地球与空间科学 · 第 5 册 · 本科三年级

University Earth and Space Sciences — Year 3

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University Earth and Space Sciences — Year 3 · 本科三年级

19Geophysical Fluid Dynamics

Stir a cup of tea and the swirl dies in a minute; the leaves gather in the middle of the bottom and nothing else happens. The ocean and the atmosphere are stirred too, by the Sun and the wind, but on a rotating planet and in layers of different density. Rotation and stratification make them obey rules that a teacup never shows: winds blow along the isobars instead of across them, columns of fluid refuse to tilt, and the wind of the upper troposphere is written in the temperatures below it. This chapter sets up the equations of these large, slow, thin flows and the few numbers that decide which terms matter.

You already know

The Coriolis and centrifugal forces in a rotating frame, the Navier–Stokes and continuity equations, viscosity, the Reynolds number and the hydrostatic relation are in the physics books. The Coriolis parameter f=2Ωsin⁡φf = 2\Omega \sin\varphi, the pressure-gradient force, geostrophic balance, the geostrophic and gradient winds and the jet streams are in the Year 1 volume, in its chapter on the general circulation of the atmosphere; the Ekman layer in its chapter on the circulation of the ocean; potential temperature, static stability and the oscillation of a lifted air parcel in its chapter on the structure of the atmosphere and the ocean.

19.1 Equations in a rotating frame

In a frame that turns with the Earth at the angular velocity Ω⃗\vec\Omega, a fluid parcel of velocity u⃗\vec u obeys

Du⃗Dt+2Ω⃗×u⃗=−1ρ∇p+g⃗+ν∇2u⃗,∂ρ∂t+∇⋅(ρu⃗)=0,\frac{\mathrm D\vec u}{\mathrm Dt} + 2\vec\Omega\times\vec u = -\frac{1}{\rho}\nabla p + \vec g + \nu\nabla^2\vec u , \qquad \frac{\partial\rho}{\partial t} + \nabla\cdot(\rho\vec u) = 0 ,

where D/Dt=∂/∂t+u⃗⋅∇\mathrm D/\mathrm Dt = \partial/\partial t + \vec u\cdot\nabla is the derivative following the parcel and ν\nu the kinematic viscosity. The centrifugal force has been added to gravitation: their sum g⃗\vec g is the effective gravity, normal to the level surfaces of the geopotential, and the vertical is defined by it. Only the Coriolis term, −2Ω⃗×u⃗-2\vec\Omega\times \vec u, remains of the rotation, and it does no work: it turns a parcel without changing its speed. The Earth turns at Ω=7.292 115×10−5 rad/s\Omega = 7.292\,115 \times 10^{-5}\,\mathrm{rad}/\mathrm{s}, once a sidereal day of 23.9345 h23.9345\,\mathrm{h}.

For motion over distances much smaller than the Earth’s radius aa, a local Cartesian frame is enough: xx eastward, yy northward, zz upward, at the latitude φ\varphi, the tangent plane of the figure below. There Ω⃗=Ω (0,cos⁡φ,sin⁡φ)\vec\Omega = \Omega\,(0, \cos\varphi, \sin\varphi), and the three components of the momentum equation are

DuDt−fv+f~w=−1ρ∂p∂x+Fx,DvDt+fu=−1ρ∂p∂y+Fy,DwDt−f~u=−1ρ∂p∂z−g+Fz,f=2Ωsin⁡φ,f~=2Ωcos⁡φ,\begin{aligned} \frac{\mathrm Du}{\mathrm Dt} - f v + \tilde f w &= -\frac{1}{\rho}\frac{\partial p}{\partial x} + F_x ,\\ \frac{\mathrm Dv}{\mathrm Dt} + f u &= -\frac{1}{\rho}\frac{\partial p}{\partial y} + F_y ,\\ \frac{\mathrm Dw}{\mathrm Dt} - \tilde f u &= -\frac{1}{\rho}\frac{\partial p}{\partial z} - g + F_z , \end{aligned} \qquad f = 2\Omega\sin\varphi,\quad \tilde f = 2\Omega\cos\varphi ,

with F⃗\vec F the friction. For the thin, nearly horizontal flows of the ocean and the atmosphere the terms in f~\tilde f are dropped: f~w\tilde f w is small beside fvfv because w≪vw \ll v, and f~u\tilde f u is a ten-thousandth of gg (Exercise 19.5). The Coriolis force then acts only in the horizontal, through the local vertical component of the rotation, Ωsin⁡φ\Omega\sin\varphi.

Definition 19.1 (ff-plane and β\beta-plane)

Near a reference latitude φ0\varphi_0, the ff-plane approximation takes the Coriolis parameter as constant, f=f0=2Ωsin⁡φ0f = f_0 = 2\Omega\sin\varphi_0. The β\beta-plane approximation keeps its first-order change with the northward distance yy: f=f0+βyf = f_0 + \beta y, with β=df/dy=2Ωcos⁡φ0/a\beta = \mathrm df/\mathrm dy = 2\Omega \cos\varphi_0/a.

At 45∘45{}^{\circ}, with the mean radius a=6371 kma = 6371\,\mathrm{km}, f0=1.031×10−4 s−1f_0 = 1.031 \times 10^{-4}\,\mathrm{s}^{-1} and β=1.62×10−11 m−1 s−1\beta = 1.62 \times 10^{-11}\,\mathrm{m}^{-1}\,\mathrm{s}^{-1}: over 1000 km1000\,\mathrm{km} of latitude ff changes by 16 %16\,\%. The ff-plane suits motions much smaller than that; the β\beta-plane is needed for basin-wide currents and planetary waves.

Left, the local frame at latitude : z along the local vertical, y northward in the tangent plane, x eastward into the page. The rotation vector splits into  about the vertical, which turns horizontal motion, and  about the northward axis, dropped for thin flows. Right, the Coriolis parameter and its -plane tangent at 45: close over a band of latitude, far from it near the equator and the pole.
Left, the local frame at latitude : z along the local vertical, y northward in the tangent plane, x eastward into the page. The rotation vector splits into  about the vertical, which turns horizontal motion, and  about the northward axis, dropped for thin flows. Right, the Coriolis parameter and its -plane tangent at 45: close over a band of latitude, far from it near the equator and the pole.
Left, the local frame at latitude φ\varphi: zz along the local vertical, yy northward in the tangent plane, xx eastward into the page. The rotation vector splits into Ωsin⁡φ\Omega\sin\varphi about the vertical, which turns horizontal motion, and Ωcos⁡φ\Omega\cos\varphi about the northward axis, dropped for thin flows. Right, the Coriolis parameter and its β\beta-plane tangent at 45∘45{}^{\circ}: close over a band of latitude, far from it near the equator and the pole.

Two more approximations simplify the equations without losing what matters. The first concerns density.

Definition 19.2 (Boussinesq approximation)

The Boussinesq approximation writes the density as ρ=ρ0+ρ′\rho = \rho_0 + \rho', with ρ0\rho_0 a constant and ∣ρ′∣≪ρ0|\rho'| \ll \rho_0, and keeps ρ′\rho' only where it is multiplied by gg. The continuity equation becomes ∇⋅u⃗=0\nabla\cdot\vec u = 0, and the momentum equation

Du⃗Dt+f k⃗×u⃗=−1ρ0∇p′+b k⃗+ν∇2u⃗,b=−g ρ′ρ0,\frac{\mathrm D\vec u}{\mathrm Dt} + f\,\vec k\times\vec u = -\frac{1}{\rho_0}\nabla p' + b\,\vec k + \nu\nabla^2\vec u , \qquad b = -g\,\frac{\rho'}{\rho_0} ,

where p′p' is the departure of the pressure from the hydrostatic pressure of the density ρ0\rho_0, k⃗\vec k the upward unit vector and bb the buoyancy.

In the ocean ρ′\rho' is a few kg/m3\mathrm{kg}/\mathrm{m}^{3} on 10251025, a fraction of a per cent, and the approximation is excellent. In the atmosphere density falls by a factor ee in about 8.5 km8.5\,\mathrm{km}; the approximation holds for layers much thinner than that, and deeper flows replace ρ0\rho_0 by a mean profile ρ0(z)\rho_0(z), with the same physics.

The second concerns the vertical. A fluid at rest is in hydrostatic equilibrium; a fluid in motion keeps it to a very good approximation when the motion is much wider than it is deep.

Definition 19.3 (Hydrostatic approximation)

The hydrostatic approximation replaces the vertical momentum equation of a moving fluid by the hydrostatic relation, ∂p/∂z=−ρg\partial p/\partial z = -\rho g.

Proposition 19.4 (When the hydrostatic approximation holds)

For a motion of horizontal scale LL, depth HH and speed UU, with a Rossby number U/(fL)U/(fL) at most of order one, the vertical acceleration is smaller than the vertical gradient of the pressure perturbation by a factor of order (U/fL) (H/L)2(U/fL)\,(H/L)^2.

Proof. When the Coriolis force is at least as large as the acceleration, the horizontal momentum equation balances the horizontal pressure gradient against it: p′/(ρ0L)∼fUp'/(\rho_0 L) \sim fU, so p′/ρ0∼fULp'/\rho_0 \sim fUL, and the vertical gradient is p′/(ρ0H)∼fUL/Hp'/(\rho_0 H) \sim fUL/H. Continuity, ∂w/∂z=−(∂u/∂x+∂v/∂y)\partial w/\partial z = -(\partial u/\partial x + \partial v/\partial y), bounds the vertical velocity by W∼UH/LW \sim UH/L, and the vertical acceleration by Dw/Dt∼UW/L=U2H/L2\mathrm Dw/\mathrm Dt \sim UW/L = U^2H/L^2. The ratio is (U2H/L2)/(fUL/H)=(U/fL)(H/L)2(U^2H/L^2)/(fUL/H) = (U/fL)(H/L)^2. ∎

A weather system 1000 km1000\,\mathrm{km} wide in a troposphere 10 km10\,\mathrm{km} deep has (H/L)2=10−4(H/L)^2 = 10^{-4} and a Rossby number of about 0.1: the error of the hydrostatic approximation is of order 10−510^{-5}. It fails only in narrow, deep motions: a thunderstorm updraught, a convective plume in the ocean.

19.2 Scales of rotating flow

Which terms of the momentum equation matter is decided by two ratios.

Definition 19.5 (Rossby and Ekman numbers)

For a flow of speed UU, horizontal scale LL and depth HH on a planet of Coriolis parameter ff, the Rossby number is Ro=U/(fL)\mathrm{Ro} = U/(fL), the ratio of the acceleration, of order U2/LU^2/L, to the Coriolis force, of order fUfU. The Ekman number is Ek=ν/(fH2)\mathrm{Ek} = \nu/(fH^2), the ratio of the viscous force, of order νU/H2\nu U/H^2, to the Coriolis force; in a turbulent flow ν\nu is replaced by an eddy viscosity.

A bathtub draining 0.1 m/s0.1\,\mathrm{m}/\mathrm{s} over 0.3 m0.3\,\mathrm{m} has a Rossby number of some thousands: the Earth’s rotation does not decide the sense of its swirl. A depression 1000 km1000\,\mathrm{km} across with winds of 15 m/s15\,\mathrm{m}/\mathrm{s} has Ro≈0.14\mathrm{Ro} \approx 0.14, and an ocean gyre Ro∼10−4\mathrm{Ro} \sim 10^{-4}. Viscosity is weaker still: the molecular viscosity of water is 10−6 m2/s10^{-6}\,\mathrm{m}^{2}/\mathrm{s}, and the eddy viscosities that stand for the turbulence of the ocean, 10−5 to 10−3 m2/s10^{-5}\text{ to }10^{-3}\,\mathrm{m}^{2}/\mathrm{s} in the vertical, give Ek∼10−5\mathrm{Ek} \sim 10^{-5} over 1000 m1000\,\mathrm{m} of depth. The two numbers are related to the Reynolds number by Re=UL/ν=(Ro/Ek)(L/H)2\mathrm{Re} = UL/\nu = (\mathrm{Ro}/\mathrm{Ek})(L/H)^2.

When both numbers are small, the steady horizontal momentum equation keeps only the Coriolis force and the pressure gradient: the flow is in geostrophic balance, f k⃗×u⃗g=−(1/ρ)∇hpf\,\vec k\times\vec u_g = -(1/\rho)\nabla_h p, which the Year 1 volume read from weather maps. Geostrophy is the limit Ro,Ek→0\mathrm{Ro}, \mathrm{Ek}\to 0; its corrections are of order Ro\mathrm{Ro}, and friction acts only in thin layers of relative thickness Ek\sqrt{\mathrm{Ek}}, the Ekman layers at the bottom of the atmosphere and the top and bottom of the ocean. On an ff-plane the geostrophic velocity has no horizontal divergence: ∂ug/∂x+∂vg/∂y=−(1/ρf)(∂2p/∂x∂y−∂2p/∂y∂x)=0\partial u_g/\partial x + \partial v_g/\partial y = -(1/\rho f)(\partial^2 p/\partial x\partial y - \partial^2 p/\partial y\partial x) = 0 for uniform ρ\rho.

The opposite limit, rotation with no pressure gradient, is the simplest motion a rotating fluid can make.

Definition 19.6 (Inertial oscillation)

An inertial oscillation is the horizontal motion of a fluid on which no horizontal force acts but the Coriolis force.

Theorem 19.7 (Inertial circles)

On an ff-plane, a parcel set moving at speed UU with no horizontal force but the Coriolis force keeps its speed and describes a circle of radius U/∣f∣U/|f|, clockwise in the Northern Hemisphere and anticlockwise in the Southern, in the inertial period 2π/∣f∣2\pi/|f|, which is half a sidereal day divided by sin⁡φ\sin\varphi.

Proof. The equations are du/dt=fv\mathrm du/\mathrm dt = fv, dv/dt=−fu\mathrm dv/\mathrm dt = -fu. With w=u+ivw = u + \mathrm iv they read dw/dt=−if w\mathrm dw/\mathrm dt = -\mathrm if\,w, so w=U e−iftw = U\,\mathrm e^{-\mathrm ift} for a start eastward: the speed ∣w∣=U|w| = U is constant and the velocity turns at the rate ff, clockwise when f>0f > 0. Integrating, the position x+iy=(iU/f)(e−ift−1)x + \mathrm iy = (\mathrm iU/f)(\mathrm e^{-\mathrm ift} - 1) runs round the point −iU/f-\mathrm iU/f at the distance U/∣f∣U/|f|. The period is 2π/∣f∣=2π/(2Ω∣sin⁡φ∣)2\pi/|f| = 2\pi/(2\Omega|\sin\varphi|), and 2π/Ω2\pi/\Omega is the sidereal day. ∎

At 45∘45{}^{\circ} the inertial period is 16.9 h16.9\,\mathrm{h}, and a current of 0.2 m/s0.2\,\mathrm{m}/\mathrm{s} turns on a circle of 1.94 km1.94\,\mathrm{km}; at 30∘30{}^{\circ} the period is a full sidereal day, and at the equator there are no inertial circles. After a storm has set the surface layer of the ocean moving and then died, the water does exactly this. Drogued drifting buoys at 15 m15\,\mathrm{m} in the North Pacific traced loops for days after a storm in October 1987, carried along by the mean current: the third path of the figure below, after the circle and the spiral.

Paths over four days of a parcel set moving eastward at 0.2\, m/ s at 45 N (dot), with no force but the Coriolis force: a circle of radius 1.94\, km run clockwise every 16.9\, h (grey); with a friction that halves the speed in 2.8 days, an inward spiral (blue); the same carried by a steady eastward current of 0.05\, m/ s, a train of shrinking loops (red).
Paths over four days of a parcel set moving eastward at 0.2 m/s0.2\,\mathrm{m}/\mathrm{s} at 45∘45{}^{\circ} N (dot), with no force but the Coriolis force: a circle of radius 1.94 km1.94\,\mathrm{km} run clockwise every 16.9 h16.9\,\mathrm{h} (grey); with a friction that halves the speed in 2.82.8 days, an inward spiral (blue); the same carried by a steady eastward current of 0.05 m/s0.05\,\mathrm{m}/\mathrm{s}, a train of shrinking loops (red).

Between geostrophy and the inertial circle lies the flow round a centre of high or low pressure, where the isobars are curved and the acceleration towards the centre is no longer negligible.

Definition 19.8 (Gradient wind)

The gradient wind is the steady, frictionless flow along curved isobars in which the pressure-gradient force, the Coriolis force and the centripetal acceleration balance.

Proposition 19.9 (The curvature correction)

Let the isobars be circles of radius rr in the Northern Hemisphere, and VgV_g the geostrophic speed that their pressure gradient would give, with Rog=Vg/(fr)\mathrm{Ro}_g = V_g/(fr). Round a low, the gradient wind is V=2Vg/(1+1+4Rog)V = 2V_g/(1 + \sqrt{1 + 4\mathrm{Ro}_g}), slower than VgV_g; round a high, V=2Vg/(1+1−4Rog)V = 2V_g/(1 + \sqrt{1 - 4\mathrm{Ro}_g}), faster, and it exists only if Rog≤1/4\mathrm{Ro}_g \le 1/4. To first order, V=Vg(1∓Rog)V = V_g(1 \mp \mathrm{Ro}_g).

Proof. Round a low the wind turns anticlockwise; the pressure-gradient force fVgfV_g points to the centre, the Coriolis force fVfV outward, and their difference provides the centripetal acceleration: fVg−fV=V2/rfV_g - fV = V^2/r. The positive root of V2+frV−frVg=0V^2 + frV - frV_g = 0 is V=(fr/2)(1+4Rog−1)V = (fr/2)(\sqrt{1 + 4\mathrm{Ro}_g} - 1); multiplying by (1+4Rog+1)/(1+4Rog+1)(\sqrt{1 + 4\mathrm{Ro}_g} + 1)/(\sqrt{1 + 4\mathrm{Ro}_g} + 1) gives the formula. Round a high, the wind turns clockwise and the Coriolis force points inward: fV−fVg=V2/rfV - fV_g = V^2/r, so V2−frV+frVg=0V^2 - frV + frV_g = 0, which has real roots only if f2r2≥4frVgf^2r^2 \ge 4frV_g; the root that tends to VgV_g when Rog→0\mathrm{Ro}_g \to 0 is V=(fr/2)(1−1−4Rog)V = (fr/2)(1 - \sqrt{1 - 4\mathrm{Ro}_g}). Expanding the square roots, V=Vg(1∓Rog+… )V = V_g(1 \mp \mathrm{Ro}_g + \dots). ∎

The Rossby number of the isobars measures the correction: a tenth for a depression of moderate size. The condition Rog≤1/4\mathrm{Ro}_g \le 1/4 is why the centre of an anticyclone has weak gradients and light winds, while that of a depression can hold steep gradients and gales.

19.3 Rotation without stratification

A rotating fluid of uniform density, in slow motion, behaves as if it were made of rigid columns parallel to the rotation axis.

Theorem 19.10 (Taylor–Proudman)

In a steady flow of an inviscid fluid of uniform density, rotating at Ω⃗\vec\Omega, with small Rossby number, the velocity does not vary along the direction of the rotation axis: (Ω⃗⋅∇)u⃗=0(\vec\Omega\cdot\nabla)\vec u = 0.

Proof. For Ro→0\mathrm{Ro}\to 0, steady and inviscid, the momentum equation reduces to 2Ω⃗×u⃗=−∇(p/ρ0+Φ)2\vec\Omega\times\vec u = -\nabla(p/\rho_0 + \Phi), with Φ\Phi the geopotential. The curl of a gradient vanishes, so ∇×(Ω⃗×u⃗)=0\nabla\times(\vec\Omega \times\vec u) = 0. For a constant Ω⃗\vec\Omega this curl is Ω⃗(∇⋅u⃗)−(Ω⃗⋅∇)u⃗\vec\Omega (\nabla\cdot\vec u) - (\vec\Omega\cdot\nabla)\vec u, and ∇⋅u⃗=0\nabla\cdot\vec u = 0 for uniform density. ∎

With Ω⃗\vec\Omega along zz, ∂u⃗/∂z=0\partial\vec u/\partial z = 0: all three velocity components are the same at every height. If a rigid bottom forbids ww there, w=0w = 0 everywhere, and the horizontal flow is the same at every level. An obstacle on the floor of a rotating tank is therefore felt all the way to the surface: the fluid above it cannot climb over it, since that would stretch or squeeze a column, and goes round it at every height. The column of fluid that stays above the obstacle is a Taylor column.

A Taylor column (schematic). (a) In a tank of uniform water rotating rapidly, a slow flow meets a low obstacle on the floor; the fluid above the obstacle (grey) is held in place up to the surface, and the flow at every height goes round the column as if the obstacle reached the top. (b) The flow seen from above is the same at every level.
A Taylor column (schematic). (a) In a tank of uniform water rotating rapidly, a slow flow meets a low obstacle on the floor; the fluid above the obstacle (grey) is held in place up to the surface, and the flow at every height goes round the column as if the obstacle reached the top. (b) The flow seen from above is the same at every level.

The atmosphere and the ocean are stratified, and stratification relaxes the constraint: a stratified fluid can vary with height, in the way the thermal wind theorem prescribes.

19.4 Stratification and the thermal wind

The Year 1 volume lifted an air parcel in a stable atmosphere and found that it oscillates about its level. The same holds in any stratified fluid, and the frequency of the oscillation is the measure of stratification.

Definition 19.11 (Buoyancy frequency)

The buoyancy frequency NN of a fluid at rest is defined by

N2=gθdθdz (air),N2=−gρ0dρθdz (seawater),N^2 = \frac{g}{\theta}\frac{\mathrm d\theta}{\mathrm dz}\ \text{(air)}, \qquad N^2 = -\frac{g}{\rho_0}\frac{\mathrm d\rho_\theta}{\mathrm dz}\ \text{(seawater)},

where θ\theta is the potential temperature of the air and ρθ\rho_\theta the potential density of the water, the density it would have if brought adiabatically to a reference pressure.

Theorem 19.12 (Oscillation of a displaced parcel)

A parcel displaced vertically by a small distance ζ\zeta from its level in a fluid at rest, adiabatically and without mixing, obeys ζ¨=−N2ζ\ddot\zeta = -N^2\zeta. If N2>0N^2 > 0 it oscillates at the angular frequency NN; if N2<0N^2 < 0 the displacement grows and the fluid is unstable.

Proof. Moved adiabatically and without mixing, the parcel keeps its potential density ρθ(z0)\rho_\theta(z_0). At the level z0+ζz_0 + \zeta it is at the pressure of its surroundings, whose potential density is ρθ(z0)+ζ dρθ/dz\rho_\theta(z_0) + \zeta\,\mathrm d\rho_\theta/\mathrm dz; two parcels at the same pressure differ in density by the difference of their potential densities, to first order. The buoyancy force per unit mass is −g(ρp−ρe)/ρ0=g ζ (dρθ/dz)/ρ0=−N2ζ-g(\rho_p - \rho_e)/\rho_0 = g\,\zeta\,(\mathrm d\rho_\theta/\mathrm dz)/\rho_0 = -N^2\zeta. For air at a given pressure the density varies as 1/θ1/\theta, so −dρθ/ρ0=dθ/θ-\mathrm d\rho_\theta/\rho_0 = \mathrm d\theta/\theta and the two forms of N2N^2 agree. ∎

In the troposphere of the standard atmosphere, which cools by 6.49 K/km6.49\,\mathrm{K}/\mathrm{km} against the 9.77 K/km9.77\,\mathrm{K}/\mathrm{km} of the dry adiabat (g/cpg/c_p, with cp=γR/(γ−1)c_p = \gamma R/(\gamma - 1), γ=1.4\gamma = 1.4 and R=286.9 J kg−1 K−1R = 286.9\,\mathrm{J}\,\mathrm{kg}^{-1}\,\mathrm{K}^{-1}), NN averages 0.0113 s−10.0113\,\mathrm{s}^{-1}, a period of 9.3 min9.3\,\mathrm{min}; in the isothermal lower stratosphere it is 0.0210 s−10.0210\,\mathrm{s}^{-1}. In the ocean, the water column of the North Atlantic at 40.5∘40.5{}^{\circ} N, 30.5∘30.5{}^{\circ} W in the annual mean has its strongest stratification in the seasonal pycnocline, N=0.0106 s−1N = 0.0106\,\mathrm{s}^{-1} at about 30 m30\,\mathrm{m}, six cycles per hour, and much weaker values below: a few cycles per hour at most, as observed across the upper ocean.

Buoyancy frequency. Left, the standard atmosphere: nearly uniform in the troposphere, twice as large in the isothermal lower stratosphere, larger still above 25\, km where the temperature rises. Right, an annual-mean column of the North Atlantic (temperature and salinity from the World Ocean Atlas 2023, potential density from EOS-80): a sharp maximum in the seasonal pycnocline, weak stratification below.
Buoyancy frequency. Left, the standard atmosphere: nearly uniform in the troposphere, twice as large in the isothermal lower stratosphere, larger still above 25 km25\,\mathrm{km} where the temperature rises. Right, an annual-mean column of the North Atlantic (temperature and salinity from the World Ocean Atlas 2023, potential density from EOS-80): a sharp maximum in the seasonal pycnocline, weak stratification below.

Stratification lets the flow vary with height, and how it does so depends on whether the surfaces of constant density follow those of constant pressure.

Definition 19.13 (Barotropic and baroclinic fluids)

A fluid is barotropic if its density is a function of pressure alone, so that surfaces of constant density coincide with surfaces of constant pressure; it is baroclinic if they cross.

In the atmosphere, a horizontal gradient of temperature along a pressure surface makes the air baroclinic. Hydrostatic balance then makes the pressure surfaces slope more steeply with height, and geostrophic balance turns the growing slope into a growing wind.

The geometry of the thermal wind (schematic, a meridional section with the warm side to the south, p_1 > p_2 > p_3 > p_4). Warm air expands, so the layer between two pressure surfaces is thicker on the warm side than on the cold: each surface slopes down towards the cold side more steeply than the one below. The geostrophic wind is proportional to the slope, and grows with height (circles, larger for stronger wind), eastward, out of the page.
The geometry of the thermal wind (schematic, a meridional section with the warm side to the south, p1>p2>p3>p4p_1 > p_2 > p_3 > p_4). Warm air expands, so the layer between two pressure surfaces is thicker on the warm side than on the cold: each surface slopes down towards the cold side more steeply than the one below. The geostrophic wind is proportional to the slope, and grows with height (circles, larger for stronger wind), eastward, out of the page.

Theorem 19.14 (Thermal wind)

In an atmosphere in hydrostatic and geostrophic balance, the geostrophic wind varies with pressure as

∂ug∂ln⁡p=Rf(∂T∂y)p,∂vg∂ln⁡p=−Rf(∂T∂x)p.\frac{\partial u_g}{\partial\ln p} = \frac{R}{f}\left(\frac{\partial T}{\partial y}\right)_p , \qquad \frac{\partial v_g}{\partial\ln p} = -\frac{R}{f}\left(\frac{\partial T}{\partial x}\right)_p .

Between two pressure levels pb>ptp_b > p_t, the thermal wind, the difference of the geostrophic winds, is

u⃗g(pt)−u⃗g(pb)=Rf ln⁡pbpt  k⃗×∇pTˉ,\vec u_g(p_t) - \vec u_g(p_b) = \frac{R}{f}\,\ln\frac{p_b}{p_t}\;\vec k\times\nabla_p\bar T ,

where Tˉ\bar T is the mean temperature of the layer: it blows along the isotherms of the layer with the cold air on its left in the Northern Hemisphere.

Proof. On a surface of constant pressure, dp=(∂p/∂y) dy+(∂p/∂z) dz=0\mathrm dp = (\partial p/\partial y) \,\mathrm dy + (\partial p/\partial z)\,\mathrm dz = 0, and with ∂p/∂z=−ρg\partial p/\partial z = -\rho g the height zpz_p of the surface satisfies g ∂zp/∂y=(1/ρ) ∂p/∂yg\,\partial z_p/\partial y = (1/\rho)\,\partial p/\partial y. In terms of the geopotential Φ=gzp\Phi = gz_p of the surface, geostrophic balance reads fug=−∂Φ/∂yfu_g = -\partial\Phi/\partial y and fvg=∂Φ/∂xfv_g = \partial\Phi/\partial x, with the derivatives taken along the surface. The hydrostatic relation and the ideal gas law give ∂Φ/∂p=−1/ρ=−RT/p\partial\Phi/\partial p = -1/\rho = -RT/p, that is ∂Φ/∂ln⁡p=−RT\partial\Phi/\partial\ln p = -RT. Differentiating fug=−∂Φ/∂yfu_g = -\partial\Phi/\partial y with respect to ln⁡p\ln p gives f ∂ug/∂ln⁡p=R ∂T/∂yf\,\partial u_g/\partial\ln p = R\,\partial T/\partial y, and likewise for vgv_g. Integrating from pbp_b to ptp_t, ln⁡p\ln p decreases by ln⁡(pb/pt)\ln(p_b/p_t), so ug(pt)−ug(pb)=−(R/f)ln⁡(pb/pt) ∂Tˉ/∂yu_g(p_t) - u_g(p_b) = -(R/f)\ln(p_b/p_t)\,\partial\bar T/\partial y, and vg(pt)−vg(pb)=(R/f)ln⁡(pb/pt) ∂Tˉ/∂xv_g(p_t) - v_g(p_b) = (R/f)\ln(p_b/p_t)\,\partial\bar T/\partial x: these are the components of the vector form, since k⃗×∇Tˉ=(−∂Tˉ/∂y,∂Tˉ/∂x)\vec k\times\nabla\bar T = (-\partial\bar T/\partial y, \partial\bar T/\partial x). ∎

Corollary 19.15 (Thermal wind in height)

In height coordinates, for the atmosphere, ∂ug/∂z=−(g/fT) ∂T/∂y+(ug/T) ∂T/∂z\partial u_g/\partial z = -(g/fT)\,\partial T/\partial y + (u_g/T)\,\partial T/\partial z; for the ocean in the Boussinesq approximation, ∂ug/∂z=(g/fρ0) ∂ρ/∂y\partial u_g/\partial z = (g/f\rho_0)\,\partial\rho/\partial y and ∂vg/∂z=−(g/fρ0) ∂ρ/∂x\partial v_g/\partial z = -(g/f\rho_0)\,\partial\rho/\partial x.

Proof. In the air, fug=−(1/ρ)∂p/∂y=−RT ∂ln⁡p/∂yfu_g = -(1/\rho)\partial p/\partial y = -RT\,\partial\ln p/\partial y and ∂ln⁡p/∂z=−g/(RT)\partial\ln p/\partial z = -g/(RT). Then

f ∂(ug/T)∂z=−R ∂∂y∂ln⁡p∂z=g ∂(1/T)∂y=−gT2∂T∂y,f\,\frac{\partial(u_g/T)}{\partial z} = -R\,\frac{\partial}{\partial y}\frac{\partial\ln p}{\partial z} = g\,\frac{\partial(1/T)}{\partial y} = -\frac{g}{T^2}\frac{\partial T}{\partial y} ,

and expanding the left side gives the formula. In the ocean, fug=−(1/ρ0)∂p/∂yfu_g = -(1/\rho_0)\partial p/\partial y and ∂p/∂z=−ρg\partial p/\partial z = -\rho g, so f ∂ug/∂z=(g/ρ0) ∂ρ/∂yf\,\partial u_g/ \partial z = (g/\rho_0)\,\partial\rho/\partial y; likewise for vgv_g. ∎

The second term of the atmospheric form, from the decrease of temperature with height, is smaller than the first and vanishes in an isothermal layer; integrated across a layer with its mean temperature, the first term alone gives nearly the pressure form, since Δz≈(RTˉ/g)ln⁡(pb/pt)\Delta z \approx (R\bar T/g) \ln(p_b/p_t) (Problem, Part IV). In the ocean the same theorem turns a section of density across a current into its vertical shear: the basis of the dynamic method of the oceanographers.

The jet streams of the Year 1 volume are thermal winds. In the January zonal mean of 1991–2020, the westerly wind at 30∘30{}^{\circ} N grows from 4.3 m/s4.3\,\mathrm{m}/\mathrm{s} at 850 hPa850\,\mathrm{hPa} to 40.4 m/s40.4\,\mathrm{m}/\mathrm{s} at 250 hPa250\,\mathrm{hPa}; with ff at 30∘30{}^{\circ} and RR, this shear is the signature of a layer whose mean temperature falls northward by 7.5 K7.5\,\mathrm{K} per 1000 km1000\,\mathrm{km}. At 45∘45{}^{\circ} N the shear from 6.0 to 23.2 m/s6.0\text{ to }23.2\,\mathrm{m}/\mathrm{s} gives 5.0 K5.0\,\mathrm{K} per 1000 km1000\,\mathrm{km}. The figure below shows the profiles and, for each latitude, the poleward drop of temperature read from the shear: largest in the subtropics of the winter hemisphere, which is where the subtropical jet stands, 43.9 m/s43.9\,\mathrm{m}/\mathrm{s} at 200 hPa200\,\mathrm{hPa} and 30∘30{}^{\circ} N in January and 41.0 m/s41.0\,\mathrm{m}/\mathrm{s} at 30∘30{}^{\circ} S in July. Above 200 hPa200\,\mathrm{hPa} at 30∘30{}^{\circ} N the wind weakens again: the thermal wind theorem read backwards says that there, in the lower stratosphere, the temperature rises towards the pole.

Left, zonal-mean zonal wind in January (NCEP–NCAR Reanalysis 1, 1991–2020 mean) at three latitudes: the wind grows with height through the troposphere. Right, the layer-mean temperature drop towards the pole between 850\, hPa and 250\, hPa read from the wind shear by the thermal wind theorem (equatorward of 25, where geostrophy fails, left out): larger in the winter hemisphere.
Left, zonal-mean zonal wind in January (NCEP–NCAR Reanalysis 1, 1991–2020 mean) at three latitudes: the wind grows with height through the troposphere. Right, the layer-mean temperature drop towards the pole between 850 hPa850\,\mathrm{hPa} and 250 hPa250\,\mathrm{hPa} read from the wind shear by the thermal wind theorem (equatorward of 25∘25{}^{\circ}, where geostrophy fails, left out): larger in the winter hemisphere.

19.5 The Rossby radius of deformation

Rotation and stratification each impose a scale; together they impose a length.

Definition 19.16 (Rossby radius of deformation)

The Rossby radius of deformation of a layer of depth HH and buoyancy frequency NN is LR=NH/∣f∣L_R = NH/|f|.

Proposition 19.17 (Potential and kinetic energy of balanced flow)

In a hydrostatic, geostrophic flow of horizontal scale LL in a layer of depth HH and buoyancy frequency NN, the ratio of the potential energy stored in the displaced density surfaces to the kinetic energy is of order (L/LR)2(L/L_R)^2.

Proof. Geostrophy gives the pressure perturbation p′/ρ0∼fULp'/\rho_0 \sim fUL; the hydrostatic relation gives the buoyancy b∼p′/(ρ0H)∼fUL/Hb \sim p'/(\rho_0H) \sim fUL/H. A buoyancy bb in a fluid of buoyancy frequency NN means density surfaces displaced vertically by η=b/N2\eta = b/N^2, which store a potential energy per unit mass of order N2η2=b2/N2∼f2U2L2/(N2H2)N^2\eta^2 = b^2/N^2 \sim f^2U^2L^2/(N^2H^2). Divided by the kinetic energy, of order U2U^2, this is (fL/NH)2=(L/LR)2(fL/NH)^2 = (L/L_R)^2. ∎

Motions much wider than LRL_R hold most of their energy in tilted density surfaces, motions much narrower in their velocity; at LRL_R the two are equal, and the instability of baroclinic flows, which feeds on the potential energy of the tilted surfaces, grows fastest near that scale. For the troposphere, with the mean NN of the standard atmosphere, H=11 kmH = 11\,\mathrm{km} and ff at 45∘45{}^{\circ}, LR=1210 kmL_R = 1210\,\mathrm{km}: the scale of the depressions and anticyclones on a weather map. For the upper kilometre of the North Atlantic column at 40.5∘40.5{}^{\circ} N, LR=38 kmL_R = 38\,\mathrm{km}, thirty times smaller: the ocean has its own weather, eddies tens of kilometres across, and a model that resolves them needs a much finer grid. On scales near LRL_R, ff changes by βLR/f\beta L_R/f, 19 %19\,\% for the atmosphere and under one per cent for the ocean: ocean eddies live on an ff-plane, weather systems feel the β\beta-plane.

In the lab — A planet on a turntable

A rotating tank: dye spiralling round a cylinder, filmed by a camera that turns with the table (AI-generated illustration).

In a laboratory of geophysical fluid dynamics, a tank of water stands on a turntable; a camera turns with it and sees the water as an observer on a planet would. Before each run the water is left to spin up until it turns as a solid body, which takes a few minutes, many turns of the table. Then the experimenters inject dye, or move an obstacle slowly along the floor: the dye rises in a vertical column above the obstacle and the flow parts round it at every level. With a layer of fresh water over salt water, or a heated outer wall and a cooled centre, the tank becomes baroclinic, and jets, eddies and meandering fronts appear, whose size the Rossby radius of the tank predicts.

19.6 Exercises

Exercise 19.1 ★

Take Ω=7.292 115×10−5 rad/s\Omega = 7.292\,115 \times 10^{-5}\,\mathrm{rad}/\mathrm{s}. (a) Compute the Coriolis parameter and the inertial period at 30∘30{}^{\circ}, 45∘45{}^{\circ} and 60∘60{}^{\circ} N. (b) Compute the radius of the inertial circle of a current of 0.20 m/s0.20\,\mathrm{m}/\mathrm{s} at the same latitudes. (c) Compare the inertial period at 30∘30{}^{\circ} with the sidereal day, 23.9345 h23.9345\,\mathrm{h}.

Solution

Solution of Exercise 19.1.

(a) f=2Ωsin⁡φf = 2\Omega\sin\varphi: 7.292×10−57.292 \times 10^{-5}, 1.031×10−41.031 \times 10^{-4} and 1.263×10−4 s−11.263 \times 10^{-4}\,\mathrm{s}^{-1}; 2π/f2\pi/f: 23.93, 16.92 and 13.82 h13.82\,\mathrm{h}. (b) U/fU/f: 2.74, 1.94 and 1.58 km1.58\,\mathrm{km}. (c) At 30∘30{}^{\circ}, sin⁡φ=1/2\sin\varphi = 1/2 and 2π/f=2π/Ω2\pi/f = 2\pi/\Omega: the inertial period is the sidereal day, 23.93 h23.93\,\mathrm{h}.

Exercise 19.2 ★

At 45∘45{}^{\circ} N, compute the Rossby number of a dust devil (10 m/s10\,\mathrm{m}/\mathrm{s}, 10 m10\,\mathrm{m}), a sea breeze (5 m/s5\,\mathrm{m}/\mathrm{s}, 20 km20\,\mathrm{km}), a depression (15 m/s15\,\mathrm{m}/\mathrm{s}, 1000 km1000\,\mathrm{km}) and an ocean gyre (0.05 m/s0.05\,\mathrm{m}/\mathrm{s}, 2000 km2000\,\mathrm{km}). Which of them are close to geostrophic balance?

Solution

Solution of Exercise 19.2.

With f=1.031×10−4 s−1f = 1.031 \times 10^{-4}\,\mathrm{s}^{-1}: dust devil 9.7×1039.7 \times 10^{3}, sea breeze 2.4, depression 0.15, gyre 2.4×10−42.4 \times 10^{-4}. The depression and the gyre are close to geostrophic balance; the dust devil turns either way, unaware of the Earth’s rotation, and the sea breeze feels it only over a day.

Exercise 19.3 ★

At 45∘45{}^{\circ} N the mean temperature of the troposphere, 250 K250\,\mathrm{K}, falls northward by 5 K5\,\mathrm{K} per 1000 km1000\,\mathrm{km}. Using the first term of the thermal wind in height, compute the vertical shear of the westerly wind and the increase of the wind over 10 km10\,\mathrm{km}.

Solution

Solution of Exercise 19.3.

∂ug/∂z=(g/fT) ∣∂T/∂y∣=9.81×5×10−6/(1.031×10−4×250)=1.90×10−3 s−1\partial u_g/\partial z = (g/fT)\,|\partial T/\partial y| = 9.81\times 5 \times 10^{-6}/(1.031 \times 10^{-4}\times250) = 1.90 \times 10^{-3}\,\mathrm{s}^{-1}; over 10 km10\,\mathrm{km} the westerly wind increases by 19 m/s19\,\mathrm{m}/\mathrm{s}.

Exercise 19.4 ★

The stability E=−(1/ρ) dρθ/dzE = -(1/\rho)\,\mathrm d\rho_\theta/\mathrm dz of the upper kilometre of the ocean lies between 50×10−850 \times 10^{-8} and 1000×10−8 m−11000 \times 10^{-8}\,\mathrm{m}^{-1}; in deep trenches it is 10−8 m−110^{-8}\,\mathrm{m}^{-1}. Compute N=gEN = \sqrt{gE}, the period of the buoyancy oscillation and NN in cycles per hour for these three values.

Solution

Solution of Exercise 19.4.

E=50×10−8E = 50 \times 10^{-8}: N=2.21×10−3 s−1N = 2.21 \times 10^{-3}\,\mathrm{s}^{-1}, a period of 47 min47\,\mathrm{min}, 1.271.27 cycles per hour. E=1000×10−8E = 1000 \times 10^{-8}: N=9.90×10−3 s−1N = 9.90 \times 10^{-3}\,\mathrm{s}^{-1}, 10.6 min10.6\,\mathrm{min}, 5.7 cycles per hour. E=10−8E = 10^{-8}: N=3.13×10−4 s−1N = 3.13 \times 10^{-4}\,\mathrm{s}^{-1}, 5.6 h5.6\,\mathrm{h}, 0.18 cycles per hour.

Exercise 19.5 ★★

A weather system has U=10 m/sU = 10\,\mathrm{m}/\mathrm{s}, L=1000 kmL = 1000\,\mathrm{km}, H=10 kmH = 10\,\mathrm{km}, at 45∘45{}^{\circ} N. (a) Estimate its vertical velocity and its vertical acceleration, and compare the latter with gg and with the vertical gradient of the pressure perturbation, fUL/HfUL/H. (b) Compute the dropped Coriolis term f~u\tilde fu and compare it with gg.

Solution

Solution of Exercise 19.5.

(a) W∼UH/L=0.1 m/sW \sim UH/L = 0.1\,\mathrm{m}/\mathrm{s} and Dw/Dt∼UW/L=10−6 m/s2\mathrm Dw/\mathrm Dt \sim UW/L = 10^{-6}\,\mathrm{m}/\mathrm{s}^{2}, 1.0×10−71.0 \times 10^{-7} of gg. The pressure term, fUL/H=0.103 m/s2fUL/H = 0.103\,\mathrm{m}/\mathrm{s}^{2}, is larger by 1×1051 \times 10^{5}: the ratio, 9.7×10−69.7 \times 10^{-6}, is Ro(H/L)2\mathrm{Ro}(H/L)^2 with Ro=0.097\mathrm{Ro} = 0.097. (b) f~u=2Ωcos⁡45∘×10=1.03×10−3 m/s2\tilde fu = 2\Omega\cos45{}^{\circ}\times10 = 1.03 \times 10^{-3}\,\mathrm{m}/\mathrm{s}^{2}, 1.05×10−41.05 \times 10^{-4} of gg.

Exercise 19.6 ★★

Take f=10−4 s−1f = 10^{-4}\,\mathrm{s}^{-1} and circular isobars of radius 300 km300\,\mathrm{km}. (a) The pressure gradient round a low gives Vg=20 m/sV_g = 20\,\mathrm{m}/\mathrm{s}: compute the gradient wind. (b) Round a high, Vg=5 m/sV_g = 5\,\mathrm{m}/\mathrm{s}: compute the gradient wind. (c) What is the largest VgV_g possible round the high, and the wind then?

Solution

Solution of Exercise 19.6.

fr=30 m/sfr = 30\,\mathrm{m}/\mathrm{s}. (a) Rog=0.667\mathrm{Ro}_g = 0.667, V=40/(1+3.667)=13.7 m/sV = 40/(1 + \sqrt{3.667}) = 13.7\,\mathrm{m}/\mathrm{s}, a third slower than geostrophy. (b) Rog=0.167\mathrm{Ro}_g = 0.167, V=10/(1+0.333)=6.34 m/sV = 10/(1 + \sqrt{0.333}) = 6.34\,\mathrm{m}/\mathrm{s}. (c) Vg≤fr/4=7.5 m/sV_g \le fr/4 = 7.5\,\mathrm{m}/\mathrm{s}, and then V=fr/2=15 m/sV = fr/2 = 15\,\mathrm{m}/\mathrm{s}, twice the geostrophic speed.

Exercise 19.7 ★★

A tank 20 cm20\,\mathrm{cm} deep turns once every 6 s6\,\mathrm{s}; its water has ν=10−6 m2/s\nu = 10^{-6}\,\mathrm{m}^{2}/\mathrm{s}. (a) Compute f=2Ωf = 2\Omega, then the Rossby number of a flow of 1 cm/s1\,\mathrm{cm}/\mathrm{s} past a cylinder 5 cm5\,\mathrm{cm} across, and the Ekman number of the tank. Will a Taylor column form? (b) Theory gives a spin-up time H/νΩH/\sqrt{\nu\Omega}: compute it in minutes and in turns of the table.

Solution

Solution of Exercise 19.7.

(a) Ω=2π/6=1.047 rad/s\Omega = 2\pi/6 = 1.047\,\mathrm{rad}/\mathrm{s}, f=2.094 s−1f = 2.094\,\mathrm{s}^{-1}. Ro=0.01/(2.094×0.05)=0.095\mathrm{Ro} = 0.01/(2.094\times0.05) = 0.095 and Ek=10−6/(2.094×0.04)=1.19×10−5\mathrm{Ek} = 10^{-6}/(2.094\times0.04) = 1.19 \times 10^{-5}: both small, so the flow obeys the Taylor–Proudman theorem and a Taylor column forms. (b) 0.2/10−6×1.047=195 s0.2/\sqrt{10^{-6} \times1.047} = 195\,\mathrm{s}, 3.3 min3.3\,\mathrm{min}, 33 turns of the table.

Exercise 19.8 ★★

In the January zonal mean of 1991–2020 the westerly wind is 4.27 m/s4.27\,\mathrm{m}/\mathrm{s} at 850 hPa850\,\mathrm{hPa} and 40.39 m/s40.39\,\mathrm{m}/\mathrm{s} at 250 hPa250\,\mathrm{hPa} at 30∘30{}^{\circ} N, 5.99 m/s5.99\,\mathrm{m}/\mathrm{s} and 23.17 m/s23.17\,\mathrm{m}/\mathrm{s} at 45∘45{}^{\circ} N. With R=286.9 J kg−1 K−1R = 286.9\,\mathrm{J}\,\mathrm{kg}^{-1}\,\mathrm{K}^{-1}, compute the meridional gradient of the layer-mean temperature at both latitudes, and say why the jet is stronger at 30∘30{}^{\circ} N.

Solution

Solution of Exercise 19.8.

∂Tˉ/∂y=−f Δu/(Rln⁡(850/250))\partial\bar T/\partial y = -f\,\Delta u/(R\ln(850/250)), with ln⁡(850/250)=1.224\ln(850/250) = 1.224. At 30∘30{}^{\circ} N, −7.29×10−5×36.12/(286.9×1.224)=−7.50 K-7.29 \times 10^{-5}\times36.12/(286.9 \times1.224) = -7.50\,\mathrm{K} per 1000 km1000\,\mathrm{km}; at 45∘45{}^{\circ} N, −1.031×10−4×17.18/351.1=−5.05 K-1.031 \times 10^{-4}\times17.18/351.1 = -5.05\,\mathrm{K} per 1000 km1000\,\mathrm{km}. The shear is proportional to the gradient divided by ff: the gradient is 1.5 times larger at 30∘30{}^{\circ} and ff 1.4 times smaller, so the shear is 2.1 times larger.

Exercise 19.9 ★★

(a) Compute the Rossby radius of the troposphere (N=0.0113 s−1N = 0.0113\,\mathrm{s}^{-1}, H=11 kmH = 11\,\mathrm{km}, 45∘45{}^{\circ} N) and of the upper ocean (N=0.003 57 s−1N = 0.003\,57\,\mathrm{s}^{-1}, H=1000 mH = 1000\,\mathrm{m}, 40.5∘40.5{}^{\circ} N). (b) With a=6371 kma = 6371\,\mathrm{km}, compute β\beta at both latitudes and the relative change βLR/f\beta L_R/f of the Coriolis parameter over each radius.

Solution

Solution of Exercise 19.9.

(a) LR=0.0113×11 000/1.031×10−4=1206 kmL_R = 0.0113\times11\,000/1.031 \times 10^{-4} = 1206\,\mathrm{km}; 0.00357×1000/9.47×10−5=37.7 km0.00357\times1000/9.47 \times 10^{-5} = 37.7\,\mathrm{km}, 32 times smaller. (b) β=2Ωcos⁡φ/a\beta = 2\Omega\cos\varphi/a: 1.62×10−111.62 \times 10^{-11} and 1.74×10−11 m−1 s−11.74 \times 10^{-11}\,\mathrm{m}^{-1}\,\mathrm{s}^{-1}. βLR/f=0.19\beta L_R/f = 0.19 for the atmosphere, 0.007 for the ocean.

Exercise 19.10 ★★★

A parcel of the surface ocean set moving at UU is slowed by a linear friction: du/dt=fv−ru\mathrm du/\mathrm dt = fv - ru, dv/dt=−fu−rv\mathrm dv/\mathrm dt = -fu - rv. (a) Solve with w=u+ivw = u + \mathrm iv and describe the path. (b) The parcel is also carried by a steady current u0u_0 eastward: give its position. (c) At 45∘45{}^{\circ} N with U=0.2 m/sU = 0.2\,\mathrm{m}/\mathrm{s}, r−1=4 daysr^{-1} = 4\text{ days} and u0=0.05 m/su_0 = 0.05\,\mathrm{m}/\mathrm{s}, give its speed relative to the current after four days and the distance it has drifted.

Solution

Solution of Exercise 19.10.

(a) dw/dt=−(r+if)w\mathrm dw/\mathrm dt = -(r + \mathrm if)w, so w=Ue−rte−iftw = U\mathrm e^{-rt}\mathrm e^{-\mathrm ift}: the velocity turns at the rate ff while its magnitude decays as e−rt\mathrm e^{-rt}. The position x+iy=U(1−e−(r+if)t)/(r+if)x + \mathrm iy = U(1 - \mathrm e^{-(r + \mathrm if)t})/(r + \mathrm if) spirals into the point U/(r+if)U/(r + \mathrm if). (b) x+iy=U(1−e−(r+if)t)/(r+if)+u0tx + \mathrm iy = U(1 - \mathrm e^{-(r + \mathrm if)t})/(r + \mathrm if) + u_0t: the spiral is drawn out into loops. (c) 0.2 e−1=0.074 m/s0.2\,\mathrm e^{-1} = 0.074\,\mathrm{m}/\mathrm{s}; the centre has drifted u0t=0.05×4×86 400=17.3 kmu_0t = 0.05\times4\times86\,400 = 17.3\,\mathrm{km} eastward.

Exercise 19.11 ★★★

Across an ocean front at 40∘40{}^{\circ} N the density of the water increases northward by 1 kg/m31\,\mathrm{kg}/\mathrm{m}^{3} over 100 km100\,\mathrm{km}, through the upper 1000 m1000\,\mathrm{m}; below, the water is uniform and still. With ρ0=1025 kg/m3\rho_0 = 1025\,\mathrm{kg}/\mathrm{m}^{3}, compute the vertical shear of the current and the current at the surface. In which direction does it flow?

Solution

Solution of Exercise 19.11.

f=9.37×10−5 s−1f = 9.37 \times 10^{-5}\,\mathrm{s}^{-1}; ∂u/∂z=(g/fρ0) ∂ρ/∂y=9.81×10−5/(9.37×10−5×1025)=1.02×10−3 s−1\partial u/\partial z = (g/f\rho_0)\,\partial \rho/\partial y = 9.81\times10^{-5}/(9.37 \times 10^{-5}\times1025) = 1.02 \times 10^{-3}\,\mathrm{s}^{-1}. With u=0u = 0 at 1000 m1000\,\mathrm{m} the surface current is 1.02 m/s1.02\,\mathrm{m}/\mathrm{s}, eastward: in the Northern Hemisphere the current flows with the light water on its right.

Exercise 19.12 ★★★

The annual-mean column at 40.5∘40.5{}^{\circ} N, 30.5∘30.5{}^{\circ} W has potential densities σθ=ρθ−1000 kg/m3\sigma_\theta = \rho_\theta - 1000\,\mathrm{kg}/\mathrm{m}^{3} of 26.029 at the surface, 26.697 at 100 m100\,\mathrm{m}, 27.079 at 500 m500\,\mathrm{m} and 27.628 at 1000 m1000\,\mathrm{m}. (a) Compute NN in each of the three layers, in s−1\mathrm{s}^{-1} and in cycles per hour. (b) Which layer is the most stable, and why? (c) Compare the values with the range of the upper ocean in Exercise 19.4.

Solution

Solution of Exercise 19.12.

(a) N2=(g/ρ) Δσθ/ΔzN^2 = (g/\rho)\,\Delta\sigma_\theta/\Delta z. 0–100 m100\,\mathrm{m}: 9.81×0.668/(1026.4×100)9.81\times0.668/(1026.4\times100), N=7.99×10−3 s−1N = 7.99 \times 10^{-3}\,\mathrm{s}^{-1}, 4.6 cycles per hour; 100–500 m500\,\mathrm{m}: 3.02×10−3 s−13.02 \times 10^{-3}\,\mathrm{s}^{-1}, 1.7 cycles per hour; 500–1000 m1000\,\mathrm{m}: 3.24×10−3 s−13.24 \times 10^{-3}\,\mathrm{s}^{-1}, 1.9 cycles per hour. (b) The top 100 m100\,\mathrm{m}: it contains the warm surface water above the seasonal pycnocline. Between 100 and 500 m500\,\mathrm{m} the water is more uniform than below. (c) E=N2/gE = N^2/g is 650×10−8650 \times 10^{-8}, 93×10−893 \times 10^{-8} and 107×10−8 m−1107 \times 10^{-8}\,\mathrm{m}^{-1}, all within the range of the upper ocean.

19.7 Problem: Winds over the Steppe of Orrin

Problem 19.1

Weekend problem — the rotation, the stratification and the winds of an invented plain at 48∘48{}^{\circ} N

The Steppe of Orrin is a flat plain at 48∘48{}^{\circ} N with a lake, Lake Orrin, 12 km12\,\mathrm{km} wide, and a small laboratory with a rotating tank. Take Ω=7.292 115×10−5 rad/s\Omega = 7.292\,115 \times 10^{-5}\,\mathrm{rad}/\mathrm{s}, g=9.81 m/s2g = 9.81\,\mathrm{m}/\mathrm{s}^{2}, R=286.9 J kg−1 K−1R = 286.9\,\mathrm{J}\,\mathrm{kg}^{-1}\,\mathrm{K}^{-1} and cp=1004 J kg−1 K−1c_p = 1004\,\mathrm{J}\,\mathrm{kg}^{-1}\,\mathrm{K}^{-1}. All values of the steppe, its lake and its winds are invented.

Part I — Does rotation matter?

  1. Compute the Coriolis parameter and the inertial period at Orrin.
  2. Compute the Rossby number of five flows: water draining from a bathtub (0.1 m/s0.1\,\mathrm{m}/\mathrm{s} over 0.3 m0.3\,\mathrm{m}); the tank of the laboratory, which turns once every 10 s10\,\mathrm{s} (with f=2Ωtankf = 2\Omega_{\text{tank}}; 5 mm/s5\,\mathrm{mm}/\mathrm{s} over 0.2 m0.2\,\mathrm{m}); the evening breeze off the lake (5 m/s5\,\mathrm{m}/\mathrm{s}, 20 km20\,\mathrm{km}); a depression (15 m/s15\,\mathrm{m}/\mathrm{s}, 1000 km1000\,\mathrm{km}); the gyre of an ocean basin at the same latitude (0.05 m/s0.05\,\mathrm{m}/\mathrm{s}, 2000 km2000\,\mathrm{km}).
  3. Which of these flows feel the rotation that drives them, and which are close to geostrophic?
  4. Compute the Ekman number of the tank (0.2 m0.2\,\mathrm{m} deep, ν=10−6 m2/s\nu = 10^{-6}\,\mathrm{m}^{2}/\mathrm{s}), of the depression (eddy viscosity 10 m2/s10\,\mathrm{m}^{2}/\mathrm{s}, depth 10 km10\,\mathrm{km}) and of the gyre (eddy viscosity 10−3 m2/s10^{-3}\,\mathrm{m}^{2}/\mathrm{s}, depth 1000 m1000\,\mathrm{m}).
  5. The Ekman layer has the thickness δ=2ν/f\delta = \sqrt{2\nu/f}. Show that δ/H=2 Ek\delta/H = \sqrt{2\,\mathrm{Ek}} and compute δ\delta for the tank and for the air of the steppe.
  6. What do these numbers say about where friction matters?

Part II — The wind at the ground.

  1. At the ground the pressure is 1012.9 hPa1012.9\,\mathrm{hPa} and the temperature 288.1 K288.1\,\mathrm{K}. Compute the density of the air.
  2. The sea-level pressure falls northward by 4 hPa4\,\mathrm{hPa} per 300 km300\,\mathrm{km}. Compute the geostrophic wind and give its direction.
  3. The same gradient surrounds a depression whose isobars have a radius of 600 km600\,\mathrm{km}. Compute the Rossby number of the isobars and the gradient wind.
  4. The same gradient surrounds an anticyclone of the same radius. Compute the gradient wind, and the largest pressure gradient, in hPa\mathrm{hPa} per 300 km300\,\mathrm{km}, that the anticyclone can hold.

Part III — Stratification.

  1. The temperature of the troposphere falls by 6.49 K/km6.49\,\mathrm{K}/\mathrm{km}. Compute the dry adiabatic lapse rate g/cpg/c_p, and NN and the period of the buoyancy oscillation at 5 km5\,\mathrm{km}, where the temperature is 255.7 K255.7\,\mathrm{K}.
  2. Above 11 km11\,\mathrm{km} the air is isothermal at 216.6 K216.6\,\mathrm{K}. Show that N2=g2/(cpT)N^2 = g^2/(c_pT) there, and compute NN and its ratio to the value of question 11.
  3. Compute the Rossby radius of the troposphere of Orrin, with the NN of question 11 and H=10 kmH = 10\,\mathrm{km}, and compare it with the size of the depression of Part I.
  4. In summer, the upper 20 m20\,\mathrm{m} of Lake Orrin are lighter than the deep water by 1.5 kg/m31.5\,\mathrm{kg}/\mathrm{m}^{3} (ρ0=1000 kg/m3\rho_0 = 1000\,\mathrm{kg}/\mathrm{m}^{3}). Compute the reduced gravity g′=g Δρ/ρ0g' = g\,\Delta\rho/\rho_0, the speed g′h\sqrt{g'h} of the slow internal waves of the upper layer, and the Rossby radius g′h/f\sqrt{g'h}/f.
  5. Will the rotation of the Earth shape the internal motions of the lake?

Part IV — The thermal wind.

  1. Two radiosonde stations stand 600 km600\,\mathrm{km} apart on the same meridian. The mean temperature of the layer from the ground, 1013 hPa1013\,\mathrm{hPa}, to 265 hPa265\,\mathrm{hPa}, about 10 km10\,\mathrm{km}, is 253.0 K253.0\,\mathrm{K} at the southern station and 249.4 K249.4\,\mathrm{K} at the northern. Compute the meridional temperature gradient in K\mathrm{K} per 1000 km1000\,\mathrm{km}.
  2. The thickness of a layer between two pressures is Δz=(RTˉ/g)ln⁡(pb/pt)\Delta z = (R\bar T/g)\ln(p_b/p_t). Compute it at both stations, and the slope of the 265 hPa265\,\mathrm{hPa} surface relative to the ground-level one.
  3. Deduce the increase of the geostrophic wind from the ground to 265 hPa265\,\mathrm{hPa}, from that slope.
  4. Compute the same increase with the thermal wind theorem in pressure.
  5. Is the air of the steppe barotropic or baroclinic? What would the wind at 265 hPa265\,\mathrm{hPa} be if it were barotropic?
  6. Compute the increase from the first term of the thermal wind in height, with the mean temperature of the standard troposphere between 0 and 10 km10\,\mathrm{km}, 255.7 K255.7\,\mathrm{K}, and compare.
  7. Compute the wind at 541 hPa541\,\mathrm{hPa}, about 5 km5\,\mathrm{km}, assuming the temperature gradient is the same at every level.
  8. The Richardson number N2/(∂u/∂z)2N^2/(\partial u/\partial z)^2 must fall below 0.25 for the shear to drive turbulence. Compute it for the troposphere of Orrin.
  9. In January the zonal-mean westerly at 250 hPa250\,\mathrm{hPa} is 23.2 m/s23.2\,\mathrm{m}/\mathrm{s} at 45∘45{}^{\circ} N and 40.4 m/s40.4\,\mathrm{m}/\mathrm{s} at 30∘30{}^{\circ} N. Compare with the wind of Orrin, and explain why a local wind can exceed the zonal mean.
  10. Give the geostrophic wind at 10 km10\,\mathrm{km} above the Steppe of Orrin.
Solution

Solution of Problem 19.1.

1. f=2×7.292 115×10−5sin⁡48∘=1.084×10−4 s−1f = 2\times7.292\,115 \times 10^{-5}\sin48{}^{\circ} = 1.084 \times 10^{-4}\,\mathrm{s}^{-1}; 2π/f=16.1 h2\pi/f = 16.1\,\mathrm{h}.

2. Bathtub 3.1×1033.1 \times 10^{3}; tank (f=4π/10=1.257 s−1f = 4\pi/10 = 1.257\,\mathrm{s}^{-1}) 0.020; breeze 2.3; depression 0.14; gyre 2.3×10−42.3 \times 10^{-4}.

3. The bathtub feels nothing of the Earth’s rotation; the breeze feels it only after some hours. The tank, the depression and the gyre have small Rossby numbers and are close to geostrophic.

4. Tank 10−6/(1.257×0.04)=2.0×10−510^{-6}/(1.257\times0.04) = 2.0 \times 10^{-5}; depression 10/(1.084×10−4×108)=9.2×10−410/(1.084 \times 10^{-4}\times10^8) = 9.2 \times 10^{-4}; gyre 10−3/(1.084×10−4×106)=9.2×10−610^{-3}/(1.084 \times 10^{-4}\times10^6) = 9.2 \times 10^{-6}.

5. δ/H=2ν/(fH2)=2 Ek\delta/H = \sqrt{2\nu/(fH^2)} = \sqrt{2\,\mathrm{Ek}}. Tank 2×10−6/1.257=1.3 mm\sqrt{2\times10^{-6}/1.257} = 1.3\,\mathrm{mm}; air 20/1.084×10−4=430 m\sqrt{20/1.084 \times 10^{-4}} = 430\,\mathrm{m}.

6. Friction acts in layers a few thousandths of the depth in the tank and the ocean, a few hundredths in the atmosphere; above them the flow is nearly frictionless.

7. ρ=p/(RT)=101 290/(286.9×288.1)=1.225 kg/m3\rho = p/(RT) = 101\,290/(286.9\times288.1) = 1.225\,\mathrm{kg}/\mathrm{m}^{3}.

8. ug=(1/ρf) ∣∂p/∂y∣=(400/300 000)/(1.225×1.084×10−4)=10.0 m/su_g = (1/\rho f)\,|\partial p/\partial y| = (400/300\,000)/(1.225 \times1.084 \times 10^{-4}) = 10.0\,\mathrm{m}/\mathrm{s}, from the west, with the low pressure to the north on the left.

9. Rog=10.04/(1.084×10−4×600 000)=0.154\mathrm{Ro}_g = 10.04/(1.084 \times 10^{-4}\times600\,000) = 0.154; V=2×10.04/(1+1.618)=8.84 m/sV = 2\times10.04/(1 + \sqrt{1.618}) = 8.84\,\mathrm{m}/\mathrm{s}, 12 %12\,\% slower.

10. V=2×10.04/(1+0.382)=12.4 m/sV = 2\times10.04/(1 + \sqrt{0.382}) = 12.4\,\mathrm{m}/\mathrm{s}. The largest VgV_g is fr/4=16.3 m/sfr/4 = 16.3\,\mathrm{m}/\mathrm{s}, a gradient ρfVg=2.16×10−3 Pa/m\rho fV_g = 2.16 \times 10^{-3}\,\mathrm{Pa}/\mathrm{m}, 6.5 hPa6.5\,\mathrm{hPa} per 300 km300\,\mathrm{km}.

11. g/cp=9.77 K/kmg/c_p = 9.77\,\mathrm{K}/\mathrm{km}. N2=(9.81/255.7)×(9.77−6.49)×10−3=1.26×10−4 s−2N^2 = (9.81/255.7)\times(9.77 - 6.49)\times10^{-3} = 1.26 \times 10^{-4}\,\mathrm{s}^{-2}, N=0.0112 s−1N = 0.0112\,\mathrm{s}^{-1}, a period of 9.3 min9.3\,\mathrm{min}.

12. With Γ=0\Gamma = 0, N2=(g/T)(g/cp)=g2/(cpT)=4.43×10−4 s−2N^2 = (g/T)(g/c_p) = g^2/(c_pT) = 4.43 \times 10^{-4}\,\mathrm{s}^{-2}, N=0.0210 s−1N = 0.0210\,\mathrm{s}^{-1}, 1.9 times the tropospheric value.

13. LR=0.0112×104/1.084×10−4=1035 kmL_R = 0.0112\times10^4/1.084 \times 10^{-4} = 1035\,\mathrm{km}, the size of the depression.

14. g′=0.0147 m/s2g' = 0.0147\,\mathrm{m}/\mathrm{s}^{2}; g′h=0.54 m/s\sqrt{g'h} = 0.54\,\mathrm{m}/\mathrm{s}; LR=0.542/1.084×10−4=5.0 kmL_R = 0.542/1.084 \times 10^{-4} = 5.0\,\mathrm{km}.

15. Yes: the lake, 12 km12\,\mathrm{km} wide, is more than twice its Rossby radius, so its internal waves and currents are turned by the Coriolis force.

16. (249.4−253.0)/600=−6.0 K(249.4 - 253.0)/600 = -6.0\,\mathrm{K} per 1000 km1000\,\mathrm{km}.

17. ln⁡(1013/265)=1.3409\ln(1013/265) = 1.3409. South: 286.9×253.0×1.3409/9.81=9922 m286.9\times253.0\times1.3409/9.81 = 9922\,\mathrm{m}; north 9781 m9781\,\mathrm{m}. The 265 hPa265\,\mathrm{hPa} surface lies 141 m141\,\mathrm{m} lower in the north, a slope of 2.35×10−42.35 \times 10^{-4} relative to the lower surface.

18. Δu=(g/f)×slope=9.81×2.35×10−4/1.084×10−4=21.3 m/s\Delta u = (g/f)\times\text{slope} = 9.81\times2.35 \times 10^{-4}/ 1.084 \times 10^{-4} = 21.3\,\mathrm{m}/\mathrm{s}.

19. (R/f)ln⁡(pb/pt) ∣∂Tˉ/∂y∣=(286.9/1.084×10−4)×1.3409×6.0×10−6=21.3 m/s(R/f)\ln(p_b/p_t)\,|\partial\bar T/\partial y| = (286.9/1.084 \times 10^{-4})\times1.3409\times6.0 \times 10^{-6} = 21.3\,\mathrm{m}/\mathrm{s}, the same: the two calculations are one.

20. Baroclinic: the temperature, hence the density, changes along the pressure surfaces. Barotropic, the wind would not change with height: 10.0 m/s10.0\,\mathrm{m}/\mathrm{s}.

21. (g/fTˉ) ∣∂T/∂y∣ Δz=9.81×6.0×10−6×104/(1.084×10−4×255.7)=21.2 m/s(g/f\bar T)\,|\partial T/\partial y|\,\Delta z = 9.81\times 6.0 \times 10^{-6}\times10^4/(1.084 \times 10^{-4}\times255.7) = 21.2\,\mathrm{m}/\mathrm{s}, within 0.3 %0.3\,\%.

22. 10.04+(286.9/1.084×10−4)×6.0×10−6×ln⁡(1013/541)=10.04+9.96=20.0 m/s10.04 + (286.9/1.084 \times 10^{-4})\times6.0 \times 10^{-6}\times \ln(1013/541) = 10.04 + 9.96 = 20.0\,\mathrm{m}/\mathrm{s}.

23. ∂u/∂z=21.3/104=2.13×10−3 s−1\partial u/\partial z = 21.3/10^4 = 2.13 \times 10^{-3}\,\mathrm{s}^{-1}; Ri=1.26×10−4/4.54×10−6=28\mathrm{Ri} = 1.26 \times 10^{-4}/4.54 \times 10^{-6} = 28, far above 0.25: the shear does not make the free troposphere turbulent.

24. The wind of Orrin, 31 m/s31\,\mathrm{m}/\mathrm{s}, is stronger than the zonal mean at 45∘45{}^{\circ} N and weaker than at 30∘30{}^{\circ} N. The polar-front jet wanders north and south; at any moment its gradient, and its wind, is concentrated over a band, and averaging round a latitude circle spreads it out.

25. 10.0+21.310.0 + 21.3: the geostrophic wind at 10 km10\,\mathrm{km} above the steppe is 31 m/s31\,\mathrm{m}/\mathrm{s}, from the west (31.3 m/s31.3\,\mathrm{m}/\mathrm{s} by the calculation).

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