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) \(\frac{{V.P}}{{4v}}\)
Only A
The Reynolds number (\(Re\)) is a dimensionless quantity that is used to predict flow patterns in different fluid flow situations. It describes the ratio of inertial forces to viscous forces and is commonly used to distinguish between laminar, transient, and turbulent flow.
For flow in a circular pipe, the Reynolds number is defined as:
\(Re = \frac{{\rho vD}}{{\mu}} = \frac{{vD}}{{\nu}}\)
where:
For flow in non-circular cross-sections, such as rectangular ducts, annular spaces, or open channels, the concept of hydraulic diameter or hydraulic radius is used to calculate the Reynolds number. This allows us to use a similar formula structure as for circular pipes.
The hydraulic radius (\(R_h\)) is defined as the ratio of the cross-sectional area of the flow channel to the wetted perimeter.
\(R_h = \frac{{\text{Cross-sectional Area}}}{{\text{Wetted Perimeter}}}\)
The hydraulic diameter (\(D_h\)) is defined as four times the hydraulic radius.
\(D_h = 4 R_h\)
This definition is chosen such that for a circular pipe of diameter D, the hydraulic diameter is equal to D.
Using the hydraulic diameter, the Reynolds number for a non-circular cross-section is given by:
\(Re = \frac{{vD_h}}{{\nu}}\)
In the given question, the parameter P is defined as the ratio of the cross-sectional area to the wetted perimeter. This is exactly the definition of the hydraulic radius (\(R_h\)).
So, \(P = R_h\).
Substituting \(R_h\) in the hydraulic diameter formula, we get:
\(D_h = 4 R_h = 4P\)
Now, substituting this expression for \(D_h\) into the Reynolds number formula for non-circular sections:
\(Re = \frac{{v D_h}}{{\nu}} = \frac{{v (4P)}}{{\nu}}\)
\(Re = \frac{{4vP}}{{\nu}}\)
This can also be written as:
\(Re = v \cdot \frac{{4P}}{{\nu}}\)
Let's compare the derived formula with the given options, where \(V\) is used for mean velocity instead of \(v\).
A) \(V.\frac{{4P}}{v}\) - This matches our derived formula \(Re = V \cdot \frac{{4P}}{{\nu}}\).
B) \(\frac{{V.P}}{v}\) - This does not match.
C) \(\frac{{V.2P}}{{4v}}\) - This simplifies to \(\frac{{V.P}}{{2v}}\), which does not match.
D) \(\frac{{V.P}}{{4v}}\) - This does not match.
Therefore, the correct expression for the Reynolds number for a non-circular cross-section, using the given parameter P, is \(V.\frac{{4P}}{v}\).
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
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’