atmospheric dynamics: lecture 13 - universiteit utrechtdelde102/lecture12atmdyn2014.pdfomega...

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Atmospheric Dynamics: lecture 13 (http://www.staff.science.uu.nl/~delde102/ ) Chapter 9 (part 2): Omega equa2on: interpreta2on Baroclinic waves and cyclogenesis Two level model Rossby waves and baroclinic instability Interpreta7on in terms of the Qvector

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Page 1: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Atmospheric Dynamics: lecture 13 (http://www.staff.science.uu.nl/~delde102/)

Chapter  9  (part  2):    

Omega  equa2on:  interpreta2on  

Baroclinic  waves  and  cyclogenesis  

Two  level  model    

Rossby  waves  and  baroclinic  instability  

Interpreta7on  in  terms  of  the  Q-­‐vector  

Page 2: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Quasi-geostrophic equations: Section 9.4

dg∇2Φ

dt= f0

2 ∂ω∂p

−β∂Φ∂x

dg∂Φ∂pdt

= −σω −RJcp p

Quasi-geostrophic vorticity eq.

Quasi-geostrophic thermodynamic eq.

σ ≡RpSp

Sp ≡αcp−∂T∂p

Page 3: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Quasi-geostrophic equations: Section 9.4

dg∇2Φ

dt= f0

2 ∂ω∂p

−β∂Φ∂x

dg∂Φ∂pdt

= −σω −RJcp p

Quasi-geostrophic vorticity eq.

Quasi-geostrophic thermodynamic eq.

∂ua∂x

+∂va∂y

+∂ω∂p

= 0

∂ug∂x

+∂vg∂y

= 0

Continuity equation:

Divergence of geostrophic wind = 0:

ug = −1f0∂Φ∂y;vg =

1f0∂Φ∂x

geostrophic wind and geopotential: €

σ ≡RpSp

Sp ≡αcp−∂T∂p

f ≡ f0 +βy

Page 4: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Omega equation

σ∇2ω + f02 ∂

2ω∂p2

= −2Rp ∇ ⋅ Q g

Qg1 = −∂ug

∂x∂T∂x

+∂vg

∂x∂T∂y

⎝ ⎜

⎠ ⎟ ; Qg2 = −

∂ug

∂y∂T∂x

+∂vg

∂y∂T∂y

⎝ ⎜

⎠ ⎟ .

Section 9.5

Since both T, ug and vg can all be expressed as a function of Φ, we can can calculate the vertical motion (ω) from the distribution of Φ only!!!

Page 5: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Omega equation

σ∇2ω + f02 ∂

2ω∂p2

= −2Rp ∇ ⋅ Q g

Qg1 = −∂ug

∂x∂T∂x

+∂vg

∂x∂T∂y

⎝ ⎜

⎠ ⎟ ; Qg2 = −

∂ug

∂y∂T∂x

+∂vg

∂y∂T∂y

⎝ ⎜

⎠ ⎟ .

Section 9.5

The omega equation is an elliptic partial differential equation

Since both T, ug and vg can all be expressed as a function of Φ, we can can calculate the vertical motion (ω) from the distribution of Φ only!!!

Page 6: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Omega equation

σ∇2ω + f02 ∂

2ω∂p2

= −2Rp ∇ ⋅ Q g

−ω ≈ w ≈ − ∇ ⋅

Q g

Qg1 = −∂ug

∂x∂T∂x

+∂vg

∂x∂T∂y

⎝ ⎜

⎠ ⎟ ; Qg2 = −

∂ug

∂y∂T∂x

+∂vg

∂y∂T∂y

⎝ ⎜

⎠ ⎟ .

Section 9.5

Suppose:

ω =W0 sinπppref

⎝ ⎜

⎠ ⎟ sin kx( )sin ly( )

upward (downward) motion if Qg-vector is convergent (divergent)

Page 7: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Interpretation of the solution of the omega equation

σ∇2ω + f02 ∂

2ω∂p2

= −2Rp ∇ ⋅ Q g

−ω ≈ w ≈ − ∇ ⋅

Q gupward (downward) motion if Qg-vector is convergent (divergent)

Page 8: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Omega equation

σ∇2ω + f02 ∂

2ω∂p2

= −2Rp ∇ ⋅ Q g

Qg1 = −∂ug

∂x∂T∂x

+∂vg

∂x∂T∂y

⎝ ⎜

⎠ ⎟ ; Qg2 = −

∂ug

∂y∂T∂x

+∂vg

∂y∂T∂y

⎝ ⎜

⎠ ⎟ .

Section 9.5

In the entrance of a jetstreak we may have:

∂T∂x

= 0; ∂T∂y

< 0;

∂vg

∂y< 0;

∂vg

∂y>>

∂vg

∂xArrows: Q-vectors; dashed: isotherms; solid lines: geopotential

y

x

cold

warm

descent

ascent upward motion if Qg-vector is convergent!

Page 9: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Q-vectors in mid-latitude cyclone

Based on a simulation with 36-level model of a the life cycle of an unstable baroclinic wave (details of this model simulation will be given later (see chapter 10 lecture notes)

Page 10: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

0 -5

15

1250 1200

1300

46°N

64°N

60°

1000

1400

warm sector

wf bbf

cf

Fig 1.85 (lower panel)

Page 11: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

0 -5

15

1250 1200

1300

46°N

64°N

60°

1000

1400

warm sector

wf bbf

cf Q-vector convergence

Fig 1.62 (lower panel)

Page 12: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

pe model

VERTICAL VELOCITY (w) (blue: up; red:down) and WIND VECTORTHICK CONTOURS: / /CONTOUR-INTERVAL: w: 1.0 hPa/hr /

run 2020 8 6 4 h P a 10 m/s

60.00 hrs

warm sector

46°N

64°N

bbf

cf

wf

60°

Q-vector convergence

Page 13: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Omega equation: example

−ω ≈ w ≈ − ∇ ⋅

Q gUpward motion if Q-vector is convergent

Analysis of divergence of geostrophic Q-vector at 850 hPa (thick lines, labeled in units of 10-15 K m-2 s-1) and the height of the 850 hPa surface (thin lines labeled in m) on April 4, 2001, 12 UTC.

Trough of a Rossby-wave

Upward motion downward motion

-

+

Page 14: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Satellite image

Meteosat satellite image in VIS-channel, April 4, 2001, 1200 UTC.

Upward motion

downward motion

Section 9.5

trough axis

Page 15: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Cyclogenesis and the life-cycle of a mid-latitude cyclone

About  24  hours  

March  2  1995  

March  3  1995  

Page 16: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Conceptual model

about  24-­‐4

8  hours  

Shapiro  and  Keyser  1990  

Pressure  and  fronts:  

temperature:  

Page 17: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Conceptual model

about  24-­‐4

8  hours  

Shapiro  and  Keyser  1990  

Pressure  and  fronts:  

temperature:  

Manifestation of Baroclinic instability of Rossby waves

Page 18: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Analysis of the stability of a zonal current in thermal

wind balance to wave-like perturbations

1.Model formulation 2.Model equations 3.Steady state 4.Linearization around steady state 5.Investigate dynamics of wave like perturbations

Procedure

Page 19: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Two level model

This model is an example of typical numerical weather prediction model of the 1950’s.

It contains the bare minimum of physics to produce cyclones by a process called baroclinic instability

Section 9.6

Page 20: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Two level model Unknowns are:

Φ1, Φ3 and ω2

(ψ=Φ/f0)

Section 9.6

Δp

Δp

Page 21: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Two level model

dg∇2Φ

dt= f0

2 ∂ω∂p

−β∂Φ∂x

dg∂Φ∂pdt

= −σω

Apply vorticity eq. to levels 1 and 3

Apply thermodynamic eq. to level 2

Unknowns are:

Φ1, Φ3 and ω2

(ψ=Φ/f0)

Section 9.6

Δp

Δp

Page 22: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Two level model

dg∇2Φ

dt= f0

2 ∂ω∂p

−β∂Φ∂x

dg∂Φ∂pdt

= −σω

Apply vorticity eq. to levels 1 and 3

Apply thermodynamic eq. to level 2

Unknowns are:

Φ1, Φ3 and ω2

(ψ=Φ/f0)

Section 9.6

Δp

Δp

Page 23: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Finite differences

dg∂Φ∂pdt

= −σω

⎢ ⎢ ⎢

⎥ ⎥ ⎥ 2

Apply thermodynamic equation to level 2:

(ψ=Φ/f0)

Section 9.6

Page 24: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Finite differences

dg∂Φ∂pdt

= −σω

⎢ ⎢ ⎢

⎥ ⎥ ⎥ 2

∂Φ∂p⎡

⎣ ⎢ ⎤

⎦ ⎥ 2≅Φ1 −Φ3p1 − p3

=Φ1 −Φ3Δp

Finite difference approximation of vertical derivative:

Apply thermodynamic equation to level 2:

(ψ=Φ/f0)

Section 9.6

Page 25: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Discretisation of equations

dg∇2Φ

dt= f0

2 ∂ω∂p

−β∂Φ∂x

∂∇2ψ∂t

+ v g ⋅ ∇ ∇2ψ( ) = f0

∂ω∂p

−β∂ψ∂x

v g ≡ ˆ k × ∇ ψ

(ψ=Φ/f0)

Vorticity-equation

Section 9.6

Page 26: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Discretisation of equations

dg∇2Φ

dt= f0

2 ∂ω∂p

−β∂Φ∂x

∂∇2ψ∂t

+ v g ⋅ ∇ ∇2ψ( ) = f0

∂ω∂p

−β∂ψ∂x

v g ≡ ˆ k × ∇ ψ

(ψ=Φ/f0)

∂∇2ψ1∂t

+ v 1 ⋅ ∇ ∇2ψ1( ) = f0

∂ω∂p⎡

⎣ ⎢ ⎤

⎦ ⎥ 1−β

∂ψ1∂x

Apply to level 1

Vorticity-equation

Section 9.6

Page 27: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Discretisation of equations

dg∇2Φ

dt= f0

2 ∂ω∂p

−β∂Φ∂x

∂∇2ψ∂t

+ v g ⋅ ∇ ∇2ψ( ) = f0

∂ω∂p

−β∂ψ∂x

v g ≡ ˆ k × ∇ ψ

(ψ=Φ/f0)

∂∇2ψ1∂t

+ v 1 ⋅ ∇ ∇2ψ1( ) = f0

∂ω∂p⎡

⎣ ⎢ ⎤

⎦ ⎥ 1−β

∂ψ1∂x

Apply to level 1

∂ω∂p⎡

⎣ ⎢ ⎤

⎦ ⎥ 1≅ω2 −ω0p2 − p0

=ω2Δp

Vorticity-equation

Section 9.6

Page 28: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Discretisation of equations

∂∂t

∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ + v g ⋅ ∇ ∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ = −

σf0ω

v ψ ≡ ˆ k × ∇ ψ

Thermodynamic equation

dg∂Φ∂pdt

= −σω

(ψ=Φ/f0)

Section 9.6

Page 29: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Discretisation of equations

∂∂t

∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ + v g ⋅ ∇ ∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ = −

σf0ω

v ψ ≡ ˆ k × ∇ ψ

Apply to level 2

Thermodynamic equation

dg∂Φ∂pdt

= −σω

(ψ=Φ/f0)

∂∂t

∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ 2

+ v g( )2 ⋅ ∇ ∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ 2

= −σf0ω2

Section 9.6

Page 30: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Discretisation of equations

∂∂t

∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ + v g ⋅ ∇ ∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ = −

σf0ω

v ψ ≡ ˆ k × ∇ ψ

Apply to level 2

Thermodynamic equation

dg∂Φ∂pdt

= −σω

(ψ=Φ/f0)

∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ 2≅ψ1 −ψ3p1 − p3

=ψ1 −ψ3Δp

∂∂t

∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ 2

+ v g( )2 ⋅ ∇ ∂ψ∂p⎛

⎝ ⎜

⎠ ⎟ 2

= −σf0ω2

u2 ≅12u1 +u3( ) = −

12∂∂y

ψ1 +ψ3( ),

Section 9.6

Page 31: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Steady state current + perturbation

ψ1 = −U1y +ψ '1 (x,y,t),

ψ3 = −U3y +ψ '3 (x,y,t),

ω2 =ω '2 (x,y,t),

U1 and U3 : geostrophic current

U1 and U3

Linear stability analysis of a geostrophic zonal current Section 9.7

Page 32: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Steady state current + perturbation

ψ1 = −U1y +ψ '1 (x,y,t),

ψ3 = −U3y +ψ '3 (x,y,t),

ω2 =ω '2 (x,y,t),

Substitute into equations and linearize around steady state

∂∂t

+U1∂∂x

⎛ ⎝ ⎜

⎞ ⎠ ⎟ ∇h

2ψ'1+β∂ψ'1∂x

=f0Δp

ω'2 ,€

U1 and U3 : geostrophic current

U1 and U3

e.g.:

Linear stability analysis of a geostrophic zonal current Section 9.7

Page 33: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Linearize all three equations around steady state geostrophic current

∂∂t

+U1∂∂x

⎛ ⎝ ⎜

⎞ ⎠ ⎟ ∇h

2ψ'1+β∂ψ'1∂x

=f0Δp

ω'2 ,

∂∂t

+U3∂∂x

⎛ ⎝ ⎜

⎞ ⎠ ⎟ ∇h

2ψ'3+β∂ψ'3∂x

=− f0Δp

ω'2 ,

∂∂t

+Um∂∂x

⎛ ⎝ ⎜

⎞ ⎠ ⎟ ψ'1−ψ'3( )−UT

∂∂x

ψ'1+ψ'3( ) =+σΔpf0

ω'2 ,

With

Um ≡U2 ≈U1 +U32

;UT ≡U1 −U32

(9.46)

Section 9.7

Page 34: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

∂∂t

+Um∂∂x

⎛ ⎝ ⎜

⎞ ⎠ ⎟ ∇h

2ψm + β∂ψm

∂x+UT

∂∂x∇h

2ψT = 0,

∂∂t

+Um∂∂x

⎛ ⎝ ⎜

⎞ ⎠ ⎟ ∇h

2ψT − 2λ2ψT( ) + β

∂ψT

∂x+UT

∂∂x

∇h2ψm + 2λ2ψm( ) = 0,

ψm =ψ1'+ψ3 '2

;ψT =ψ1'−ψ3 '2with

We can reduce this set of three equations to

Section 9.7

Page 35: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Substitute wave-like solutions

ψm = Aexp i lx + my −ωt( )[ ], ψT = Bexp i lx + my −ωt( )[ ]

Section 9.7

Page 36: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Substitute wave-like solutions

ψm = Aexp i lx + my −ωt( )[ ], ψT = Bexp i lx + my −ωt( )[ ]

Leads to a pair of simultaneous linear algebraic equations for the coefficients A and B:

cx −Um( )k2 + β[ ]A −UTk2B = 0

UT k2 − 2λ2( )A − cx −Um( ) k2 + 2λ2( ) + β[ ]B = 0,

k2 ≡ l2 + m2 and cx ≡ω / l.

λ2 =f02

σ Δp( )2Inverse of Rossby radius of deformation

Section 9.7

Page 37: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Dispersion relation

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

Non-trivial solutions will exist only if the determinant of the coefficients of A and B is zero. Thus the phase speed must satisfy the condition

ψm = Aexp i lx + my −ωt( )[ ], ψT = Bexp i lx + my −ωt( )[ ]Remember:

Page 38: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Dispersion relation

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

δ ≡ β2λ4

k 4 k 2+2λ 22 - UT

2 2λ 2-k 2

k 2+2λ 2 .

Non-trivial solutions will exist only if the determinant of the coefficients of A and B is zero. Thus the phase speed must satisfy the condition

ψm = Aexp i lx + my −ωt( )[ ], ψT = Bexp i lx + my −ωt( )[ ]Remember:

Page 39: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Dispersion relation

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

δ ≡ β2λ4

k 4 k 2+2λ 22 - UT

2 2λ 2-k 2

k 2+2λ 2 .

Non-trivial solutions will exist only if the determinant of the coefficients of A and B is zero. Thus the phase speed must satisfy the condition

If δ < 0, cx is imaginary⇒ exponential growth

Baroclinic instability

ψm = Aexp i lx + my −ωt( )[ ], ψT = Bexp i lx + my −ωt( )[ ]Remember:

(9.58 & 9.59)

Page 40: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Baroclinic instability in a special cases

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

δ ≡ β2λ4

k 4 k 2+2λ 22 - UT

2 2λ 2-k 2

k 2+2λ 2 .

Dispersion relation:

Section 9.7

Page 41: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Baroclinic instability in a special cases

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

δ ≡ β2λ4

k 4 k 2+2λ 22 - UT

2 2λ 2-k 2

k 2+2λ 2 .

Dispersion relation:

special case, β=0

cx =Um ±UTk2 − 2λ2

k2 + 2λ2⎛

⎝ ⎜

⎠ ⎟

1/2

Section 9.7

(9.60)

Page 42: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Baroclinic instability in a special cases

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

δ ≡ β2λ4

k 4 k 2+2λ 22 - UT

2 2λ 2-k 2

k 2+2λ 2 .

Dispersion relation:

special case, β=0

cx =Um ±UTk2 − 2λ2

k2 + 2λ2⎛

⎝ ⎜

⎠ ⎟

1/2

For waves with zonal wave numbers satisfying k2<2λ2, this expression has an imaginary part.

Section 9.7

(9.60)

Page 43: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Baroclinic instability in a special cases

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

δ ≡ β2λ4

k 4 k 2+2λ 22 - UT

2 2λ 2-k 2

k 2+2λ 2 .

Dispersion relation:

special case, β=0

cx =Um ±UTk2 − 2λ2

k2 + 2λ2⎛

⎝ ⎜

⎠ ⎟

1/2

For waves with zonal wave numbers satisfying k2<2λ2, this expression has an imaginary part. Therefore, all waves with wavelengths greater than a critical wavelength will amplify.

Section 9.7

(9.60)

Page 44: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Critical wavelength:

Lc =2πλ

≈ 3000 km

special case, β=0, continued:

Page 45: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Critical wavelength:

Lc =2πλ

≈ 3000 km

special case, UT =0:

cx =Um −βk2

cx =Um −β

k2 + 2λ2or

NO THERMAL WIND: BAROTROPIC

special case, β=0, continued:

Page 46: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Critical wavelength:

Lc =2πλ

≈ 3000 km

special case, UT =0:

cx =Um −βk2

cx =Um −β

k2 + 2λ2or

NO THERMAL WIND: BAROTROPIC

special case, β=0, continued:

This is the dispersion relation for barotropic stable Rossby waves

Page 47: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Hovemöller diagram The 500 hPa geopotential (given in dm) as a function of time and longitude. The values are average values of geopotentials between 35°N and 60°N. Ridges are shown by horizontal hatching; troughs are shown by vertical hatching. The slanted straight lines indicate a succession of maximum develop-ment of troughs and ridges (Figure 7.13).

group velocity

phase velocity

Dispersive waves!! group velocity>phase velocity

x

time

November 1945

Fig. 9.13

Section 9.7

Page 48: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Neutral stability curve

Neutral stability curve, δ=0, for the two-level baroclinic model

cx =Um −β k2 + λ2( )k2 k2 + 2λ2( )

± δ1/ 2,

δ ≡ β2λ4

k 4 k 2+2λ 22 - UT

2 2λ 2-k 2

k 2+2λ 2 .

Dispersion relation:

Section 9.7

δ=0

Page 49: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Instability: optimum wavelength

Short waves are stabilized by static stability

Long waves are stabilized by beta-effect

Section 9.7

k =2πLx

Lx = 3.8×106 m

Assuming m=0:

Page 50: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Instability: manifestation in a simplified numerical model

Geopotential, Temperature, Q-vector at 864 hPa

http://www.staff.science.uu.nl/~delde102/BaroclinicLifeCycle.htm

Page 51: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Geopotential field and Vertical motion (taken from Holton, 2004)

Given the following expression for the geopotential field:

where Φ0 is a function of p alone, c is a constant speed, l a zonal wave number, and p0=1000hPa. (a) Use the quasi-geostrophic vorticity equation to obtain the horizontal divergence field consistent with this Φ-field. (Assume df/dy=0) (b) Assuming that ω(p0)=0, obtain an expression for ω(x, y, p, t) by integrating the continuity equation with respect to pressure. (c) Sketch the geopotential fields at 750 hPa and at 250 hPa. Indicate regions of positive and negative vertical velocity at 500 hPa.

Φ =Φ0 p( ) + cf0 −y cos πp / p0( ) +1[ ]( ) + l−1 sin l x − ct( )[ ]

Problem 9.3 Homework

Comment: you will see how vertical motion is related to the geopotential wave (phase, phase speed and wavelength)

Page 52: Atmospheric Dynamics: lecture 13 - Universiteit Utrechtdelde102/Lecture12AtmDyn2014.pdfOmega equation € σ∇2ω+f 0 2∂ 2ω ∂p2 =− 2R p ∇ ⋅ Q g € Q g 1 =− ∂u g ∂x

Next week:

•  Interpretation of baroclinic instability, using the omega equation and Q-vectors

•  Solutions of the omega equation •  Numerical simulation of idealized

unstable baroclinic wave