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author | Prefetch | 2021-05-05 20:18:57 +0200 |
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committer | Prefetch | 2021-05-05 20:18:57 +0200 |
commit | 93c8b6e86aeafb2f1b7f6b4d39049276ebbcc91c (patch) | |
tree | 5265075e00cabcddfc9f1ce7df26b9272674ca5d /content/know/concept/reynolds-number | |
parent | e394d6c45bcc1e5650bcbeff5a3246316f6842f0 (diff) |
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diff --git a/content/know/concept/reynolds-number/index.pdc b/content/know/concept/reynolds-number/index.pdc new file mode 100644 index 0000000..bd18f2f --- /dev/null +++ b/content/know/concept/reynolds-number/index.pdc @@ -0,0 +1,157 @@ +--- +title: "Reynolds number" +firstLetter: "R" +publishDate: 2021-05-04 +categories: +- Physics +- Fluid mechanics +- Fluid dynamics + +date: 2021-05-04T09:45:22+02:00 +draft: false +markup: pandoc +--- + +# Reynolds number + +The [Navier-Stokes equations](/know/concept/navier-stokes-equations/) +are infamously tricky to solve, +so we would like a way to qualitatively predict +the behaviour of a fluid without needing the flow $\va{v}$. +Consider the main equation: + +$$\begin{aligned} + \pdv{\va{v}}{t} + (\va{v} \cdot \nabla) \va{v} + = - \frac{\nabla p}{\rho} + \nu \nabla^2 \va{v} +\end{aligned}$$ + +Let us introduce the dimensionless variables $\va{v}'$, $\va{r}'$, $t'$ and $p'$, +where $U$ and $L$ are respectively a characteristic velocity and length +of the system at hand: + +$$\begin{aligned} + \va{v} = U \va{v}' + \qquad + \va{r} = L \va{r}' + \qquad + t = \frac{L}{U} t' + \qquad + p = \rho U^2 p' +\end{aligned}$$ + +In this non-dimenionsalization, the differential operators are scaled as follows: + +$$\begin{aligned} + \pdv{t} + = \frac{U}{L} \pdv{t'} + \qquad \quad + \nabla + = \frac{1}{L} \nabla' +\end{aligned}$$ + +Putting everything into the main Navier-Stokes equation then yields: + +$$\begin{aligned} + \frac{U^2}{L} \pdv{\va{v}'}{t'} + \frac{U^2}{L} (\va{v}' \cdot \nabla') \va{v}' + = - \frac{U^2}{L} \nabla' p' + \frac{U \nu}{L^2} \nabla'^2 \va{v}' +\end{aligned}$$ + +After dividing out $U^2/L$, +we arrive at the form of the original equation again: + +$$\begin{aligned} + \pdv{\va{v}'}{t'} + (\va{v}' \cdot \nabla') \va{v}' + = - \nabla' p' + \frac{\nu}{U L} \nabla'^2 \va{v}' +\end{aligned}$$ + +The constant factor of the last term +leads to the definition of the **Reynolds number** $\mathrm{Re}$: + +$$\begin{aligned} + \boxed{ + \mathrm{Re} + \equiv \frac{U L}{\nu} + } +\end{aligned}$$ + +If we choose $U$ and $L$ appropriately for a given system, +the Reynolds number allows us to predict the general trends. +It can be regarded as the inverse of an "effective viscosity": +when $\mathrm{Re}$ is large, viscosity only has a minor role, +but when $\mathrm{Re}$ is small, it dominates the dynamics. + +Another way is thus to see the Reynolds number +as the characteristic ratio between the advective term +(see [material derivative](/know/concept/material-derivative/)) +to the [viscosity](/know/concept/viscosity/) term, +since $\va{v} \sim U$: + +$$\begin{aligned} + \mathrm{Re} + \approx \frac{\big| (\va{v} \cdot \nabla) \va{v} \big|}{\big| \nu \nabla^2 \va{v} \big|} + \approx \frac{U^2 / L}{\nu U / L^2} + = \frac{U L}{\nu} +\end{aligned}$$ + +In other words, $\mathrm{Re}$ +describes the relative strength of intertial and viscous forces. +Returning to the dimensionless Navier-Stokes equation: + +$$\begin{aligned} + \pdv{\va{v}'}{t'} + (\va{v}' \cdot \nabla') \va{v}' + = - \nabla' p' + \frac{1}{\mathrm{Re}} \nabla'^2 \va{v}' +\end{aligned}$$ + +For large $\mathrm{Re} \gg 1$, +we can neglect the latter term, +such that redimensionalizing yields: + +$$\begin{aligned} + \pdv{\va{v}}{t} + (\va{v} \cdot \nabla) \va{v} + = - \nabla p +\end{aligned}$$ + +Which is simply the main [Euler equation](/know/concept/euler-equations/) +for an ideal fluid, i.e. a fluid without viscosity. + + + +## Stokes flow + +A notable case is so-called **Stokes flow** or **creeping flow**, +meaning flow at $\mathrm{Re} \ll 1$. +In this limit, the Navier-Stokes equations can be linearized: +since $\mathrm{Re}$ is the advective-to-viscous ratio, +$\mathrm{Re} \ll 1$ implies that we can ignore the advective term, leaving: + +$$\begin{aligned} + \boxed{ + \pdv{\va{v}}{t} + = - \frac{\nabla p}{\rho} + \nu \nabla^2 \va{v} + } +\end{aligned}$$ + +This equation is called the **unsteady Stokes equation**. +Usually, however, such flows are assumed to be steady +(i.e. time-invariant), leading to the **steady Stokes equation**: + +$$\begin{aligned} + \boxed{ + \nabla p + = \eta \nabla^2 \va{v} + } +\end{aligned}$$ + +This equation is much easier to solve than the full Navier-Stokes equation +thanks to being linear, +and has some interesting properties, such as time-reversibility. + + + +## References +1. B. Lautrup, + *Physics of continuous matter: exotic and everyday phenomena in the macroscopic world*, 2nd edition, + CRC Press. +2. R. Fitzpatrick, + [Dimensionless numbers in incompressible flow](https://farside.ph.utexas.edu/teaching/336L/Fluid/node17.html), + University of Texas. |