# Reynolds number

(Difference between revisions)
 Revision as of 21:10, 30 August 2007 (view source)Jasond (Talk | contribs)m← Older edit Revision as of 15:13, 16 January 2008 (view source)Jmortizz (Talk | contribs) Newer edit → Line 55: Line 55: ==References== ==References== *{{reference-book | author=Batchelor G K | year=1967 | title=An Introduction to Fluid Dynamics | rest=Cambridge University Press}} *{{reference-book | author=Batchelor G K | year=1967 | title=An Introduction to Fluid Dynamics | rest=Cambridge University Press}} + + *[http://158.110.32.35/download/CERN07/R_ARFM_90.pdf] Rott, N., “Note on the history of the Reynolds number,” Annual Review of Fluid Mechanics, Vol. 22, 1990, pp. 1–11. [[Category: Dimensionless parameters]] [[Category: Dimensionless parameters]]

## Revision as of 15:13, 16 January 2008

The Reynolds number characterises the relative importance of inertial and viscous forces in a flow. It is important in determining the state of the flow, whether it is laminar or turbulent. At high Reynolds numbers flows generally tend to be turbulent, which was first recognized by Osborne Reynolds in his famous pipe flow experiments. Consider the momentum equation which is given below $\frac{\partial}{\partial t}\left( \rho u_i \right) + \frac{\partial}{\partial x_j} \left[ \rho u_i u_j + p \delta_{ij} \right] = \frac{\partial}{\partial x_j} \tau_{ij}$

The terms on the right are the inertial forces and those on the left correspond to viscous forces. If $U$, $L$, $\rho$ and $\mu$ are the reference values for velocity, length, density and dynamic viscosity, then

inertial force ~ $\frac{\rho U^2}{L}$

viscous force ~ $\frac{\mu U}{L^2}$

Their ratio is the Reynolds number, usually denoted as $Re$ $Re = \frac{\mbox{inertial force}}{\mbox{viscous force}} = \frac{\rho U L}{\mu}$

In terms of the kinematic viscosity $\nu = \frac{\mu}{\rho}$

the Reynolds number is given by $Re = \frac{U L}{\nu}$

## Reynolds number as a ratio of time scales

Consider an impulsively started flat plate moving in its own plane with velocity $U$. Due to the no-slip condition on the plate a boundary layer gradually develops on the plate. At time $t$, the thickness of the boundary layer is of the order of $\sqrt{\nu t}$ (see Batchelor(1967), section 4.3). Let $L$ be the characteristic length scale. The time taken for viscous and convective effects to travel a distance $L$ is $T_{v} = \frac{L^2}{\nu}$

and $T_{c} = \frac{L}{U}$

The ratio of viscous to convective time scales is $\frac{ T_{v} }{ T_{c} } = \frac{(L^2/\nu)}{(L/U)} = \frac{UL}{\nu} = Re$

Thus the Reynolds number is a measure of the viscous and convective time scales. A large Reynolds number means that viscous effects propagate slowly into the fluid. This is the reason why boundary layers are thin in high Reynolds number flows because the fluid is being convected along the flow direction at a much faster rate than the spreading of the boundary layer, which is normal to the flow direction.