What is the ratio of Inertia force to viscous force called?
Reynold's number
In the study of fluid mechanics, various forces act on a fluid during its motion. Two fundamental forces are the inertia force and the viscous force. The ratio of these forces is a very important dimensionless number used to characterize fluid flow regimes.
Inertia force is related to the momentum of the fluid. It represents the tendency of the fluid to resist changes in its state of motion. Essentially, it's proportional to the mass of the fluid particle and its acceleration.
Viscous force is related to the fluid's resistance to flow, or its viscosity. It represents the internal friction within the fluid and between the fluid and the boundaries it flows past. Viscous forces tend to oppose the motion and cause energy dissipation.
The ratio of the inertia force to the viscous force is a dimensionless quantity that helps predict flow patterns in different fluid flow situations. Let's look at the options provided and the force ratios they represent:
The mathematical representation of the Reynold's number ($\text{Re}$) is given by:
\(\text{Re} = \frac{\text{Inertia Force}}{\text{Viscous Force}}\)
Alternatively, it can be expressed as:
\(\text{Re} = \frac{\rho v L}{\mu}\)
Where:
A low Reynold's number indicates that viscous forces are dominant, leading to laminar flow. A high Reynold's number indicates that inertia forces are dominant, leading to turbulent flow.
Therefore, the ratio of inertia force to viscous force is specifically called the Reynold's number.
Match the following and select the correct answer from the codes given below the lists
List I | List II | ||
A. | Steam Nozzle | 1. | Mach number |
B. | Compressible flow | 2. | Reaction turbine |
C. | Surface Tension | 3. | Biot number |
D. | Heat conduction | 4. | Nusselt number |
5. | Supersaturation | ||
6. | Weber number | ||
The Reynold’s number, used for critical velocity for turbulent flow of fluids, is given by the relation
Reynolds number for non - circular cross-section is:
[V = mean velocity, ν = kinematic viscosity, P = ratio of cross-sectional area to the wetted perimeter]
A) \(V.\frac{{4P}}{v}\)
B) \(\frac{{V.P}}{v}\)
C) \(\frac{{V.2P}}{{4v}}\)
D) \(\frac{{V.P}}{{4v}}\)
When the Mach number is less than unity, the flow is
The only possible dimensionless group that combines velocity ‘V’, body size ‘L’, fluid density ‘ρ’ & surface tension ‘σ’