A flow whose streamline is represented by a curve is called two dimensional flow.
The total energy of a liquid particle is the sum of potential energy, kinetic energy and pressure energy.
The length of divergent portion in a Venturimeter is equal to the convergent portion.
A pitot tube is used to measure the velocity of flow at the required point in a pipe.
C. The length of divergent portion in a Venturimeter is equal to the convergent portion.
Decreases
Increases
Remain same
None of these
Specific gravity of liquids
Specific gravity of solids
Specific gravity of gases
Relative humidity
One-dimensional flow
Two-dimensional flow
Three-dimensional flow
Four-dimensional flow
0.384 Cd × L × H1/2
0.384 Cd × L × H3/2
1.71 Cd × L × H1/2
1.71 Cd × L × H3/2
Specific weight
Specific mass
Specific gravity
Specific density
400 kg/cm²
4000 kg/cm²
40 × 10⁵ kg/cm²
40 × 10⁶ kg/cm²
Pascal's law
Archimedess principle
Principle of floatation
Bernoulli's theorem
Meta centre should be above e.g.
Centre of buoyancy and e.g. must lie on same vertical plane
A righting couple should be formed
All of the above
wA
wx
wAx
wAx/sinθ
One dimensional flow
Streamline flow
Steady flow
Turbulent flow
Gauge pressure + atmospheric pressure
Gauge pressure - atmospheric pressure
Atmospheric pressure - gauge pressure
Gauge pressure - vacuum pressure
0.3 to 0.45
0.50 to 0.75
0.75 to 0.95
0.95 to 1.0
One dimensional flow
Uniform flow
Steady flow
Turbulent flow
Acts in the plane of the interface normal to any line in the surface
Is also known as capillarity
Is a function of the curvature of the interface
Decreases with fall in temperature
One
Two
Three
Four
Measure the velocity of a flowing liquid
Measure the pressure of a flowing liquid
Measure the discharge of liquid flowing in a pipe
Measure the pressure difference of liquid flowing between two points in a pipe line
Up-thrust
Buoyancy
Center of pressure
All the above are correct
Underground flow
Flow past tiny bodies
Flow of oil in measuring instruments
All of these
Wake
Drag
Lift
Boundary layer
A × √(m × i)
C × √(m × i)
AC × √(m × i)
mi × √(A × C)
Gauge pressure
Absolute pressure
Positive gauge pressure
Vacuum pressure
N-m/s2
N-s/m2
Poise
Stoke
Reynold's number
Froude's number
Mach number
Euler's number
dQ/Q = 3/2 × (dH/H)
dQ/Q = 2 × (dH/H)
dQ/Q = 5/2 × (dH/H)
dQ/Q = 3 × (dH/H)
Maximum
Minimum
Zero
Nonzero finite
μ π³ N² R² /1800 t
μ π³ N² R⁴ /1800 t
μ π³ N² R² /3600 t
μ π³ N² R⁴ /3600 t
N/mm2
N/m2
Head of liquid
All of these
Plus
Minus
Divide
None of these
Less than
More than
Equal to
None of these
500 kg
1000 kg
1500 kg
2000 kg