Is steady
Is one dimensional
Velocity is uniform at all the cross sections
All of the above
D. All of the above
(2/3) × Cd (L - nH) × √(2gh)
(2/3) × Cd (L - 0.1nH) × √(2g) × H3/2
(2/3) × Cd (L - nH) × √(2g) × H²
(2/3) × Cd (L - nH) × √(2g) × H5/2
Centre of pressure
Centre of buoyancy
Metacentre
None of these
Bourdon tube
Pirani Gauge
Micro-manometer
Lonisation gauge
19.24 kPa
29.24 kPa
39.24 kPa
49.24 kPa
Directly proportional to the area of the vessel containing liquid
Directly proportional to the depth of liquid from the surface
Directly proportional to the length of the vessel containing liquid
Inversely proportional to the depth of liquid from the surface
Cohesion
Adhesion
Viscosity
Surface tension
Pressure in pipes, channels etc.
Atmospheric pressure
Very low pressure
Difference of pressure between two points
Velocity of approach
Lower critical velocity
Higher critical velocity
None of these
One dimensional flow
Uniform flow
Steady flow
Turbulent flow
More
Less
Same
More or less depending on size of glass tube
Remain same
Decreases
Increases
None of these
Less than 2000
Between 2000 and 4000
More than 4000
Less than 4000
Same as
Less than
More than
None of these
Avoid the tendency of breaking away the stream of liquid
To minimise frictional losses
Both (A) and (B)
None of these
Equal to
Directly proportional
Inversely proportional
None of these
Metacentre
Center of pressure
Center of buoyancy
Center of gravity
Tensile stress
Compressive stress
Shear stress
Bending stress
Any weight, floating or immersed in a liquid, is acted upon by a buoyant force
Buoyant force is equal to the weight of the liquid displaced
The point through which buoyant force acts, is called the center of buoyancy
Center of buoyancy is located above the center of gravity of the displaced liquid
Gauge pressure
Absolute pressure
Positive gauge pressure
Vacuum pressure
Steady
Unsteady
Laminar
Vortex
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
Less than 2000
Between 2000 and 4000
More than 4000
Less than 4000
0° C
0° K
4° C
100° C
0.375
0.5
0.707
0.855
Capillary tube method
Orifice type viscometer
Rotating cylinder method
All of these
Neutral
Stable
Unstable
None of these
Fluids are capable of flowing
Fluids conform to the shape of the containing vessels
When in equilibrium, fluids cannot sustain tangential forces
When in equilibrium, fluids can sustain shear forces
Lift
Drag
Stagnation pressure
Bulk modulus
(8/15) Cd. 2g. H
(8/15) Cd. 2g. H3/2
(8/15) Cd. 2g. H²
(8/15) Cd. 2g. H5/2
0.5 a. √2gH
0.707 a. √2gH
0.855 a. √2gH
a. √2gH