l/d² = (l₁/d₁²) + (l₂/d₂²) + (l₃/d₃²)
l/d³ = (l₁/d₁³) + (l₂/d₂³) + (l₃/d₃³)
l/d⁴ = (l₁/d₁⁴) + (l₂/d₂⁴) + (l₃/d₃⁴)
l/d⁵ = (l₁/d₁⁵) + (l₂/d₂⁵) + (l₃/d₃⁵)
D. l/d⁵ = (l₁/d₁⁵) + (l₂/d₂⁵) + (l₃/d₃⁵)
Steady flow
Uniform flow
Free vortex
Forced vortex
Pressure
Velocity
Square of velocity
Cube of velocity
v₁²/2g
v₂²/2g
0.5 v₁²/2g
0.375 v₂²/2g
1000 kg
4000 kg
2000 kg
8000 kg
Wake
Drag
Lift
Boundary layer
At the inlet
At the outlet
At the summit
At any point between inlet and outlet
Energy
Work
Mass
Length
Pascal's law
Archimedess principle
D-Alembert's principle
None of these
Supersonics, as with projectile and jet propulsion
Full immersion or completely enclosed flow, as with pipes, aircraft wings, nozzles etc.
Simultaneous motion through two fluids where there is a surface of discontinuity, gravity forces, and wave making effect as with ship's hulls
All of the above
π w ω² r²/4g
π w ω² r³/4g
π w ω² r⁴/4g
π w ω² r²/2g
Capillary tube method
Orifice type viscometer
Rotating cylinder method
All of these
p = T × r
p = T/r
p = T/2r
p = 2T/r
Supersonics, as with projectile and jet propulsion
Full immersion or completely enclosed flow, as with pipes, aircraft wings, nozzles etc.
Simultaneous motion through two fluids where there is a surface of discontinuity, gravity forces, and wave making effect, as with ship's hulls
All of the above
Increases
Decreases
Remain unaffected
Unpredictable
Specific weight
Mass density
Specific gravity
None of these
Equal to
Less than
More than
None of these
Steady
Unsteady
Laminar
Vortex
Same
More
Less
None of these
The nature of the liquid and the solid
The material which exists above the free surface of the liquid
Both of die above
Any one of the above
The bodies A and B have equal stability
The body A is more stable than body B
The body B is more stable than body A
The bodies A and B are unstable
Pressure of liquid
Discharge of liquid
Pressure difference between two points in a channel
Pressure difference between two points in a pipe
Adhesion
Cohesion
Viscosity
Compressibility
Neutral
Stable
Unstable
None of these
Red wood
Say bolt
Engler
Orsat
0.405 + (0.003/H)
0.003 + (0.405/H)
0.405 + (H/0.003)
0.003 + (H/0.405)
Meta center
Center of pressure
Center of buoyancy
Center of gravity
4wd/σ cosα
σ cosα/4wd
4σ cosα/wd
wd/4σ cosα
Is uniform flow
Is steady uniform flow
Takes place in straight lines
Involves zero transverse component of flow
Has the dimensions of 1/pressure
Increases with pressure
Is large when fluid is more compressible
Is independent of pressure and viscosity
Dynamic viscosity/density
Dynamic viscosity × density
Density/dynamic viscosity
1/dynamic viscosity × density