Midterm Exam Questions for Amath/Atmos 505 and OCEAN 511 - Autumn 06 - Prof. Dale Durran, Exams of Dynamics

Midterm exam questions for the courses amath/atmos 505 and ocean 511, held in autumn 06. The questions cover topics such as buoyancy, exner function, potential temperature, boussinesq equations, vorticity, and velocity fields. Students are required to derive equations and show relationships between various quantities.

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Pre 2010

Uploaded on 03/11/2009

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AMATH/ATMOS 505, OCEAN 511—Autumn 06
Midterm/Homework 3
1. Buoyancy and alternative expressions for the pressure-gradient force: Define the
Exner function as π= (p/p00)R/cp, where pis pressure, cpis the specific heat of
air at constant pressure, Ris the gas constant for air, and p00 = 1000 mb. The
potential temperature θsatisfies πθ =T, where Tis temperature.
(a) Show that
cpθπ=p
ρ,
which provides an alternative expression for the pressure gradient force.
(b) Express the hydrostatic relation in terms of πand θ.
(c) Divide the total Exner function and potential temperature into a vertically
varying hydrostatically-balanced piece (denoted by an overbar) and a remain-
der, such that
π(x, y, z, t) = π(z) + π0(x, y , z, t),
θ(x, y, z, t) = θ(z) + θ0(x, y , z, t).
Show the the unapproximated momentum equation for inviscid flow (neglecting
Coriolis forces) may be expressed as
Du
Dt +cpθπ0=gθ0
θk
Note that this approach gives a simple exact way to relate potential temperature
perturbations to buoyancy forces.
2. As discussed in class, the Boussinesq equations
Du
Dt +P=bk,Db
Dt +N2w= 0, · u= 0,(1)
may be expressed in terms of pressure potential, buoyancy, and Brunt-V¨ais¨al¨a fre-
quency, where these quantities are defined either as
P=pp
ρ0
b=gρρ
ρ0
N2=g
ρ0
dz ,(2)
or
P=cpθ0(ππ)b=gθθ
θ0
N2=g
θ0
dz .(3)
“Derive” the Boussinesq system from the appropriate π-θform of the unapproxi-
mated governing equations. Do not do a scaling analysis as part of your derivation,
simply note what approximations are required to arrive at (1) with variables defined
by (3).
pf3

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AMATH/ATMOS 505, OCEAN 511—Autumn 06 Midterm/Homework 3

  1. Buoyancy and alternative expressions for the pressure-gradient force: Define the Exner function as π = (p/p 00 )R/cp^ , where p is pressure, cp is the specific heat of air at constant pressure, R is the gas constant for air, and p 00 = 1000 mb. The potential temperature θ satisfies πθ = T , where T is temperature.

(a) Show that cpθ∇π =

∇p ρ

which provides an alternative expression for the pressure gradient force. (b) Express the hydrostatic relation in terms of π and θ. (c) Divide the total Exner function and potential temperature into a vertically varying hydrostatically-balanced piece (denoted by an overbar) and a remain- der, such that π(x, y, z, t) = π(z) + π′(x, y, z, t), θ(x, y, z, t) = θ(z) + θ′(x, y, z, t). Show the the unapproximated momentum equation for inviscid flow (neglecting Coriolis forces) may be expressed as

Du Dt

  • cpθ∇π′^ = g θ′ θ

k

Note that this approach gives a simple exact way to relate potential temperature perturbations to buoyancy forces.

  1. As discussed in class, the Boussinesq equations

Du Dt

  • ∇P = bk, Db Dt

  • N 2 w = 0, ∇ · u = 0, (1)

may be expressed in terms of pressure potential, buoyancy, and Brunt-V¨ais¨al¨a fre- quency, where these quantities are defined either as

P =

p − p ρ 0 b = −g

ρ − ρ ρ 0

N 2 = −

g ρ 0

dρ dz

or

P = cpθ 0 (π − π) b = g θ − θ θ 0

N 2 =

g θ 0

dθ dz

“Derive” the Boussinesq system from the appropriate π-θ form of the unapproxi- mated governing equations. Do not do a scaling analysis as part of your derivation, simply note what approximations are required to arrive at (1) with variables defined by (3).

  1. Determine how the vorticity equation for inviscid barotropic flow

Dωi Dt

= (~ω · ∇)ui − (∇ · ~u)ωi.

simplifies for two dimensional flows. Let ~x = (x, y, z), ~ω = (ξ, η, ζ), and assume that all variables are independent of z and ~u = (u, v, 0).

(a) Derive (trivial) equations for ξ and η, and the equation for Dζ/Dt. (b) Under what additional conditions is ζ conserved along a Lagrangian tra- jectory following the flow?

  1. Show that for inviscid barotropic flow

D Dt

( ωi ρ

) = eij

( ωj ρ

)

. (4)

where eij is the strain rate tensor

eij =

( ∂ui ∂xj

∂uj ∂xi

) .

(a) As part of the derivation, it will be helpful to decompose ∂ui/∂xj into eij and an anti-symmetric piece that can be simplified using the relation

∂ui ∂xj

∂uj ∂xi = −ijkωk. (5)

Derive equation (5). Hint: you may wish to use the identity

ijkklm = δilδjm − δimδjl.

(b) Derive equation (4).

Interpretation: your result implies that the changes in ~ω/ρ following the flow are due to stretching and tilting of the vortex lines as the fluid element deforms. In fact as proved by Cauchy, the changes in ~ω/ρ due to flow deformation are proportional to those undergone by an infinitesimal segment of the vortex line δ`~ a the same point in the fluid.

  1. The nondivergent velocity field “induced” by (or associated with) an isolated straight vortex line of strength ζ 0 is a cylindrically circular flow around the line with tangential velocity at a distance r perpendicular to the vortex line of uT = ζ 0 /(2πr). Given this, show that the velocity field induced by a planar sheet of straight vortex lines is a piecewise uniform flow with a discontinuous jump at the vortex sheet itself, such that if the vortex sheet lies in the x-y plane z = 0, with individual vortex lines oriented parallel to the positive y-axis, then v = w = 0 and

u =

{ ζ 0 / 2 if z > 0; −ζ 0 / 2 if z < 0.