
The velocity of successive fluid particles, at any point, is the same at successive periods of time
The magnitude and direction of the velocity do not change from point to point in the fluid
The fluid particles move in plane or parallel planes and the streamline patterns are identical in each pleasure
Less than 2000
Between 2000 and 2800
More than 2800
None of these
0.34 times
0.67 times
0.81 times
0.95 times
Avoid interruption in the flow
Increase discharge
Increase velocity
Maintain pressure difference
Steady uniform
Non-steady non-uniform
Non-steady uniform
Steady non-uniform
1 and 2.5
2.5 and 4
4 and 6
1 and 6
0° C
0° K
4° C
100° C
14π R1/2/15Cd × a √(2g)
14π R3/2/15Cd × a √(2g)
14π R5/2/15Cd × a √(2g)
14π R7/2/15Cd × a √(2g)
Steady
Unsteady
Uniform
Laminar
dp/ρ + g.dz + v.dv = 0
dp/ρ - g.dz + v.dv = 0
ρ.dp + g.dz + v.dv = 0
ρ.dp - g.dz + v.dv = 0
Low pressure
High pressure
Low velocity
High velocity