# Reynolds number

### From CFD-Wiki

(9 intermediate revisions not shown) | |||

Line 1: | Line 1: | ||

- | The Reynolds number | + | 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 [[Navier-Stokes equations|momentum equation]] which is given below |

- | <math> | + | :<math> |

\frac{\partial}{\partial t}\left( \rho u_i \right) + | \frac{\partial}{\partial t}\left( \rho u_i \right) + | ||

\frac{\partial}{\partial x_j} | \frac{\partial}{\partial x_j} | ||

Line 7: | Line 7: | ||

</math> | </math> | ||

- | The terms on the right are the inertial forces and those on the left correspond to viscous forces. If <math>U</math>, <math>L</math>, <math>\rho</math> and <math>\mu</math> are the reference values for velocity, length, density and dynamic viscosity, then | + | The terms on the right are the [[inertial forces]] and those on the left correspond to [[viscous forces]]. If <math>U</math>, <math>L</math>, <math>\rho</math> and <math>\mu</math> are the reference values for [[velocity]], [[length]], [[density]] and [[dynamic viscosity]], then |

inertial force ~ <math>\frac{\rho U^2}{L}</math> | inertial force ~ <math>\frac{\rho U^2}{L}</math> | ||

Line 15: | Line 15: | ||

Their ratio is the Reynolds number, usually denoted as <math>Re</math> | Their ratio is the Reynolds number, usually denoted as <math>Re</math> | ||

- | <math> | + | :<math> |

Re = \frac{\mbox{inertial force}}{\mbox{viscous force}} = \frac{\rho U L}{\mu} | Re = \frac{\mbox{inertial force}}{\mbox{viscous force}} = \frac{\rho U L}{\mu} | ||

</math> | </math> | ||

Line 21: | Line 21: | ||

In terms of the kinematic viscosity | In terms of the kinematic viscosity | ||

- | <math> | + | :<math> |

\nu = \frac{\mu}{\rho} | \nu = \frac{\mu}{\rho} | ||

</math> | </math> | ||

Line 27: | Line 27: | ||

the Reynolds number is given by | the Reynolds number is given by | ||

- | <math> | + | :<math> |

Re = \frac{U L}{\nu} | Re = \frac{U L}{\nu} | ||

</math> | </math> | ||

+ | |||

+ | ==Reynolds number as a ratio of time scales== | ||

+ | |||

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

+ | |||

+ | :<math> | ||

+ | T_{v} = \frac{L^2}{\nu} | ||

+ | </math> | ||

+ | |||

+ | and | ||

+ | |||

+ | :<math> | ||

+ | T_{c} = \frac{L}{U} | ||

+ | </math> | ||

+ | |||

+ | The ratio of viscous to convective time scales is | ||

+ | |||

+ | :<math> | ||

+ | \frac{ T_{v} }{ T_{c} } = \frac{(L^2/\nu)}{(L/U)} = \frac{UL}{\nu} = Re | ||

+ | </math> | ||

+ | |||

+ | 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. | ||

+ | |||

+ | ==References== | ||

+ | *{{reference-book | author=Batchelor, G K | year=1967 | title=An Introduction to Fluid Dynamics | rest=Cambridge University Press}} | ||

+ | |||

+ | *{{reference-book |author=Rott, N | year=1990 | title=Note on the history of the Reynolds number| rest =Annual Review of Fluid Mechanics, Vol. 22, 1990, pp. 1–11}} | ||

+ | |||

+ | [[Category: Dimensionless parameters]] |

## Latest revision as of 09:15, 3 January 2012

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

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

inertial force ~

viscous force ~

Their ratio is the Reynolds number, usually denoted as

In terms of the kinematic viscosity

the Reynolds number is given by

## Reynolds number as a ratio of time scales

Consider an impulsively started flat plate moving in its own plane with velocity . Due to the no-slip condition on the plate a boundary layer gradually develops on the plate. At time , the thickness of the boundary layer is of the order of (see Batchelor(1967), section 4.3). Let be the characteristic length scale. The time taken for viscous and convective effects to travel a distance is

and

The ratio of viscous to convective time scales is

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.

## References

**Batchelor, G K (1967)**,*An Introduction to Fluid Dynamics*, Cambridge University Press.

**Rott, N (1990)**,*Note on the history of the Reynolds number*, Annual Review of Fluid Mechanics, Vol. 22, 1990, pp. 1–11.