6Fluid dynamics on a rotating frame

IB Fluid Dynamics



6.1 Equations of motion in a rotating frame
The Lagrangian (particle) acceleration in a rotating frame of reference is given
by
Du
Dt
+ 2 × u + × ( × x),
as you might recall from IA Dynamics and Relativity. So we have the equation
of motion
ρ
u
t
+ u · u + 2 × u
= −∇p ρω × ( × x) + gρ.
This is complicated, so we want to simplify this. We will first compare the
centrifugal force compared to gravity. We have
|| =
2π
1 day
s
1
2π × 10
5
s
1
.
The largest scales are 10 × 10
4
km. Compared to gravity g, we have
| × ( × x)|
|g|
(2π)
2
× 10
10
. × 10
7
10
4 × 10
3
.
So the centrifugal term is tiny compared to gravity, and we will ignore it.
Alternatively, we can show that
×
(
ω × x
) can be given by a scalar potential,
and we can incorporate it into the potential term, but we will not do that.
Next, we want to get rid of the non-linear terms. We consider motions for
which
|u · u| |2 ×u|.
The scales of these two terms are U
2
/L and U respectively. So we need
R
o
=
U
L
1.
This is known as the Rossby number. In our atmosphere, we have
U 10 m s
1
and L 1 × 10
3
km. So we get
R
o
=
10
10
6
· 10
4
0.1.
So we can ignore the non-linear terms. Thus we get
Proposition (Euler’s equation in a rotating frame).
u
t
+ 2 × u =
1
ρ
p + g.
Definition
(Coriolis parameter/planetary vorticity)
.
We conventionally write
2 = f , and we call this the Coriolis parameter or the planetary vorticity.
Note that since we take the cross product of
f
with
u
, only the component
perpendicular to the velocity matters. Assuming that fluid flows along the
surface of the earth, we only need the component of
f
normal to the surface,
namely
f = 2Ω sin θ,
where θ is the angle from the equator.