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(1)

The Equations of Motion in a Rotating Coordinate System

Chapter 3

(2)

Since the earth is rotating about its axis and since it is

convenient to adopt a frame of reference fixed in the earth, we need to study the equations of motion in a rotating

coordinate system.

Before proceeding to the formal derivation, we consider briefly two concepts which arise therein:

Effective gravity and Coriolis force

(3)

g* g g*

g

effective gravity g on a spherical earth

2R 2R

R R

effective gravity on an earth with a slight equatorial bulge g is everywhere normal to the earth’s surface

Effective Gravity

(4)

Effective Gravity

If the earth were a perfect sphere and not rotating, the only gravitational component g* would be radial.

Because the earth has a bulge and is rotating, the effective

gravitational force g is the vector sum of the normal gravity to the mass distribution g*, together with a centrifugal force

2R, and this has no tangential component at the earth’s surface.

gg * 2R

(5)

A line at rest in an inertial system A line that rotates with

the roundabout

Apparent trajectory of the ball in a rotating

coordinate system

The Coriolis force

(6)

Mathematical derivation of the Coriolis force

Representation of an arbitrary vector A(t)

i k

j

i ´

j ´ k ´

A(t) = A1(t)i + A2(t)j + A3(t)k

rotating

reference system

A(t) = A(t)i ´ + A(t)j ´ + A(t)k´

inertial

reference system

(7)

The derivative of A(t) with respect to time d

dt

dA dt

dA dt

dA dt

aA

i j k

123

the subscript “a” denotes the derivative in an inertial reference frame

In the rotating frame of reference

 

 

a 1

1

1

1

1

d dA d

A ...

dt dt dt

dA A ...

dt

d A ...

dt

  

  

  

   

  

   

A i

i

i i

i +

The time derivative of an arbitrary vector A(t)

(8)

a a + da

 

b

Unit vector perpendicular to  and a

d dt

a a b

a

 

| || |sin  

Let a be any vector rotating with angular velocity 

(9)

Position vector r(t)

O

The relative velocity in a rotating frame of reference is

u  d 

i  

j  

k  dt

dr dt

dr dt

dr dt

r

1 2 3

and

u

a

   ur

Want to calculate

u

a

 d dt

a

r

the absolute velocity of an air parcel

(10)

This air parcel starts relative to the earth with a poleward velocity V.

It begins relative to space with an additional eastwards velocity V

u

a

   ur

Example

Earth’s radius

Re

(11)

We need to calculate the absolute acceleration if we wish to apply Newton's second law

d dt

a

u

a

Measurements on the earth give only the relative velocity u and therefore the relative acceleration

d dt

u

With A = ua

d dt

d dt

a a a

a

u u

    u

u

a

   ur

d dt

d dt

a a

uu  2    u  (   r )

(12)

d dt

d dt

a a

uu  2    u  (   r )

absolute acceleration

relative acceleration

Coriolis-

acceleration Centripetal acceleration

(13)

   

    

 

( ) ( )

| |

r R

2 R

Position vector r is split up

r R

| | r  ( .r   )   R

The Centripetal acceleration is directed inwards towards the axis of rotation and has magnitude ||2R.

Centripetal acceleration

(14)

Newton’s second law in a rotating frame of reference

 d dt

a au

F In an inertial frame:

density force per

unit mass In a rotating frame:

[d ( )]

dt

u  2  u     rF

(15)

 d  

dt

u   F 2   u  (   r )

Alternative form

Coriolis force Centrifugal force

(16)

Let the total force F = g* + F´ be split up

 d  

dt

u    F g *  2   u  (   r )

  (   r )   | | 

2

R

With

gg * 

2

R

 d  

dt

u    F g  2  u

The centrifugal force associated with the earth’s rotation no longer appears explicitly in the equation; it is contained in the effective gravity.

(17)

When frictional forces can be neglected, F’ is the pressure gradient force

  

F pT per unit volume

 d  

dt

u    F g  2  u

d

dt u p

T

   1   

g 2  u

per

unit mass

This is the Euler equation in a rotating frame of reference.

total pressure

(18)

u

2  u

the Coriolis force acts normal to the

rotation vector and normal to the velocity.

is directly proportional to the magnitude of u and .

Note: the Coriolis force does no work because u ( 2  u)  0

The Coriolis force does no work

(19)

Define pT  p z0( )  p where

p0(z) and 0(z) are the reference pressure and density fields p is the perturbation pressure

Important: p0(z) and 0(z) are not uniquely defined Euler’s equation becomes

dp

dz0   g 0

D

Dtu p

u g

       

 



2 1 0

 

Perturbation pressure, buoyancy force

g = (0, 0, g)

(20)

But the total force is uniquely defined.

Important: the perturbation pressure gradient

and buoyancy forceare not uniquely defined.

1 0

p     

    g  

   0

  

 

g

 1

 p

Indeed 1 0 1 T

p      p

   g        g

(21)

A mathematical demonstration

D 1 p ' b ˆ

Dt    

u k

Momentum equation Continuity equation

  u 0

The divergence of the momentum equation gives:

   

2

p '  b ˆ 

         u u k

This is a diagnostic equation!

(22)

Newton’s 2nd law vertical component

Dw p

T

Dt z g

     

mass  acceleration = force

(23)

buoyancy form

Dw 1 p

Dt z b

   

 

pT po (z) p

(z) '

o

    

Put

Then

where

dp o

dz g

  o

where

b g   o 

   

  

(24)

buoyancy force is NOT unique

b g     o 

   

  

it depends on choice of reference density o(z)

but

1 p

T

1 p'

g b

z z

 

    

   

is unique

(25)

Buoyancy force in a hurricane

o

( ) z

o

( ) z

(26)

z



  constant

T

Initiation of a thunderstorm

(27)

 = constant

tropopause negative buoyancy

outflow

inflow

LCL LFC

original heated air

negative buoyancy positive

buoyancy

(28)

Some questions

How does the flow evolve after the original thermal has reached the upper troposphere?

What drives the updraught at low levels?

Observation in severe thunderstorms: the updraught at cloud base is negatively buoyant!

Answer: - the perturbation pressure gradient

(29)

outflow

inflow

original heated air

LFC LCL

positive buoyancy

HI HI

HI HI

LO

p'

(30)

Show Hector movie

(31)

Scale analysis

Assume a homogeneous fluid  = constant.

Euler’s equation becomes:

D

Dtu p

 2    u 1

 

U

L U P

L

2 2 

scales:

D Dt U L

U

U

L Ro u

u

/ ~ /

2 2 2

2

 

Then

Rossby number

(32)

2 = 104 s1 L = 106 m L

U = 10 ms1

U 10

Extratropical cyclone

(33)

U = 50 m/sec

2 = 5 X 105 L = 5 x 105 m

Ro U

 L 

  

2

50

5 10 5 5 105 2

Tropical cyclone

(34)

L

L = 10 - 100 m U = 10 ms1 2 = 104s1

Ro U

  10 

10 3 10 4

Dust devil

(35)
(36)

Show dust devil movie

(37)

L

L = 100 m U = 50 ms1

2 = 104s1

Ro  5 103

Waterspout

(38)

 

5

Aeroplane wing

(39)

The Rossby number

(40)

(i) Large scale meteorological and oceanic flows are strongly constrained by rotation (Ro << 1), except possibly in

equatorial regions.

(ii)Tropical cyclones are always cyclonic and appear to

derive their rotation from the background rotation of the earth. They never occur within 5 deg. of the equator

where the normal component of the earth's rotation is small.

(iii) Most tornadoes are cyclonic, but why?

(iv) Dust devils do not have a preferred sense of rotation as expected.

(v) In aerodynamic flows, and in the bath (!), the effect of the

Summary

(41)

Many of the flows we shall consider have horizontal dimensions which are small compared with the earth's radius.

In studying these, it is both legitimate and a great

simplification to assume that the earth is locally flat and to use a rectangular coordinate system with z pointing vertically upwards.

Holton (§2.3, pp31-35) shows the precise circumstances under which such an approximation is valid.

In general, the use of spherical coordinates merely refines the theory, but does not lead to a deeper understanding of the phenomena.

Coordinate systems and the earth's sphericity

(42)

equator

j i

k

Take rectangular coordinates fixed relative to the earth and centred at a point on the surface at latitude.

(43)

Ω

Ω

|Ω | sin k

|Ω | cosj

f-plane or -plane

| | cos | | sin

   

Ω Ω j Ω k

2 Ωu  | Ω | cos   j u  | Ω | sin   k u

(44)

2

2 2

2 2

  

 







 u

 

v w

u u

sin cos

sin cos

 

In component form

I will show that for middle latitude, synoptic-scale weather systems such as extra-tropical cyclones, the terms involving cos  may be neglected.

2 Ω u   2| Ω | cos    j u 2 | Ω | sin   k u

(45)

To a good approximation

2   u  2 |  |sin  ku   f u f  2 |  |sin  f  f k

Coriolis parameter

(46)

Much of the significant weather in middle latitudes is associated with extra-tropical cyclones, or depressions.

We shall base our scaling on such systems.

Let L, H, T, U, W, P and R be scales for the horizontal size, vertical extent, time, |uh|, w, perturbation pressure, and density in an extra-tropical cyclone, say at 45° latitude, where f (= 2sin  ) and 2cos  are both of order 104.

U ms W ms

L m km H m km

T L U s day P Pa mb

10 10

10 10 10 10

10 1 10 10

1 2 1

6 3 4

5 3

; ;

( ); ( );

/ ~ (~ ); ( )

and

Scale analysis of the equations for middle

latitude synoptic systems

(47)

horizontal momentum equations

Du

Dt v w p

x Dv

Dt u p

y

 

 

2 2 1

2 1

sin cos

sin

scales U2/L 2 U sin  2W cos  P/L

104 103 106 103

orders

D

Dtuh f h hp

k u   1

(48)

vertical momentum equations Dw

Dt u p

zT g

 2   1 

 cos

scales UW/L 2U cos PT/ g orders

the atmosphere is strongly hydrostatic on the synoptic scale.

negligible

7 3

10 10 10 10

(49)

Question: when we subtract the reference pressure p0 from pT, is it still legitimate to neglect Dw/Dt etc?

vertical momentum equations

Dw 1 p

2 u cos b

Dt z

      

 

scales UW/L 2U cos P/ gT/T0

orders

still negligible

7 3 1 1

10

10

 10

10

H* = height scale for a perturbation pressure difference p of 10 mb assume that H*  H

(50)

Dw 1 p

2 u cos b

Dt z

      

 

orders 107 103 101 101

0 1 p b

z

   

 

In synoptic-scale disturbances, the perturbations are in close hydrostatic balance

Remember: it is small departures from this equation which In summary

(51)

The hydrostatic approximation permits enormous simplifications in dynamical studies of large-scale

motions in the atmosphere and oceans.

The hydrostatic approximation

(52)

Summary of momentum equations

D

Dt u h f h h p

k u

     1

 0 1 p b

z

   

 

+ a continuity equation + a thermodynamic equation

(53)

End of

Chapter 3

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