---
title: "Fluid Kinematics"
book: "University Physics — Year 2"
subject: physics
language: en
chapter: 2
exercises: 12
source: https://one-course.com/books/physics/4/en/chapter/2-fluid-kinematics
---

# Chapter 2 — Fluid Kinematics

Stand on a bridge and watch the river. A leaf drifts past, speeds up between the piers, slows in the pool below, circles once in an eddy and moves on. You could describe the river by following that leaf — its position and velocity at every instant — or by standing still and recording, at every point of the river, how fast the water passes. The second description is the fluid physicist’s: a *velocity field*. This chapter sets up the two descriptions, learns to compute the acceleration of a particle from the field, writes the conservation of mass as a local law, and classifies flows by whether they swirl — the vocabulary that Euler’s and Navier’s equations will need.

![A river past a bridge: fast, smooth water between the piers, eddies in their lee — a velocity field to be read at fixed points, not a single trajectory to be followed.](https://one-course.com/images/onecourse/chapters/physics-4/b2-fluid-kinematics/img-6210f765eb02.jpg)

*A river past a bridge: fast, smooth water between the piers, eddies in their lee — a velocity field to be read at fixed points, not a single trajectory to be followed.*

## 2.1 The continuum description

**Definition 2.1 (Fluid particle; the continuum hypothesis).**

A *fluid particle* is a volume of fluid small enough to be treated as a point on the scale of the flow, yet large enough to contain a huge number of molecules, so that its density $\rho$, pressure $P$, temperature $T$ and mean velocity $\vect v$ are well-defined averages (the *mesoscopic* scale, typically a micrometre). The *continuum hypothesis* assumes such a scale exists: the mean free path $\ell$ of the molecules must be much smaller than the scale $L$ of the flow, $\ell/L \ll 1$. In air at atmospheric pressure $\ell \approx 70\,\mathrm{nm}$; in a liquid $\ell$ is the molecular size. The fluid is then described by *fields* $\rho(M, t)$, $P(M, t)$, $\vect v(M, t)$ defined at every point.

**Definition 2.2 (Lagrangian and Eulerian descriptions).**

The *Lagrangian* description follows each [fluid particle](#def-b2-fluid-kinematics-particle): its position $\vect r(t)$ and velocity $\dd\vect r/\dd t$ as functions of time and of its initial position. The *Eulerian* description gives, at each fixed point $M$ and time $t$, the velocity $\vect v(M, t)$ of the particle that is passing through $M$ at that instant. A *pathline* is the trajectory of a particle; a *streamline* at time $t$ is a curve tangent at every point to $\vect v(M, t)$; a *stream tube* is the surface made of the streamlines through a closed curve. A flow is *stationary* (steady) when the Eulerian fields do not depend on time, $\partial\vect v/\partial t = \vect 0$; then streamlines and pathlines coincide and are fixed.

**Example 2.3 (Two descriptions of one flow).**

Water in a garden hose of section $S$ at flow rate $Q$ moves at $v = Q/S$ everywhere: the Eulerian field is uniform and the Lagrangian motion of each particle is uniform. In the tapering nozzle the Eulerian field is still steady but $v$ increases along the axis: every particle *accelerates* as it passes through, though nothing at any fixed point changes with time. That is the first thing the [Eulerian description](#def-b2-fluid-kinematics-euler) must learn to express.

![Left: a steady converging flow — the streamlines are fixed, a marked particle follows one of them and accelerates as the tube narrows. Right: the Eulerian description records the velocity vector at fixed points; the Lagrangian one follows a particle along its pathline.](https://one-course.com/images/onecourse/chapters/physics-4/b2-fluid-kinematics/fig-486768573077.svg)

*Left: a steady converging flow — the [streamlines](#def-b2-fluid-kinematics-euler) are fixed, a marked particle follows one of them and accelerates as the tube narrows. Right: the [Eulerian description](#def-b2-fluid-kinematics-euler) records the velocity vector at fixed points; the Lagrangian one follows a particle along its [pathline](#def-b2-fluid-kinematics-euler).*

## 2.2 The material derivative

**Theorem 2.4 (Material (particle) derivative).**

The rate of change of a quantity $G(M, t)$ (scalar or vector) *for the [fluid particle](#def-b2-fluid-kinematics-particle)* passing through $M$ at time $t$ is

$$
\frac{\mathrm DG}{\mathrm Dt} = \frac{\partial G}{\partial t} + (\vect v\cdot
\operatorname{\vect{grad}})\,G ,
\qquad\text{in particular}\qquad
\vect a = \frac{\mathrm D\vect v}{\mathrm Dt} = \frac{\partial\vect v}{\partial t} +
(\vect v\cdot\operatorname{\vect{grad}})\,\vect v ,
$$

where $(\vect v\cdot\operatorname{\vect{grad}}) = v_x\partial_x + v_y\partial_y +
v_z\partial_z$. The first term is the *local* rate of change (at a fixed point), the second the *convective* one (because the particle moves to where $G$ is different). For the velocity, $(\vect v\cdot
\operatorname{\vect{grad}})\vect v = \operatorname{\vect{grad}}(v^2/2) +
(\operatorname{\vect{curl}}\vect v)\wedge\vect v$.

**Proof.** In $\dd t$ the particle moves from $M$ to $M + \vect v\,\dd t$, so $\dd G =
G(M + \vect v\dd t, t + \dd t) - G(M, t) = \partial_tG\,\dd t + \dd t\,(v_x\partial_x
+ v_y\partial_y + v_z\partial_z)G$ to first order (chain rule for a function of four variables). The vector identity is checked on the $x$ component: $[\operatorname{\vect{grad}}(v^2/2)]_x = v_x\partial_xv_x + v_y\partial_x
v_y + v_z\partial_xv_z$ and $[(\operatorname{\vect{curl}}\vect v)\wedge\vect v]_x =
v_y(\partial_yv_x - \partial_xv_y) + v_z(\partial_zv_x - \partial_xv_z)$ (with the components of $\operatorname{\vect{curl}}\vect v$ given below in [Definition 2.12](#def-b2-fluid-kinematics-vorticity)); their sum is $v_x\partial_xv_x +
v_y\partial_yv_x + v_z\partial_zv_x$. ∎

**Example 2.5 (Acceleration in a steady nozzle).**

A one-dimensional steady flow $v(x) = v_0(1 + x/L)$ along a nozzle: the local term vanishes, and $a = v\,\dd v/\dd x = v_0^2(1 + x/L)/L$. A particle that enters at $v_0 = 2\,\mathrm{m}/\mathrm{s}$ and leaves at $2v_0$ over $L
= 5\,\mathrm{cm}$ feels $a = 80$ to $160\,\mathrm{m}/\mathrm{s}^{2}$: eight to sixteen $g$, in a flow where nothing depends on time.

**Example 2.6 (Local versus convective).**

Temperature at a weather station falls during the night ($\partial T/
\partial t < 0$: local), and falls for an air parcel carried northward by the wind ($\vect v\cdot\operatorname{\vect{grad}}T < 0$: convective, or *advective*). A thermometer on a balloon drifting with the wind records the sum, $\mathrm DT/\mathrm Dt$; the weather station records only the first term.

## 2.3 Conservation of mass

**Definition 2.7 (Mass flow rate and volume flow rate).**

The *mass flow rate* through an oriented surface $S$ is the mass crossing it per unit time, $D_m = \sum\rho\,\vect v\cdot\vect n\,\dd S$ — the flux of the *mass current density* $\vect j = \rho\vect v$ (unit $\mathrm{kg}\,\mathrm{m}^{-2}\,\mathrm{s}^{-1}$); the *volume flow rate* is $D_V = \sum\vect v
\cdot\vect n\,\dd S$ ($\mathrm{m}^{3}/\mathrm{s}$). For a uniform velocity normal to a plane section of area $S$, $D_m = \rho vS$ and $D_V = vS$.

**Proof.** In $\dd t$ the fluid crossing the element $\dd S$ is that contained in the oblique cylinder of base $\dd S$ and generator $\vect v\,\dd t$, of volume $\vect v\cdot\vect n\,\dd S\,\dd t$ and mass $\rho$ times that. ∎

**Theorem 2.8 (Local conservation of mass).**

At every point of a fluid,

$$
\frac{\partial\rho}{\partial t} + \operatorname{div}(\rho\vect v) = 0 ,
\qquad\text{where}\qquad
\operatorname{div}\vect A = \frac{\partial A_x}{\partial x} + \frac{\partial A_y}{\partial y} +
\frac{\partial A_z}{\partial z}
$$

is the *divergence* of a vector field: the net outgoing flux of $\vect A$ through the surface of a small volume, per unit volume. Equivalently $\mathrm D\rho/\mathrm Dt + \rho\operatorname{div}\vect v = 0$.

**Proof.** Take the fixed box $[x, x + \dd x]\times[y, y + \dd y]\times[z, z + \dd z]$. Its mass $\rho\,\dd x\dd y\dd z$ changes at the rate $\partial_t\rho\,\dd x\dd y
\dd z$. Mass enters through the face at $x$ at the rate $j_x(x)\dd y\dd z$ and leaves through the face at $x + \dd x$ at $j_x(x + \dd x)\dd y\dd z$: net outflow $\partial_xj_x\,\dd x\dd y\dd z$, and likewise for $y$ and $z$. Conservation of mass — no mass is created — gives $\partial_t\rho = -
(\partial_xj_x + \partial_yj_y + \partial_zj_z)$. The second form follows from $\operatorname{div}(\rho\vect v) = \vect v\cdot\operatorname{\vect{grad}}\rho +
\rho\operatorname{div}\vect v$. ∎

**Remark 2.9 (The divergence, a first meeting).**

The derivation shows what $\operatorname{div}$ measures: the flux leaving a small box per unit volume. Summing over the boxes that tile a finite volume $V$, the interior faces cancel pairwise and only the outer surface remains: $\iint_{\partial V}\vect A\cdot\vect n\,\dd S = \iiint_V
\operatorname{div}\vect A\,\dd\tau$ — the divergence (Ostrogradski) theorem, which we shall state properly in [Chapter 11](https://one-course.com/books/physics/4/en/chapter/11-maxwells-equations#ch-b2-maxwell-equations) and use throughout electromagnetism; it is proved in the Year 3 mathematics volume. Integrated over a fixed volume, the local law reads $\dd m_V/\dd t = -D_m^{\text{out}}$: the mass inside changes by what crosses the boundary.

![Left: the mass balance of a fixed box — the net outflow through its six faces, per unit volume, is the divergence of v. Right: in a steady flow the mass flow rate is the same through every section of a stream tube.](https://one-course.com/images/onecourse/chapters/physics-4/b2-fluid-kinematics/fig-6317b4b3c87b.svg)

*Left: the mass balance of a fixed box — the net outflow through its six faces, per unit volume, is the divergence of $\rho\vect v$. Right: in a steady flow the [mass flow rate](#def-b2-fluid-kinematics-flowrate) is the same through every section of a stream tube.*

**Corollary 2.10 (Incompressible flow; stream tubes).**

A flow is *incompressible* when the density of each particle stays constant, $\mathrm D\rho/\mathrm Dt = 0$, which is equivalent to

$$
\operatorname{div}\vect v = 0 .
$$

A homogeneous liquid flows incompressibly; so does a gas at speeds well below the speed of sound (see [Chapter 7](https://one-course.com/books/physics/4/en/chapter/7-sound-waves-in-fluids#ch-b2-sound-waves)). In a steady flow the [mass flow rate](#def-b2-fluid-kinematics-flowrate) $\rho vS$ is the same through every section of a stream tube; if moreover the flow is incompressible and $\rho$ uniform, $vS$ is constant: the fluid speeds up where the tube narrows.

**Proof.** $\mathrm D\rho/\mathrm Dt = -\rho\operatorname{div}\vect v$. For the tube, apply the integrated balance to the volume between two sections: no flux through the lateral surface (velocity tangent), steady state, so inflow equals outflow. ∎

**Example 2.11 (Blood).**

The aorta (section $2.5\,\mathrm{cm}^{2}$) carries $5\,\mathrm{L}/\mathrm{min}$ $= 83\,\mathrm{cm}^{3}/\mathrm{s}$: $v = 33\,\mathrm{cm}/\mathrm{s}$. The same flow passes through some $10^{10}$ capillaries of total section about $2500\,\mathrm{cm}^{2}$: $v = 0.3\,\mathrm{mm}/\mathrm{s}$ — slow enough for exchanges through the walls, the point of the branching.

## 2.4 Vorticity and irrotational flows

**Definition 2.12 (Vorticity).**

The *vorticity* of a flow is the vector field

$$
\vect\omega = \operatorname{\vect{curl}}\vect v , \qquad
\operatorname{\vect{curl}}\vect A = \Bigl(\frac{\partial A_z}{\partial y} -
\frac{\partial A_y}{\partial z},\; \frac{\partial A_x}{\partial z} - \frac{\partial A_z}
{\partial x},\; \frac{\partial A_y}{\partial x} - \frac{\partial A_x}{\partial y}\Bigr) .
$$

A flow is *irrotational* where $\vect\omega = \vect 0$.

**Proposition 2.13 (Vorticity measures local rotation).**

A small fluid element centred at $M$ rotates, as a whole, with the angular velocity $\vect\Omega = \tfrac12\vect\omega(M)$. In a solid-body rotation $\vect v = \vect\Omega\wedge\vect{OM}$ the [vorticity](#def-b2-fluid-kinematics-vorticity) is uniform, $\vect\omega = 2\vect\Omega$; in the plane shear flow $\vect v = ky\,\vect e_x$ it is $\vect\omega = -k\vect e_z$: a paddle wheel dropped in a shear flow turns although the [streamlines](#def-b2-fluid-kinematics-euler) are straight.

**Proof.** Near $M$, $\vect v(M + \vect\epsilon) = \vect v(M) + \mathbf G\vect\epsilon$ with $\mathbf G$ the matrix of $\partial_jv_i$; split it into its symmetric part (a pure strain, which stretches the element without turning it as a whole) and its antisymmetric part, whose matrix $\tfrac12(\partial_jv_i -
\partial_iv_j)$ is that of $\vect\epsilon \mapsto \tfrac12\vect\omega\wedge\vect\epsilon$ ([Theorem 1.2](https://one-course.com/books/physics/4/en/chapter/1-rigid-body-mechanics#thm-b2-rigid-body-mechanics-field)). Solid rotation about $\vect e_z$: $\vect v = \Omega(-y, x, 0)$, $\omega_z = \partial_xv_y - \partial_yv_x = 2\Omega$. Shear: $\omega_z = -\partial_y(ky) = -k$. ∎

**Definition 2.14 (Velocity potential; circulation).**

In an [irrotational flow](#def-b2-fluid-kinematics-vorticity) the velocity derives from a *velocity potential*: $\vect v = \operatorname{\vect{grad}}\varphi$ (the circulation of $\vect v$ along a path then depends only on its ends, $\int_A^B\vect v
\cdot\dd\vect l = \varphi(B) - \varphi(A)$). If the flow is also incompressible, $\Delta\varphi = \operatorname{div}\operatorname{\vect{grad}}
\varphi = 0$: the potential obeys Laplace’s equation, exactly like the electrostatic potential in a charge-free region — a *potential flow*. The *circulation* of the velocity along a closed curve $C$ is $\Gamma = \oint_C\vect v\cdot\dd\vect l$.

**Proof.** That a curl-free field on a simply connected region is a gradient, and that a gradient is curl-free ($\partial_y\partial_z\varphi = \partial_z\partial_y\varphi$), are the Year 2 mathematics volume’s; Laplace’s equation follows from $\operatorname{div}\vect v = 0$. ∎

**Example 2.15 (Three plane flows).**

(i) *[Stagnation flow](#ex-b2-fluid-kinematics-planeflows)* $\vect v = k(x, -y)$: $\operatorname{div}\vect v =
0$, $\vect\omega = \vect 0$, $\varphi = \tfrac12k(x^2 - y^2)$; [streamlines](#def-b2-fluid-kinematics-euler) $xy =$ const, hyperbolas — a jet hitting a wall, near the axis. (ii) *[Point vortex](#ex-b2-fluid-kinematics-planeflows)* $\vect v = \dfrac{\Gamma}{2\pi r}\vect e_\theta$ (plane polar coordinates): incompressible and *irrotational everywhere except at $r = 0$*, $\varphi = \Gamma\theta/2\pi$ (multivalued), and the circulation on any circle around the centre is $\Gamma$ — the [vorticity](#def-b2-fluid-kinematics-vorticity) is concentrated on the axis. (iii) *[Rankine vortex](#ex-b2-fluid-kinematics-planeflows)*: a core $r < a$ in solid rotation $v_\theta = \Omega r$ ([vorticity](#def-b2-fluid-kinematics-vorticity) $2\Omega$) matched to the [point vortex](#ex-b2-fluid-kinematics-planeflows) $v_\theta = \Omega a^2/r$ outside: the model of a tornado, a bathtub swirl or the eddy behind the bridge pier — the velocity peaks at the edge of the core.

![Three plane flows. Left: the stagnation flow, irrotational, with hyperbolic streamlines. Middle: the point vortex — circular streamlines, yet zero vorticity away from the centre. Right: the Rankine vortex profile, solid rotation in the core and a point vortex outside.](https://one-course.com/images/onecourse/chapters/physics-4/b2-fluid-kinematics/fig-9206be7bc8d1.svg)

*Three plane flows. Left: the [stagnation flow](#ex-b2-fluid-kinematics-planeflows), irrotational, with hyperbolic [streamlines](#def-b2-fluid-kinematics-euler). Middle: the [point vortex](#ex-b2-fluid-kinematics-planeflows) — circular [streamlines](#def-b2-fluid-kinematics-euler), yet zero [vorticity](#def-b2-fluid-kinematics-vorticity) away from the centre. Right: the [Rankine vortex](#ex-b2-fluid-kinematics-planeflows) profile, solid rotation in the core and a [point vortex](#ex-b2-fluid-kinematics-planeflows) outside.*

**Remark 2.16 (Why the circulation matters).**

For a small plane loop of area $\dd S$ with normal $\vect n$, the circulation is $\oint\vect v\cdot\dd\vect l = \vect\omega\cdot\vect n\,\dd S$ — the [vorticity](#def-b2-fluid-kinematics-vorticity) is the circulation per unit area, exactly as the divergence is the flux per unit volume. (Check it on the solid-body rotation: $2\pi r\cdot\Omega r = 2\Omega\cdot\pi r^2$.) Summed over a surface, this gives Stokes’ theorem, $\oint_C\vect v\cdot\dd\vect l = \iint_S
\operatorname{\vect{curl}}\vect v\cdot\vect n\,\dd S$, stated in [Chapter 11](https://one-course.com/books/physics/4/en/chapter/11-maxwells-equations#ch-b2-maxwell-equations). A wing generates lift by carrying a circulation around itself; a vortex line persists in a perfect fluid (Kelvin’s theorem) — which is why the eddy behind the pier survives so long.

**Method 2.17 (Reading a velocity field).**

Given $\vect v(M, t)$: (1) is it steady? ($\partial_t\vect v = \vect 0$); (2) is it incompressible? ($\operatorname{div}\vect v = 0$); (3) is it irrotational? ($\operatorname{\vect{curl}}\vect v = \vect 0$; if so find $\varphi$); (4) find the [streamlines](#def-b2-fluid-kinematics-euler) from $\dd x/v_x = \dd y/v_y = \dd z/
v_z$ at fixed $t$, and the [pathlines](#def-b2-fluid-kinematics-euler) from $\dd\vect r/\dd t = \vect v(\vect r,
t)$; (5) compute the acceleration $\partial_t\vect v + (\vect v\cdot
\operatorname{\vect{grad}})\vect v$. In plane polar coordinates $(r, \theta)$, $\operatorname{div}\vect v = \dfrac1r\dfrac{\partial(rv_r)}{\partial r} + \dfrac1r
\dfrac{\partial v_\theta}{\partial\theta}$ and $\omega_z = \dfrac1r\dfrac{\partial(rv_\theta)}
{\partial r} - \dfrac1r\dfrac{\partial v_r}{\partial\theta}$ (admitted here; derived in [Chapter 11](https://one-course.com/books/physics/4/en/chapter/11-maxwells-equations#ch-b2-maxwell-equations)).

## 2.5 Exercises

**Exercise 2.1 ★.**

The mean free path of air is $70\,\mathrm{nm}$ at $1\,\mathrm{bar}$ and varies as $1/P$. Is the continuum description valid for (a) air around a car, (b) air in a $1\,\text{µ}\mathrm{m}$ microchannel at $1\,\mathrm{bar}$, (c) air at $100\,\mathrm{km}$ altitude ($P \approx 3 \times 10^{-7}\,\mathrm{bar}$) around a $1\,\mathrm{m}$ satellite? Give $\ell/L$ in each case.

**Solution of Exercise 2.1.**

(a) $\ell/L \sim 7 \times 10^{-8}$: continuum. (b) $0.07$: marginal — the continuum laws start to fail (slip at the walls). (c) $\ell = 70 \times 10^{-9}
/3 \times 10^{-7} = 0.23\,\mathrm{m}$, $\ell/L = 0.23$: no continuum; the gas is a rain of independent molecules (free-molecular regime).

**Exercise 2.2 ★.**

Steady one-dimensional flow $v(x) = v_0(1 + x/L)$ for $0 \le x \le L$. Acceleration of a particle at $x$; time it takes to cross from $0$ to $L$; compare with $L/v_0$ and $L/2v_0$.

**Solution of Exercise 2.2.**

$a = v\,\dd v/\dd x = v_0^2(1 + x/L)/L$ (from $v_0^2/L$ to $2v_0^2/L$). $\dd x/\dd t = v_0(1 + x/L)$: $t = (L/v_0)\ln2 = 0.69\,L/v_0$, between $L/2v_0$ and $L/v_0$.

**Exercise 2.3 ★.**

In a pipe of radius $R$ the velocity profile is $v(r) = v_{\max}(1 -
r^2/R^2)$ along the axis. [Volume flow rate](#def-b2-fluid-kinematics-flowrate); mean speed $\langle v\rangle
= D_V/\pi R^2$; numbers for $R = 5\,\mathrm{mm}$, $v_{\max} = 0.4\,\mathrm{m}/\mathrm{s}$.

**Solution of Exercise 2.3.**

$D_V = \int_0^Rv_{\max}(1 - r^2/R^2)\,2\pi r\,\dd r = \tfrac12\pi R^2v_{\max}$; $\langle v\rangle = v_{\max}/2 = 0.20\,\mathrm{m}/\mathrm{s}$; $D_V = 1.6 \times 10^{-5}\,\mathrm{m}^{3}/\mathrm{s} =
16\,\mathrm{mL}/\mathrm{s}$.

**Exercise 2.4 ★.**

For each field, say whether the flow is incompressible and whether it is irrotational; give the [vorticity](#def-b2-fluid-kinematics-vorticity): (a) $\vect v = (ax, -ay, 0)$; (b) $\vect v = (-\Omega y, \Omega x, 0)$; (c) $\vect v = (ax, ay, 0)$; (d) $\vect v =
(ky, 0, 0)$; (e) $\vect v = (ax, -ay, bz)$ — for which $b$ is it incompressible?

**Solution of Exercise 2.4.**

(a) $\operatorname{div} = 0$, $\vect\omega = \vect 0$: incompressible, irrotational. (b) $\operatorname{div} = 0$, $\omega_z = 2\Omega$: solid rotation. (c) $\operatorname{div} = 2a \ne 0$, irrotational (a plane source). (d) $\operatorname{div} = 0$, $\omega_z = -k$: shear. (e) $\operatorname{div} = b$: incompressible iff $b = 0$; irrotational for every $b$.

**Exercise 2.5 ★★.**

A garden hose of inner diameter $12\,\mathrm{mm}$ fills a $10\,\mathrm{L}$ bucket in $50\,\mathrm{s}$. Speed in the hose; speed in a $3\,\mathrm{mm}$ nozzle; if the nozzle tapers over $4\,\mathrm{cm}$, estimate the mean acceleration of a particle crossing it (in $g$); time spent in the nozzle.

**Solution of Exercise 2.5.**

$D_V = 0.20\,\mathrm{L}/\mathrm{s}$. Hose $S = 1.13\,\mathrm{cm}^{2}$: $v = 1.8\,\mathrm{m}/\mathrm{s}$; nozzle $S = 7.1\,\mathrm{mm}^{2}$: $v = 28\,\mathrm{m}/\mathrm{s}$. Mean acceleration $\Delta(v^2/2)/L
= (28^2 - 1.8^2)/0.08 \approx 1 \times 10^{4}\,\mathrm{m}/\mathrm{s}^{2} \approx 1000\,g$. Time $\approx
\int\dd x/v$: a few milliseconds ($4\,\mathrm{ms}$ for a linear speed profile).

**Exercise 2.6 ★★.**

Unsteady plane flow $\vect v = (U, V\cos\omega t)$ with $U$, $V$, $\omega$ constant. (a) [Streamlines](#def-b2-fluid-kinematics-euler) at time $t$. (b) [Pathline](#def-b2-fluid-kinematics-euler) of the particle at the origin at $t = 0$. (c) Sketch both for $V = U$ at $t = 0$ and at $t = \pi/2\omega$; why do they differ? (d) Acceleration of a particle.

**Solution of Exercise 2.6.**

(a) $\dd y/\dd x = (V/U)\cos\omega t$: straight lines of slope $(V/U)\cos\omega t$, all parallel, tilting with time. (b) $x = Ut$, $y =
(V/\omega)\sin\omega t$: the sinusoid $y = (V/\omega)\sin(\omega x/U)$. (c) At $t = 0$ the [streamlines](#def-b2-fluid-kinematics-euler) are at $45{}^{\circ}$ and the [pathline](#def-b2-fluid-kinematics-euler) leaves the origin at $45{}^{\circ}$; at $t = \pi/2\omega$ the [streamlines](#def-b2-fluid-kinematics-euler) are horizontal while the [pathline](#def-b2-fluid-kinematics-euler) is a fixed sinusoid. They differ because the flow is unsteady: a [streamline](#def-b2-fluid-kinematics-euler) is a snapshot, a [pathline](#def-b2-fluid-kinematics-euler) a history. (d) $\vect a = \partial_t\vect v = (0, -V\omega\sin\omega t)$ — the field is uniform, so the convective term vanishes.

**Exercise 2.7 ★★.**

A river $50\,\mathrm{m}$ wide and $2.0\,\mathrm{m}$ deep flows at $1.2\,\mathrm{m}/\mathrm{s}$. (a) Flow rate. (b) It enters a gorge $15\,\mathrm{m}$ wide and $4.0\,\mathrm{m}$ deep: speed. (c) A tributary adds $30\,\mathrm{m}^{3}/\mathrm{s}$; downstream the river is $60\,\mathrm{m}$ wide and $2.5\,\mathrm{m}$ deep: speed. (d) Hot gas flows steadily in a pipe of constant section; between two points its temperature doubles at constant pressure: what happens to its speed?

**Solution of Exercise 2.7.**

(a) $D_V = 50 \times 2 \times 1.2 = 120\,\mathrm{m}^{3}/\mathrm{s}$. (b) $120/60 = 2.0\,\mathrm{m}/\mathrm{s}$. (c) $150/150 = 1.0\,\mathrm{m}/\mathrm{s}$. (d) $\rho \propto 1/T$ at constant $P$ halves; $\rho vS$ is conserved: the speed doubles.

**Exercise 2.8 ★★.**

*[Rankine vortex](#ex-b2-fluid-kinematics-planeflows).* $v_\theta = \Omega r$ for $r < a$, $v_\theta = \Omega a^2/r$ for $r > a$. (a) [Vorticity](#def-b2-fluid-kinematics-vorticity) in each region (use the polar formula). (b) Circulation on a circle of radius $r$ centred on the axis, in both regions; relate to the [vorticity](#def-b2-fluid-kinematics-vorticity) flux. (c) A tornado: $a = 50\,\mathrm{m}$, $v_{\max} = 70\,\mathrm{m}/\mathrm{s}$: $\Omega$, $\Gamma$, and the speed at $500\,\mathrm{m}$. (d) Is the core flow irrotational? The outside? Where is the "rotation" physically?

**Solution of Exercise 2.8.**

(a) $\omega_z = \frac1r\frac{\dd(rv_\theta)}{\dd r}$: $2\Omega$ inside, $0$ outside. (b) Inside $\Gamma = 2\pi r\cdot\Omega r = 2\Omega\cdot\pi r^2$, the flux of the [vorticity](#def-b2-fluid-kinematics-vorticity); outside $\Gamma = 2\pi\Omega a^2$, constant, the flux of the whole core. (c) $\Omega = v_{\max}/a = 1.4\,\mathrm{rad}/\mathrm{s}$; $\Gamma = 2\pi av_{\max}
= 2.2 \times 10^{4}\,\mathrm{m}^{2}/\mathrm{s}$; at $500\,\mathrm{m}$: $\Omega a^2/r = 7\,\mathrm{m}/\mathrm{s}$. (d) The core rotates like a solid; outside, the flow is irrotational: particles go round the axis without spinning about themselves. The [vorticity](#def-b2-fluid-kinematics-vorticity) — the rotation — lives in the core.

**Exercise 2.9 ★★.**

*[Stagnation flow](#ex-b2-fluid-kinematics-planeflows)* $\vect v = k(x, -y)$. (a) Potential $\varphi$ and check $\Delta\varphi = 0$. (b) [Streamlines](#def-b2-fluid-kinematics-euler); the function $\psi = kxy$ is constant on them — show that $v_x = \partial\psi/\partial y$, $v_y = -\partial\psi/
\partial x$ (the *stream function*). (c) Acceleration field; show it is $\operatorname{\vect{grad}}(v^2/2)$ and interpret. (d) [Pathline](#def-b2-fluid-kinematics-euler) of a particle starting at $(x_0, y_0)$: $x = x_0\eu^{kt}$, $y = y_0\eu^{-kt}$.

**Solution of Exercise 2.9.**

(a) $\varphi = \tfrac12k(x^2 - y^2)$, $\Delta\varphi = k - k = 0$. (b) $\dd x/
kx = \dd y/(-ky)$: $xy =$ const; $\partial_y\psi = kx = v_x$, $-\partial_x\psi =
-ky = v_y$. (c) $\vect a = (v_x\partial_x + v_y\partial_y)\vect v = k^2(x, y) =
\operatorname{\vect{grad}}\bigl(\tfrac12k^2(x^2 + y^2)\bigr) = \operatorname{\vect{grad}}
(v^2/2)$: in a steady [irrotational flow](#def-b2-fluid-kinematics-vorticity) the acceleration is the gradient of the kinetic energy per unit mass; it points away from the stagnation point — a particle decelerates as it approaches the wall along $y$ and accelerates away along $x$. (d) $\dot x = kx$, $\dot y = -ky$: $x = x_0\eu^{kt}$, $y = y_0\eu^{-kt}$ ($xy$ constant).

**Exercise 2.10 ★★★.**

*An expanding flow.* One-dimensional flow $v(x, t) = x/(t + \tau)$ for $t > 0$, $\tau > 0$ constant. (a) [Pathlines](#def-b2-fluid-kinematics-euler): show $x(t) = x_0(1 +
t/\tau)$; acceleration of a particle, both from the [pathline](#def-b2-fluid-kinematics-euler) and from the [material derivative](#thm-b2-fluid-kinematics-material). (b) The density is uniform at each time, $\rho(t)$: use mass conservation to find $\rho(t)$. (c) Check by following the mass between two particles. (d) Why is this field a one-dimensional model of a uniformly expanding universe?

**Solution of Exercise 2.10.**

(a) $\dd x/\dd t = x/(t + \tau)$ gives $x = x_0(1 + t/\tau)$, $\ddot x = 0$; [material derivative](#thm-b2-fluid-kinematics-material): $\partial_tv + v\partial_xv = -x/(t + \tau)^2 + x/(t + \tau)^2
= 0$. (b) $\partial_t\rho + \partial_x(\rho v) = \dot\rho + \rho/(t + \tau) = 0$: $\rho =
\rho_0\tau/(t + \tau)$. (c) Two particles’ separation grows as $(1 + t/\tau)$ and the mass between them is fixed: $\rho \propto 1/(1 + t/\tau)$. (d) $v =
Hx$ with $H = 1/(t + \tau)$: a Hubble law, free expansion (no acceleration), density falling as the inverse of the scale factor.

**Exercise 2.11 ★★★.**

*Source in a stream.* Superpose a uniform flow $\vect v = U\vect e_x$ and a plane source $\vect v = \dfrac{q}{2\pi r}\vect e_r$ ($q$ the [volume flow rate](#def-b2-fluid-kinematics-flowrate) per unit length along $z$). (a) Potential $\varphi = Ux +
(q/2\pi)\ln r$; check both flows are incompressible and irrotational (except at the origin). (b) Stagnation point. (c) Stream function $\psi
= Uy + q\theta/2\pi$; the [streamline](#def-b2-fluid-kinematics-euler) through the stagnation point is $r\sin\theta = (q/2\pi U)(\pi - \theta)$: sketch it. (d) Show that far downstream this [streamline](#def-b2-fluid-kinematics-euler) is at $y = \pm q/2U$: the flow outside it is the flow around a blunt half-body of width $q/U$.

**Solution of Exercise 2.11.**

(a) $\vect v = \operatorname{\vect{grad}}\varphi = (U + qx/2\pi r^2, qy/2\pi r^2)$; the source has $v_r = q/2\pi r$, $\operatorname{div} = \frac1r\dd(rv_r)/\dd r
= 0$ and no $\theta$ dependence, so $\omega_z = 0$; sums of such fields are again incompressible and irrotational. (b) On the negative $x$ axis, $U - q/2\pi r = 0$: $x_s = -q/2\pi U$. (c) At the stagnation point $\theta =
\pi$, $y = 0$: $\psi = q/2$; the [streamline](#def-b2-fluid-kinematics-euler) $Ur\sin\theta + q\theta/2\pi = q/2$, i.e. $r\sin\theta = (q/2\pi U)(\pi - \theta)$ — a curve leaving $x_s$ and opening downstream. (d) $\theta \to 0$: $y \to q/2U$; $\theta \to 2\pi$ (lower branch): $y \to -q/2U$. The fluid inside that [streamline](#def-b2-fluid-kinematics-euler) comes from the source; outside it, the uniform stream flows around a half-body of asymptotic width $q/U$.

**Exercise 2.12 ★★★.**

*Vortex and sink.* Plane flow $\vect v = -\dfrac{q}{2\pi r}\vect e_r +
\dfrac{\Gamma}{2\pi r}\vect e_\theta$ for $r > a$. (a) Show it is incompressible and irrotational. (b) [Streamlines](#def-b2-fluid-kinematics-euler): logarithmic spirals $r = r_0\eu^{-q\theta/\Gamma}$. (c) Acceleration of a particle: show it is purely radial, $-v^2/r\,\vect e_r$. (d) Time for a particle to spiral from $r_0$ to $a$; number of turns it makes. (e) Numbers: $q =
1.5 \times 10^{-3}\,\mathrm{m}^{2}/\mathrm{s}$, $\Gamma = 3 \times 10^{-2}\,\mathrm{m}^{2}/\mathrm{s}$, $r_0 = 0.5\,\mathrm{m}$, $a = 2\,\mathrm{cm}$.

**Solution of Exercise 2.12.**

(a) $\operatorname{div}\vect v = \frac1r\partial_r(-q/2\pi) = 0$; $\omega_z =
\frac1r\partial_r(\Gamma/2\pi) = 0$. (b) $\dd r/v_r = r\,\dd\theta/v_\theta$ gives $\dd r/r = -(q/\Gamma)\dd\theta$. (c) $a_r = v_r\partial_rv_r - v_\theta^2/r =
-(q^2 + \Gamma^2)/4\pi^2r^3 = -v^2/r$; $a_\theta = v_r\partial_rv_\theta + v_rv_\theta/r
= 0$. (d) $\dd r/\dd t = -q/2\pi r$: $t = \pi(r_0^2 - a^2)/q$; turns $= (\Gamma/2\pi q)\ln(r_0/a)$. (e) $t = 520\,\mathrm{s} \approx 9\,\mathrm{min}$; $10$ turns.

## 2.6 Problem: From the plughole to the hurricane

**Problem 2.1.**

Weekend problem — the same kinematics at three scales: the swirl above a drain, a tornado, and a cyclone seen from a satellite

**Part I — The bathtub.** A bath is drained through a hole of radius $a = 2\,\mathrm{cm}$; the water, of depth $h = 20\,\mathrm{cm}$, leaves at the [volume flow rate](#def-b2-fluid-kinematics-flowrate) $D_V =
0.30\,\mathrm{L}/\mathrm{s}$. Away from the hole the flow is modelled as plane (independent of depth): $\vect v = v_r(r)\vect e_r + v_\theta(r)\vect e_\theta$.

1. Using mass conservation through a cylinder of radius $r$ and height $h$ , show that $v_r = -q/2\pi r$ with $q = D_V/h$ ; value of $q$ .
2. Before the plug was pulled the water had been stirred and turned at $1.0\,\mathrm{cm}/\mathrm{s}$ at $r = 50\,\mathrm{cm}$ . Admitting that each ring of water keeps its angular momentum as it moves inward ( $rv_\theta$ constant), find $v_\theta(r)$ and the circulation $\Gamma$ .
3. Check that the flow is incompressible and irrotational for $r > a$ .
4. [Streamlines](#def-b2-fluid-kinematics-euler) : show they are logarithmic spirals and find how many turns a particle makes between $r = 50\,\mathrm{cm}$ and $r = a$ .
5. Time for a particle to go from $50\,\mathrm{cm}$ to the hole, and its azimuthal speed on arrival.
6. Acceleration of a particle at $r$ ; compare with $g$ at $r = a$ . (The free surface dips where the pressure must balance it — the funnel; next chapter.)
7. The Earth’s rotation gives any fluid at rest in the bath a "background" rotation at the local vertical rate $\Omega_\oplus\sin\lambda \approx 5 \times 10^{-5}\,\mathrm{rad}/\mathrm{s}$ . Compare the azimuthal speed it would give at $50\,\mathrm{cm}$ with the $1\,\mathrm{cm}/\mathrm{s}$ of the stirring, and say whether the sense of rotation of a draining bath is decided by the hemisphere.

**Part II — The tornado as a [Rankine vortex](#ex-b2-fluid-kinematics-planeflows).** Core radius $a = 60\,\mathrm{m}$, maximum wind $v_{\max} = 80\,\mathrm{m}/\mathrm{s}$, air density $\rho = 1.2\,\mathrm{kg}/\mathrm{m}^{3}$.

8. Write $v_\theta(r)$ in both regions and give $\Omega$ and $\Gamma$ .
9. [Vorticity](#def-b2-fluid-kinematics-vorticity) in the core and outside; sketch $v_\theta$ and $\omega_z$ against $r$ .
10. Acceleration of an air particle at the edge of the core; compare with $g$ .
11. Show that a small paddle wheel placed outside the core drifts around the tornado without spinning about its own axis, while one placed in the core turns once per revolution around the axis.
12. Kinetic energy of the core, per metre of height.
13. Kinetic energy of the outer flow per metre of height, between $a$ and $R = 5\,\mathrm{km}$ ; why does it depend on $R$ only logarithmically?
14. With a height of $1\,\mathrm{km}$ , total kinetic energy; compare with the energy released by $1\,\mathrm{t}$ of TNT ( $4.2\,\mathrm{GJ}$ ).
15. Air also flows inward and upward in a tornado. If the core is fed by a radial inflow at $5\,\mathrm{m}/\mathrm{s}$ through its lateral surface over the first $300\,\mathrm{m}$ of height, what vertical speed must the air reach at the top of that layer (uniform over the core’s section)?

**Part III — The cyclone.** A tropical cyclone is modelled as a [Rankine vortex](#ex-b2-fluid-kinematics-planeflows) of core radius $a = 40\,\mathrm{km}$ and $v_{\max} = 50\,\mathrm{m}/\mathrm{s}$. The Earth’s rotation is felt through the *planetary [vorticity](#def-b2-fluid-kinematics-vorticity)* $f = 2\Omega_\oplus\sin\lambda
\approx 5 \times 10^{-5}\,\mathrm{s}^{-1}$ at latitude $20{}^{\circ}$: a ring of air at rest relative to the ground already carries, in the inertial frame, the azimuthal speed $fr/2$ about any vertical axis.

16. [Vorticity](#def-b2-fluid-kinematics-vorticity) of the core and circulation $\Gamma$ of the cyclone; compare the core [vorticity](#def-b2-fluid-kinematics-vorticity) with $f$ .
17. A ring of air of radius $r_0 = 500\,\mathrm{km}$ , initially at rest relative to the ground, is drawn in toward the centre by the low pressure. Admitting that its angular momentum per unit mass about the axis, $r(v_\theta + fr/2)$ , is conserved, find its velocity $v_\theta$ relative to the ground at $r = 100\,\mathrm{km}$ and at $r = 40\,\mathrm{km}$ .
18. In which sense does the cyclone turn in the northern hemisphere, and why? Why is the sense fixed for a cyclone and not for a bath?
19. Why can air not be drawn all the way to the axis this way — what limits the wind and leaves an eye?
20. Air converges into the cyclone at $5\,\mathrm{m}/\mathrm{s}$ through a cylinder of radius $500\,\mathrm{km}$ and height $1\,\mathrm{km}$ : [mass flow rate](#def-b2-fluid-kinematics-flowrate) drawn in ( $\rho = 1.2\,\mathrm{kg}/\mathrm{m}^{3}$ ).
21. The cyclone moves bodily westward at $6\,\mathrm{m}/\mathrm{s}$ . Write the Eulerian velocity field seen from the ground in terms of the field $\vect v_0$ of the vortex in its own frame; is the flow steady in the ground frame? Which side of the storm has the stronger winds?

**Part IV — Flow rates and a summary.**

22. Rain falls at $50\,\mathrm{mm}/\mathrm{h}$ over a catchment of $10\,\mathrm{km}^{2}$ and all of it reaches a river of section $40\,\mathrm{m}^{2}$ : mean speed of the river in flood.
23. Blood: the aorta ( $2.5\,\mathrm{cm}^{2}$ ) carries $5.0\,\mathrm{L}/\mathrm{min}$ ; the capillaries have a total section of $0.25\,\mathrm{m}^{2}$ : speeds in each; time for blood to cross a $1\,\mathrm{mm}$ capillary.
24. A tank of section $S$ drains through a hole of section $s$ at the bottom; the exit speed is $\sqrt{2gh}$ ( $h$ the water level — admitted, derived in the next chapter). Write mass conservation and find $h(t)$ and the emptying time for $S = 1\,\mathrm{m}^{2}$ , $s = 1\,\mathrm{cm}^{2}$ , $h_0 = 1\,\mathrm{m}$ .
25. Give the three flows of Parts I–III in one table: radius, speed, [vorticity](#def-b2-fluid-kinematics-vorticity) of the core, circulation — and the quantity, conserved during the inflow, that makes them spin up.

**Solution of Problem 2.1.**

**1.** Through a cylinder of radius $r$: $2\pi rh|v_r| = D_V$, so $v_r = -q/2\pi r$, $q = D_V/h = 1.5 \times 10^{-3}\,\mathrm{m}^{2}/\mathrm{s}$.

**2.** $rv_\theta = 0.5 \times 0.01 = 5 \times 10^{-3}\,\mathrm{m}^{2}/\mathrm{s}$: $v_\theta = \Gamma/2\pi r$ with $\Gamma = 3.1 \times 10^{-2}\,\mathrm{m}^{2}/\mathrm{s}$.

**3.** $\operatorname{div}\vect v = \frac1r\partial_r(rv_r) = 0$, $\omega_z =
\frac1r\partial_r(rv_\theta) = 0$.

**4.** $\dd r/r = -(q/\Gamma)\dd\theta$: $r = r_0\eu^{-q\theta/\Gamma}$; turns $= (\Gamma/2\pi q)\ln(r_0/a) = 3.3 \times 3.2 \approx 11$.

**5.** $t = \pi(r_0^2 - a^2)/q = 520\,\mathrm{s} \approx 9\,\mathrm{min}$; $v_\theta(a) =
0.25\,\mathrm{m}/\mathrm{s}$.

**6.** $\vect a = -(v^2/r)\vect e_r$; at $r = a$: $v^2 = 0.25^2 + 0.012^2$, $a = 3.1\,\mathrm{m}/\mathrm{s}^{2} \approx 0.3g$.

**7.** $\Omega_\oplus\sin\lambda\,r = 5 \times 10^{-5} \times 0.5 = 2.5 \times 10^{-5}\,\mathrm{m}/\mathrm{s}$, four hundred times less than the stirring: the hemisphere decides nothing in an ordinary bath (it does in a tank left still for a day).

**8.** $v_\theta = \Omega r$ ($r < a$), $\Omega a^2/r$ ($r > a$); $\Omega = 80/60
= 1.33\,\mathrm{rad}/\mathrm{s}$, $\Gamma = 2\pi av_{\max} = 3.0 \times 10^{4}\,\mathrm{m}^{2}/\mathrm{s}$.

**9.** $\omega_z = 2\Omega = 2.7\,\mathrm{s}^{-1}$ in the core, $0$ outside; $v_\theta$ rises linearly to $80\,\mathrm{m}/\mathrm{s}$ then falls as $1/r$; $\omega_z$ is a step.

**10.** $a = v_{\max}^2/a = 6400/60 = 107\,\mathrm{m}/\mathrm{s}^{2} \approx 11g$, inward.

**11.** Outside, the [vorticity](#def-b2-fluid-kinematics-vorticity) is zero: a small element translates along its circle without rotating about itself — the paddle wheel keeps its orientation. In the core (solid rotation) it turns with the fluid, once per revolution.

**12.** $E_{\text{core}} = \int_0^a\tfrac12\rho\Omega^2r^2\,2\pi r\,\dd r =
\tfrac14\pi\rho\Omega^2a^4 = 2.2 \times 10^{7}\,\mathrm{J}/\mathrm{m}$.

**13.** $E_{\text{out}} = \int_a^R\tfrac12\rho(\Omega a^2/r)^2\,2\pi r\,\dd r =
\pi\rho\Omega^2a^4\ln(R/a) = 8.7 \times 10^7 \times 4.4 = 3.8 \times 10^{8}\,\mathrm{J}/\mathrm{m}$; the integrand $\rho v^2r \propto 1/r$, hence the logarithm.

**14.** $4.0 \times 10^{8}\,\mathrm{J}/\mathrm{m} \times 1000\,\mathrm{m} = 4 \times 10^{11}\,\mathrm{J}$: about $100\,\mathrm{t}$ of TNT.

**15.** Inflow $2\pi a \times 300 \times 5 = 5.7 \times 10^{5}\,\mathrm{m}^{3}/\mathrm{s}$ through $\pi a^2 = 1.1 \times 10^{4}\,\mathrm{m}^{2}$: $v_z = 50\,\mathrm{m}/\mathrm{s}$.

**16.** $\omega = 2v_{\max}/a = 2.5 \times 10^{-3}\,\mathrm{s}^{-1} = 50f$; $\Gamma = 2\pi av_{\max}
= 1.3 \times 10^{7}\,\mathrm{m}^{2}/\mathrm{s}$.

**17.** $r_0\cdot fr_0/2 = r(v_\theta + fr/2)$: $v_\theta = f(r_0^2 - r^2)/2r$; $60\,\mathrm{m}/\mathrm{s}$ at $100\,\mathrm{km}$, $155\,\mathrm{m}/\mathrm{s}$ at $40\,\mathrm{km}$.

**18.** $f > 0$ in the northern hemisphere gives $v_\theta > 0$: counterclockwise seen from above (cyclonic). Over $500\,\mathrm{km}$ the planetary rotation is the dominant initial rotation; in a bath the stirring is.

**19.** Friction with the sea removes angular momentum, and the pressure gradient cannot balance the centripetal acceleration of an ever faster ring: the air rises before reaching the axis, in the eye wall, leaving a calm eye.

**20.** $\rho\,2\pi rHv = 1.2 \times 2\pi \times 5 \times 10^5 \times 10^3 \times 5 =
1.9 \times 10^{10}\,\mathrm{kg}/\mathrm{s}$.

**21.** $\vect v(M, t) = -U\vect e_x + \vect v_0(M + Ut\,\vect e_x)$: the pattern is advected, the field is unsteady in the ground frame. The translation adds to the swirl on the side where $v_\theta$ points west — the north (right-hand) side of the westward track.

**22.** $0.05 \times 10^7/3600 = 139\,\mathrm{m}^{3}/\mathrm{s}$; $v = 139/40 = 3.5\,\mathrm{m}/\mathrm{s}$.

**23.** $D_V = 83\,\mathrm{cm}^{3}/\mathrm{s}$: aorta $0.33\,\mathrm{m}/\mathrm{s}$; capillaries $0.33\,\mathrm{mm}/\mathrm{s}$; $3\,\mathrm{s}$ per millimetre.

**24.** $S\,\dd h/\dd t = -s\sqrt{2gh}$: $\sqrt h = \sqrt{h_0} -
\frac sS\sqrt{g/2}\,t$, empty at $T = (S/s)\sqrt{2h_0/g} = 10^4 \times 0.45 =
4500\,\mathrm{s} \approx 75\,\mathrm{min}$.

**25.** Bath: $r \sim 0.5\,\mathrm{m}$, $v \sim 1\,\mathrm{cm}/\mathrm{s}$, $\Gamma =
3 \times 10^{-2}\,\mathrm{m}^{2}/\mathrm{s}$; tornado: $60\,\mathrm{m}$, $80\,\mathrm{m}/\mathrm{s}$, $\omega = 2.7\,\mathrm{s}^{-1}$, $\Gamma = 3 \times 10^{4}\,\mathrm{m}^{2}/\mathrm{s}$; cyclone: $40\,\mathrm{km}$, $50\,\mathrm{m}/\mathrm{s}$, $\omega =
2.5 \times 10^{-3}\,\mathrm{s}^{-1}$, $\Gamma = 1.3 \times 10^{7}\,\mathrm{m}^{2}/\mathrm{s}$. In each, the angular momentum per unit mass $rv_\theta$ of the converging fluid is conserved: inflow spins it up.