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The convective approximations
Raphaël Raynaud, Ludovic Petitdemange, Emmanuel Dormy
To cite this version:
Raphaël Raynaud, Ludovic Petitdemange, Emmanuel Dormy. The convective approximations. Euro-pean GdR Dynamo, Jul 2013, Ascona, Switzerland. �hal-02428472�
The Convective Approximations
Raphaël Raynaud, Ludovic Petitdemange, Emmanuel Dormy
raphael.raynaud@ens.fr
LRA,Département de Physique, École normale supérieure
I
NTRODUCTION
Convection can occur in a shallow layer of fluid with a small temperature contrast across the layer. Thus, it is natural to hope for a simpler descrip-tion of buoyantly driven flows via an expansion of the fully compressible equations. The Boussinesq approximation performs well in modeling con-vection in laboratory experiments, but it is however unsatisfactory for large stratified systems, the lower part of which is compressed by the overly-ing material. More general approximations are then required to describe convection in natural systems like oceans, stars or planetary cores.
C
ONSERVATION LAWS
•
Mass conservation∂
tρ + ∇ · (ρV) = 0
•
Momentum conservationρD
tV = −∇P + ρg + F
νwith
g = −∇U
andF
ν= ∇ · (τ )
and
τ
ij= 2µ
1
2
(∂
iv
j+ ∂
jv
i) −
1
3
∂
kv
kδ
ijwhere
µ
is the dynamic viscosity of the fluid•
Energy conservation∂
tu
tot+ ∇ · I
tot= 0
where
u
tot= ρ E
k+ E
I+ U
(total energy)I
tot= ρV E
k+ E
H+ U
+ I
q+ I
ν (total energy flux) withE
H= E
I+ P/ρ
(specific enthalpy)I
q= −K∇T
(heat flux)I
iν= −V
jτ
ji (viscous energy flux)•
Conservation laws and the first principle of thermodynamicsd E
I= −P d ρ
−1+ T d S
lead to the heat transfert equation
ρT D
tS + ∇ · (I
q) = Q
νwith the viscous heating
Q
ν= τ
ij∇
jV
iT
HE REFERENCE STATE
Decomposition of the thermodynamics variables into the sum of a steady variable corresponding to the reference atmosphere and a convective dis-turbance
f = f
a+ f
cThe reference state must be in quasiequilibrium
•
mechanical quasiequilibrium: hydrostatic balance−∇P
a+ ρ
ag = 0
•
thermal quasiequilibrium: “well mixed” isentropic reference state∇S
a= 0
This defines the adiabatic gradient
∇T
a=
∂T
∂P
S∇P
a= α
sg =
αT
aC
pg
∇T
a=
g
C
p (in the case of a perfect gas)T
HE
B
OUSSINESQ APPROXIMATION
•
“thin layer approximation”: a dimensionless parameter must tend tozero when the size of the convective region tends to zero
•
resulting set of equations∇ · (V) = 0
D
tV = −∇Π − αT g +
µ
ρ
0∇
2V
D
tT = κ∇
2T
T
HE ANELASTIC APPROXIMATION
•
non-dimensionalizing the equations: a dimensionless parametermust tend to zero when the temperature contrast goes to zero
•
resulting set of equations∇ · (ρ
aV) = 0
D
tV = −∇
P
cρ
a− α
SS
cg + F
ν/ρ
aD
t(T
aS
c) + ∇ · (I
qa+ I
qc) − ρ
aα
SS
cV · g = Q
νN
UMERICAL IMPLEMENTATION
•
mean field approach for the heat transfert equationsplit the variables into a mean and fluctuating part,
f = hf i + f
tso that
hhf ii = hf i
andhf
ti = 0
This creates a turbulent entropy flux termI
St= ρ
ahS
tV
ti ∝ ∇Sc
Hypothesis: the turbulent diffusion of entropy dominates over the molecular diffusion of temperature in the heat transfert equation
•
assume a polytropic reference state (P ∝ ρ
γ) for a perfect gas Two additional non-Boussinesq control parameters:– the polytropic index
n = 1/(γ − 1)
– the degree of stratification
N
ρ= ln
ρa(bottom)ρa(top)
C
ONCLUSIONS
•
practical interest: filter out fast processes (acoustic/seismicpro-cesses) and retain slow processes (convection)
=⇒
low Mach approximation=⇒
faster numerical integration•
method: from a thermodynamical point of view, consider thecon-vective state as a small departure from a steady reference state References:
– Braginsky & Roberts, GAFD, 1995
– The anelastic dynamo benchmark: Jones et al., Icarus, 2011 – Brown et al., APJ, 2012
I
SSUES
•
use of a non steady reference state•
consistency and domain of validity of the different variants of theanelastic approximation