Балкански 2024, Теория — Задача 3. Wind at the national weather forecast scale

Concours Général de Physique «Minko Balkanski» — 8 août 2024 · 8 август 2024 г.

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Условие

The air that makes up the Earth's atmosphere is concentrated in a layer about ten kilometers thick: the troposphere.

This air is considered to be a fluid made up of elementary domains whose horizontal dimensions in France are about a few dozen kilometers and its vertical dimensions about ten meters.

The first part of this problem presents different models of atmospheric equilibrium. The second part describes the horizontal and vertical movements of this atmosphere on a large scale and presents the so-called geostrophic wind model.

Throughout the problem, air will be considered as an ideal gas.

Horizontal velocity of the windVhV_h10ms−110ms^{-1}
Vertical velocity of the windVzV_z10−2ms−110^{-2}ms^{-1}
Timescale of horizontal and vertical movementsτ\tau105s10^5s
Scale of horizontal pressure gradients∥∇hP∥\Vert\nabla_h P\Vert10−3Nm−310^{-3}Nm^{-3}

Table 1: Characteristics of the atmosphere at medium latitudes (ϕ≈45∘\phi \approx 45^{\circ})

Some numerical values

Ideal gas constant: R=8.3Jmol−1K−1R = 8.3Jmol^{-1}K^{-1}

Atmospheric pressure at sea level: P0=105PaP_0 = 10^5Pa

Molar mass of air: Ma=29g⋅mol−1M_a = 29g \cdot mol^{-1}

Radius of the Earth: rT=6.4⋅103kmr_T = 6.4 \cdot 10^3km

Gravitational acceleration in France: g=9.8ms−2g = 9.8ms^{-2}

Typical latitude of France: ϕ=45∘\phi = 45^{\circ}

1. Atmospheric equilibrium models

We consider air in equilibrium in the terrestrial reference frame RR. Each element of this fluid is therefore in equilibrium under the action of forces external to this element, which are of two types: pressure forces and the force due to the gravitational field.

1. Air being an ideal gas, calculate its density ρ0=ρ(P0,T0)\rho_0 = \rho(P_0, T_0) under normal conditions - temperature T0=273KT_0 = 273K and pressure P=P0P = P_0.

2. We choose an orthonormal reference system in RR. The state of the atmosphere is characterized by the pressure fields P(x,y,z)P(x, y, z) and temperature fields T(x,y,z)T(x, y, z):

2. (a) Write the mechanical equilibrium condition of air subjected to pressure forces and the gravity field, assumed to be locally uniform.

2. (b) Deduce that P only depends on zz and establish the equation allowing us to determine P(z)P(z) as a function of Ma,P,g,TM_a, P, g, T and the ideal gas constant RR.

3. We first consider the atmosphere in isothermal equilibrium.

3. (a) Justify that the pressure varies with the altitude zz according to a law of the type

P(z)=P0exp(−zH)(4)P(z) = P_0exp(-\frac{z}{H}) \qquad (4)

where HH is a length called the scale height of the atmosphere to be expressed as a function of Ma,R,gM_a, R, g and TT. Calculate the scale height H0H_0 of the isothermal atmosphere at T0=273KT_0 = 273K.

3. (b) Is the assumption of uniform temperature justified?

4. We now consider the atmosphere in adiabatic equilibrium characterized at any altitude by the relation P=KργP = K\rho^{\gamma} where KK is a constant and γ=CpCv≈1.4\gamma = \frac{C_p}{C_v} \approx 1.4 is the ratio of the heat capacities at constant pressure and volume of ideal diatomic gases.

4. (a) Discuss how we can find the explicit form of P(z)P(z) and T(z)T(z). From now on we assume that their explicit forms are:

P(z)=P0(1−zγγ−1H0)γγ−1(5)P(z) = P_0(1 - \frac{z}{\frac{\gamma}{\gamma-1}H_0})^{\frac{\gamma}{\gamma-1}} \qquad (5)
T(z)=T0(1−zγγ−1H0)(6)T(z) = T_0(1 - \frac{z}{\frac{\gamma}{\gamma-1}H_0}) \qquad (6)

4. (b) Numerically calculate the vertical temperature gradient in Kkm−1Kkm^{-1} corresponding to this model of atmosphere in adiabatic equilibrium.

4. (c) Trace the general appearances of the pressure variations and its gradient as a function of altitude. (The general appearance is requested and not the precise one!)

4. (d) Numerically calculate the pressure gradient for z=0,2500z = 0, 2500 and 5000m5000m.

4. (e) From the pressure gradients found, give an order of magnitude of the scale of the vertical dimension LzL_z on which the pressure varies by 100Pa100Pa.

4. (f) Express the ratio of the air densities ρ(P,T)/ρ(P0,T0)\rho(P, T)/\rho(P_0, T_0) as a function of z,H0z, H_0 and γ\gamma. Calculate ρ\rho at 2500m2500m altitude.

2. Dynamics of atmospheric movements: the geostrophic wind

5. Figure 4 shows the isobaric lines in hPahPa and separated by 2hPa2hPa each, at sea level in Western Europe on 23 January 2002 at midnight.

Carte des isobares (en hPa) au niveau de la mer sur l'Europe de l'Ouest et l'Atlantique, Servei de Meteorologia de Catalunya ; dépression centrée vers 972 hPa à l'ouest, isobares cotées 976 à 1024, graduation de latitude 30° à 50° à droite, mentions « Pressió hPa » et « Anàlisi 00Z 23-GEN-02 ».
Figure 4 – Isobaric lines

5. (a) Determine on this pressure map the value of the horizontal pressure gradient in Bordeaux. Compare with the data in Table 1. From now on, the value of the horizontal pressure gradient used in numerical applications will be that given by Table 1.

5. (b) Knowing that we usually attribute horizontal dimensions LhL_h to elementary domains such that the horizontal pressure varies on average by 100Pa100Pa, determine an order of magnitude of LhL_h.

In the rest of the problem, we analyse on this scale.

6. (a) Give the expression of the Earth's gravitational field g→∗(r→)\overrightarrow{g}^*(\overrightarrow{r}) at a point identified by r→\overrightarrow{r} relative to the center of the Earth, assumed to be a homogeneous sphere of mass MTM_T. We will denote by GG the universal gravitational constant.

6. (b) Propose an expression giving the variation with altitude zz of the module g∗(z)=∣∣g→∗∣∣g^*(z) = ||\overrightarrow{g}^*|| as a function of the ratio zrT\frac{z}{r_T} and g∗(0)g^*(0). What is the relative error committed at 2500m2500m altitude if we replace g∗(z)g^*(z) by g0∗=g∗(0)g_0^* = g^*(0).

7. Let R0R_0 be the terrestrial barycentric, geocentric reference frame, which we will consider as Galilean, and let RlR_l be the local terrestrial reference frame, whose origin OO has latitude ϕ\phi (Figure 5). We choose OxOx tangent to the parallel passing through OO and directed towards the East, OyOy tangent to the meridian passing through OO and directed towards the North. The reference frame RlR_l is in motion with respect to R0R_0 by a uniform diurnal rotation movement of angular velocity ω\omega.

Sphère terrestre avec l'axe des pôles N–S, l'équateur et un parallèle ; au point O du parallèle, les axes x (vers l'Est), y (vers le Nord) et z (verticale, dans le prolongement d'une droite en pointillés issue du centre) ; l'angle de latitude φ est marqué au centre.
Figure 5 – Reference frames

7. (a) Specify in RlR_l the direction of the resulting acceleration Γ→E(r→)\overrightarrow{\Gamma}_E(\overrightarrow{r}). For a point of altitude zz vertically above OO, establish the expression of its modulus ΓE(z)\Gamma_E(z) as a function of ω,z,rT\omega, z, r_T and ϕ\phi. What is the relative error made on ΓE\Gamma_E at 2500m2500m altitude if we replace ΓE(z)\Gamma_E(z) by ΓE0=ΓE(0)\Gamma_{E0} = \Gamma_E(0). Calculate the typical value of ΓE0\Gamma_{E0} in France.

7. (b) Let g→(r→)\overrightarrow{g}(\overrightarrow{r}) be the local effective gravitational field, whose direction is given by that of a freely hanging pendulum. Deduce from the previous results the relationship between the gravitational field g→(r→)\overrightarrow{g}(\overrightarrow{r}), the terrestrial gravitational field g→∗(r→)\overrightarrow{g}^*(\overrightarrow{r}) and the resulting acceleration Γ→E(r→)\overrightarrow{\Gamma}_E(\overrightarrow{r}). Justify the hypothesis of a locally uniform gravitational field g→\overrightarrow{g} used in 1.

7. (c) A particle of mass mm moves at speed V→\overrightarrow{V} in RlR_l. Give the expression for the inertial acceleration due to that speed ΓC→\overrightarrow{\Gamma_C} as a function of V→\overrightarrow{V} and ω→\overrightarrow{\omega}. Express this inertial force FC→\overrightarrow{F_C} in OxyzOxyz as a function of m,ωm, \omega, of latitude ϕ\phi and of the components (Vx,Vy,Vz)(V_x, V_y, V_z) of V→\overrightarrow{V}.

8. The forces of gravity, inertia and pressure gradient act on moving atmospheric air. Write the vector equation of motion of a particle domain. Deduce the three equations giving the coordinates of the local acceleration Γ→=A→\overrightarrow{\Gamma} = \overrightarrow{A} in OxyzOxyz.

9. We first propose to study the vertical movements of air within the framework of the adiabatic equilibrium atmosphere model.

9. (a) Evaluate the orders of magnitude of the different terms located in the second term of the equation of vertical motion, using the results found in question 4.d) when placed at an altitude of 2500m2500m, for a latitude of ϕ=45∘\phi = 45^{\circ} and a wind of the order of 10ms−110ms^{-1}. What can we deduce from this about the importance of the vertical component of the inertial force due to speed?

9. (b) Observations show that apart from very brief periods of adaptation to vertical disturbances, the updrafts or downdrafts are particularly stable over time. What can we conclude from this concerning the amplitude of the vertical acceleration? From the data in Table 1, estimate the order of magnitude of the vertical acceleration. By then making the legitimate simplifications, what does the equation of vertical air motion reduce to? Conclude with regard to the results of Part 1.

10. We now study the horizontal movements of the air by placing ourselves at an altitude of 2500m2500m.

10. (a) Based on the data in Table 1, simplify the equations of horizontal motion. We define the Coriolis parameter kk by k=2ωsinϕk = 2\omega sin\phi: what are its respective numerical values at latitudes of 45∘45^{\circ} in the Northern and Southern hemispheres.

10. (b) The horizontal relative velocity is defined by Vh→=Vxex→+Vyey→\overrightarrow{V_h} = V_x\overrightarrow{e_x} + V_y\overrightarrow{e_y} . Show that the horizontal Coriolis force (the one carrying the parameter kk) per unit mass can be expressed in the form: fCh=−k(ez→∧Vh→)f_{Ch} = -k(\overrightarrow{e_z} \wedge \overrightarrow{V_h}). What can we conclude about the orientation of the vector fCh→\overrightarrow{f_{Ch}} relative to the vector Vh→\overrightarrow{V_h} in the Northern and Southern hemispheres?

10. (c) Calculate the modulus of the horizontal Coriolis force per unit mass fCh→\overrightarrow{f_{Ch}} at an altitude of 2500m2500m for which the wind has a horizontal speed of 15ms−115ms^{-1} at a latitude of 45∘45^{\circ}. Taking as the horizontal pressure gradient at the same altitude that given by Table 1, calculate the modulus of the horizontal pressure force per unit mass fPh→\overrightarrow{f_{Ph}}.

10. (d) In general, observations show that the tangential accelerations undergone by the particle domains in their horizontal movements are always very small in the large atmospheric movements in our mid-latitudes. Similarly, normal accelerations are generally very small except in front of moving depressions. Using the data in Table 1, estimate the order of magnitude of the moduli of the quantities fCh→\overrightarrow{f_{Ch}}, fPh→\overrightarrow{f_{Ph}} and of the horizontal acceleration Γh→=Ah→\overrightarrow{\Gamma_h} = \overrightarrow{A_h}. What can we conclude for the value of the vector sum fPh→+fCh→\overrightarrow{f_{Ph}} + \overrightarrow{f_{Ch}}?

11. The fictitious wind with horizontal speed Vg→\overrightarrow{V_g} which identically satisfies the equation fPh→+fCh→=0\overrightarrow{f_{Ph}} + \overrightarrow{f_{Ch}} = 0 is called geostrophic wind.

11. (a) Show that this wind is entirely determined by knowledge of the spatial distribution of pressure and express its velocity field Vg→\overrightarrow{V_g} using the horizontal pressure gradient ∇h→(P)\overrightarrow{\nabla_h}(P).

11. (b) What is the value of the acceleration Γg\Gamma_g and the local nature of the trajectory of the particles constituting the geostrophic wind? Specify on a diagram the respective orientations of Vg→\overrightarrow{V_g}, fPh→\overrightarrow{f_{Ph}} and fCh→\overrightarrow{f_{Ch}} in the Northern and Southern hemispheres.

11. (c) Given the orders of magnitude in Table 1, verify that, for the latitude of 45∘45^{\circ}, the module VgV_g of the geostrophic velocity is equal to VhV_h. Define using Figure 6 the latitude range for which the relative deviation ∣Vg−Vh∣Vh\frac{|V_g-V_h|}{V_h} remains less than 30%30\%.

Courbe décroissante de (V_g − V_h)/V_h en % (axe vertical de −40 à 120) en fonction de la latitude φ en degrés (axe horizontal de 20 à 90) : environ 107 % à 20°, nulle vers 47°, tendant vers environ −30 % à 90° ; mention « (1/ρ)‖∇_h(P)‖ = Cte ».
Figure 6 – Relative deviation as a function of latitude

11. (d) Deduce the two conditions necessary for the geostrophic wind to be a good approximation Vg→≈Vh→\overrightarrow{V_g} \approx \overrightarrow{V_h} of the real wind. Are these conditions verified at equatorial latitudes (ϕ<20∘\phi < 20^{\circ})?

Решение

Внимание: Непълно решение

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Оригинал в Архива: CGP_2024.pdf