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On the (non linear) foundations of Boussinesq approximation applicable to a thin layer of fluid
R. Perez Cordon, M. G. Velarde
To cite this version:
R. Perez Cordon, M. G. Velarde. On the (non linear) foundations of Boussinesq approxi- mation applicable to a thin layer of fluid. Journal de Physique, 1975, 36 (7-8), pp.591-601.
�10.1051/jphys:01975003607-8059100�. �jpa-00208290�
LE JOURNAL DE PHYSIQUE
ON THE (NON LINEAR) FOUNDATIONS OF BOUSSINESQ APPROXIMATION APPLICABLE
TO A THIN LAYER OF FLUID
R. PEREZ CORDON
Departamento
de FisicaUniversidad Autonoma de
Madrid,
Canto Blanco(Madrid), Spain
and M. G. VELARDE
(*)
Service de
Physique Théorique
C.E.N. de
Saclay,
BP2,
91190Gif-sur-Yvette,
France(Reçu
le3 février 1975, accepté
le 18 mars1975)
Résumé. 2014 La
description thermohydrodynamique
d’une fine couche horizontale de fluidequelconque, chauffée par le bas
(problème
deRayleigh-Bénard)
est effectuée ici par une méthodeperturbative
à deux paramètres. Aupremier
ordre de perturbation on obtient les équations ditesde Boussinesq-Oberbeck, en accord avec des résultats antérieurs de Mihaljan
[Astrophys.
J., 136 (1962)1126].
Les difficultés inhérentes à la méthode d’obtention des termes d’ordre supérieur sontici (contrairement à la théorie de Mihaljan) exclues du
développement.
Ceci est rendu possible parun choix convenable d’un champ
adiabatique
hydrostatique de référence et de deux paramètres ayant le même ordre de grandeur. Dans une limite bien précise la théorie présentée ici recouvred’anciens résultats obtenus par Malkus pour des couches de gaz dilué.
Abstract. 2014 A two-parameter
perturbation
scheme for thethermohydrodynamic
descriptionof a
horizontal layer
of a single component arbitrary fluid heated from below(Rayleigh-Bénard problem)
is presented here. The firstapproximation
leads to the Boussinesq-Oberbeck equations.This agrees with previous results obtained
by
Mihaljan[Astrophys.
J. 136(1962) 1126].
Contraryto Mihaljan’s
theory
however, the series expansion given here is free from inherent difficulties inobtaining higher
order approximations viz. non-Boussinesq effects. This is done by choosing a suitableadiabatic
hydrostatic
reference field and two parameters of the same order ofmagnitude.
In a welldefined limit the theory presented here recovers earlier results obtained by Malkus (as yet unpublished)
for dilute ideal gas layers.
Classification
Physics Abstracts
6.315
1. Introduction. - The
stability analysis
of a thinhorizontal fluid
layer
heated from below(Rayleigh-
Bénard
problem)
isgenerally
carried out within theso-called
Boussinesq [1] (1903)
or Oberbeck[2] (1888) approximation (see
for details Chandrasekhar[3]
chapter 2,
and for remarks of historicalinterest, Joseph [4]).
Thisapproximation
contains a numberof
approximations of varying importance.
For instanceviscous
dissipation
orcompressibility
effects aredisregarded,
as well as temperature variations of such (*) Permanent address : Departamento de Fisica-C-3, Univer- sidad Autonoma de Madrid, Canto Blanco (Madrid) Spain.parameters
asviscosity,
thermalconductivity
orthermal
expansion
coefficient. However viscous dissi-pation,
may beimportant
on occasions. For if thebody
force islarge
or if thelength
scale of theproblem
is
large,
viscousheating plays
a drastic role. Suchmight
be the case for convection in the earth’s mantle.On the other hand if
compressibility
effects are ofimportance they
arecomparable
inmagnitude
toviscous
heating
effects when the Gruneisen’s constant is of orderunity.
Thishappens
to be the commonsituation with standard
liquids
and gases. There is yet anotherimportant
feature of nonBoussinesq
effectsof a different nature. A drastic
qualitative
différenceArticle published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphys:01975003607-8059100
occurs in the convective cell structure of
fluids
with,a strong temperature
dependence
of theviscosity (see
for details Hoard et al.[5]) (1).
Thus one is faced with the
problem
ofassessing
therole of the
Boussinesq-Oberbeck approximation
withinthe
general thermohydrodynamic despription
of thefluid
layer. Mihaljan [6]
was thefirst author
to startlooking
at arigorous approach
tothe problem.
Partially
atleast,
he succeeded. He wasable
todefine
a
two-parameter perturbative scheme
for a rathergeneral description
of thethermohydrodynarnics
offluid
layers.
Let L and 9 berespective}y the
verticaldepth
of a horizontal fluidlayer an4 the
transversetemperature
difference. He carried arewlar change
ofvariables to two new
parameters,
say e1and qà
bothsmaller than
unity (they
are defined insection
2below).
Thelayer
is assumed of smallaspect
ratio viz.horizontally
of infinite extent. TheBoussinesq
equa- tions are obtained at theë? e’ approximation
viz.the first-order series
expansion
terms. YetMihaljan’s
scheme was ill defined. For el and e2J".tum out
to
be parameters withgreatly
different values for â standardexperimental
situation ofRayleigh-Bénard C9nvection.
It is found than for standard fluid
layers
andthermal
constraints el and 92 can be of
respective
order81 -
l0-4, e2 ~ lo- il (see section 2 fQr..
moredetails).
Thus one wonders aboutthe meaning
toascribe to
Mihaljan’s
second-orderapproximations.
This should be 2
given by
the8( 8g and gt 8j terÀii»
Yet0 0 1
03B521 03B502 » E1 el 2-
_."
The
difficulty
was discussed andsolved by
Malkus
[7].
However Malkus’sanalysis
isrçstriçted
todilute ideal gas
layers.
As neithert4
restrictedMalkus
analysis
nor itsgeneralization
hasappeared
in the literature we set ourselves te
preiblem
ofassessing Boussinesq approximation
on atirer footing.
Thus in section 2 wegive
asc,,1iemàtjc
andcritical account of
Mihaljan’s [6]
work. Section 3is devoted to the discussion of the
usefu.lÍ1ess
ofdefining
a adiabatichydrostatic reference fîcld ’(*.b.f).
A brief account of the Malkus
analyse f6r
atinte
ideal gas
layer
isgiven
in section 4. Insection
5 astraightforward generalization
ofMîhaljan’s° theory
is
presented although
it still leads to an illdefined perturbative
scheme. Ageneral perturbative scheme,
well defined at all
orders,
ispresented
inseçtion
6.However no
explicit
consideration isgiven here
toany
nôn Boussinesq
contributions.They
will be thesubject of
a separate paper.2.
Critique
ofMihaljan’s analysis (1962).
- Themost
rigorous exposition,
available up to now in theliterature,
of thegeneral thermohydrodynamic
des-criptipn pifa
horizontal thin fluidlayer leading
to theBoussinesq approximation (see
références[1, 2,
3and
8])
is that ofMihaljan [6].
Astraightforward generalization
however will beprovided
in section 5.For the sake of
completeness
and forunity
of expo- sition in this paper at present weneed,
areview,
albeit
&C1¥11Íatic,
ofMihaljan’s
work. This will aid usin the
Wfiçrstanding
of some inherent difficulties inMihaljan’% §cheme
whentrying
to account for non-Boussinesq
effects.Let us
consider
ahorizontal, single component isotropic fiuid layer
ofdepth Land
infinite horizontalextent.
Mihaljan
starts with thefollowing assumptions : i)
Thedçnsity
of the fluid is a function oftempe-
rature
l"/Í}one;
and a, thevolumetrid° expansion coefficient ’j
considered constant. Thus we have anequation pf statc
p = Po[1 - c«T - Top . (2.1)
Here
p is density. To is
some reference temperature to which a4cnsity
pocorresponds. Eq. (2.1) precludes
any
pressure dependence.
We shall find this restrictionunnecessary
in order to obtain theBoussinesq approxi- mation, ’(sep
section 5below).
ii)
Theéwific
heat at constantvolume,
the thermalconductivity K
and the shear and bulkviscosities,
denotedrespectively by
J11 and J.l2 arefunctions
oftempérature only.
Thus we have theequilibrium relations
and
Here
U denotes
the internal energy, cp thespecific
heat at
citant
pressure and P is the scalar thermo-dyna11}ÎC
pressure. We shall denote in thefollowing
0 e T -
To.
It may be useful to takeTo
as thetempérature
at the bottom of thelayer
but this neednot
necessarily
be so.With the restrictions
imposed
above thehydrody-
namic
equations
read as follows :e) A non linear steady temperature profile at rest amounts to the case of a temperature dependent conductivity.
Here a
subscript
denotes a cartesian compohent,subscript
3 represents the vertical direction.bij
is Kronecker’s delta and Einstein’s summation conventMl onrepeated
indicé is ùkdi For convenience we have introducedthe
quantity
7r , 1where Z is the numerical value of the vertical coordinate.
Eq. (2 .1 )
and the useof parameter
6 allows us to rewrite the differential system in thefollowing
wayThe
following
functions havebeing
definedWe shall now define
scaling
units : for bothspecific
heats : Co ==
cv(To).
For both viscosities /10 ae’pi(To) ;
for thermal
conductivity : Ko
=K(To).
Thug-One canexpress the material parameters in
dimensionless
form. We shall take them
primed
below.Notice
that03BC1 > p2 and one has
03BC’2
--_(03BC2/03BC0) 1, 03BC’1 =
1.The
scaling
unit for temperature is 8 *fo - Ti
where
Tl
is the temperatures at the topboundary.
Height (the only length
hereconsideted)
is §éàledby
the cent gap L. Velocities are scaled
by
V =Koi L
where a reference thermometric
conductivity
viz.thermal
diffusivity,
is definedby
xo _--Ko/Po
co. For the pressure we takePo -
poV2
and time is scaledaccording
to to =LI
V.Density
is measured in units of po. Just to fix ideas for a L = 1 cm waterlayer
and0 = 1 with
To
around 300 K onehas 10-4;
Ko 10’ uo ~ 10-2;
co -101 ; K ’ Á" 1 0-2 .
V -
10- 2 ; Po - 10-4 ;
Vo ==(po/po) £- 10-2 }.
Notice that a reference kinematic
viscosity
vo has also been introduced.’
It is
important
to observe that twoscalings
aresuperposed
in the pressure term. One comes from the upper bound of thehydrostatic
pressure variationalong
thevertical,
thisscaling being given by Po
= pogL.
The otherscaling
comes from Bemoulli’stheorem. It
gives
a maximum variation of pressure ofordre ] p/v2max
where vmax is the upper bound for thevelocity
field.Clearly
both scales are ofquite
differentorder of
magnitude.
For water in the case referred toabove one has po
V2 ~ 10-4
whereas pogL ~ 103.
We will see later that upon
evaluating
the pressuregradient
thehydrostatic
part can bedropped.
If we now
incorporate
thescaling quantités
andlook upon the
primed (dimensionless)
fieldsonly,
the
orienal eq. J2 . 8)
to(2.10)
become :We have also introduced the
following
definitions :Thus we have
eight
parameters6 is a reference Prandtl number and R --_
agOL 3/xo
vois the
Rayleigh
number. We have definedfour pimo-
nomials and
by Buckingham’s pi-theorem
weonly
have
four independent quantities.
These can be takenE1, E2, G and a. For the water
layer
referred to aboveone has the
following
estimatesfor a
Rayleigh
number of value R -103.
A
perturbative
scheme can be defined now. The obvious parameters to substitute for L and0,
are ai and e2. The transformation{ L, 0 1 --+ {
81,E2 }
isallowed as the Jacobian is
non-vanishing.
These arethe
parameters
usedby Mihaljan (1962) (2).
For easy of reference we
shall,
inexpanding,
takethe
following
convention for a function4>(el, 82),
and write
For a function
P(P’, B’)
we shall writeand so on.
Once all functions and parameters are
formally expanded
one collects the zeroth-ziroth order contri-bution,
called here the first non trivialapproximation.
One gets
We have used the definition
Notice that in the
equations
above the bulkviscosity
does not show up. Thus in the first order
approxima-
tion velocities are considered much smaller that the
speed
of sound in the fluid. Notice also thatThe eq.
(2.19)
to(2.22)
are notyet
theBoussinesq equations
asconinionly
used in the ’iiterature. Theparameters
a, cv, K and /l1 are not strict constants. Toactually
get the standardBoussinesq approximation
one must
impose
Cy = co, K ==Ko,
/l1 == po. ThusMilhaljan’s
scheme is notstrictly
consistent even at the level ofBoussinesq approximation.
This apparent gap in thelogical
framework ofMihaljan’s analysis
is overcome in section 6 below.
(2) Here and later on one of the parameters will basically be 0, the temperature difference across the fluid layer. Thus one wonders
about the relevance d: discussing turbulent behaviour for high enough Rayleigh number in a given fluid layer within the Boussinesq approximation.
It is of interest to note that the
equations
usedby
Palm
[9]
andSegel
and Stuart[10]
can be obtained from eq.(2.19)
to(2.22)
here. It suffices to return to adescription
in terms of the dimensional fields and toincorporate
a functional form pi =J-lo(1
+y8)
wherey is a parameter defined
by
these authors. Thus these authors’equations
that were assumed to describesome
non-Boussinesq
effects arise in fact fromMihaljan’s
zeroth-zeroth orderapproximation.
It is clear that when
carrying
onMihaljan’s
per- turbative scheme tohigher
orderapproximations,
nopressure
dependence
can be taken into account and yet this is not anegligible
contribution as we shownow.
For, assuming
anequation
of state likeone has for a standard fluid for a range of values
given
above
whereas for a pressure
drop
of10- 3
C.G.S. units and X -10-11, X AP - 10-8.
Such pressuredependent
terms can in fact be
disregarded
at the firstapproxima-
tion. Yet for
higher
order corrections it may not be soanymore.
Lastly,
one remarks onMihaljan’s
unfortunate selectionofparameters.
For if e1 >1,
82 » 1 one has however E1 > 92.Already
a second orderapproxi-
mation does not appear very
meaningful.
This showsan inherent
difficulty
ofMihaljan’s
scheme to describequasi-Boussinesq layers.
3.
Utility
of a référence adiabatichydrostatic
field.- Let us introduce the
following a.h.f., Pa, Ta,
Pathrough
the differentialequations (3)
Pa = Pa (Z),
p. =z(7,, Jazz Ka = Z(7,, Pi)
andTa
=Ta(z).
We have also assumed the fluidlayer
to be at rest. Define now a
perturbation
upon the a.h.f. Theperturbations
will be denoted with tildedquantities.
One has :Assuming
now for convenience in ourreasonning,
(3) In this section the third cartesian coordinate X3 will be sometimes denoted by z.
Ka
=Ko held
constant,and pa
=Po[1 - a(Ta - To)]
we get from
(3.1)
and(3.2)
Solutions of
(3. .1 b)
and(3. 2b)
are(fl
appears as anarbitrary parameter)
and
We consider now the
hydrodynamic
eq.(2.4), (2. 5)
and the energy
equation
Notice that eq.
(2.6b)
here differs fromMihaljan’s
eq.
(2.6)
in that we have notincorporated
anychange
of internal energy due to volumetric variations and K is not
Ko. Using
eq.(2.4) (2.5)
and(2. 6b)
we have forthe
perturbed
fields(3. 3)
and(3.4)
We shall now make use of the same
scaling
para- meters introduced in thepreceding
section andgive to fl
the value8/L,
constant. The two parameters el and 92 are also considered and aperturbative
schemedeveloped
for eq.(3.7)
to(3.9). Up
to the first nontrivial
approximation
one getsIn eq.
(3 .11)
we have introduced forFi’
theexpression given
in(2.22).
In retrospect eq.
(3 .10)
to(3 .12)
are in factMihaljan’s
first order eq.(2.19)
to(2.21).
Yet a fewremarks are of
pertinent
interest. Incomparing
withMihaljan’s approximation (1962)
and here eqs.(2.19)
to
(2.21))
we notice thatdropping
thehydrostatic
pressure
gradient
whencomputing
pressure variations amounts todropping
the two scales referred to earlier.Thus all terms become of the same order of
magnitude.
On the other hand
dropping
thesteady
heat fluxKo fl
in the energy
equation
leaves the internal energychanges
due to heat transferonly.
Furthermore the contributionP a v.
0 is eliminated from eq.3.12
ax, ,
. q( )
by using
eq.(3.10).
Also eq.(3.10)
to(3.12)
indeedrefer to
perturbations
upon agiven
a.h.f. solution of thehydrodynamic equations.
All terms in theseequations
arenumerically
alike. This is not so inMihaljan’s equations.
Also in order to understand now the
utility
ofMihaljan’s
scheme weproceed
as follows. Let thea.h.f. be
given by
eq.(3.5)
and(3.6).
Astraight-
forward
perturbative analysis
will now begiven.
Lettilded
quantities again
denoteperturbation
upon the a.h.f. of reference. A directprocedure
is toproceed
like Chandrasekhar
(1961) (Chap. 2).
Thus oneagain,
gets up to first order in the tildedquantities,
the firsteq.
(3.10),
but for the Navier-Stokesequation
onenow gets
where F* represents the part of F that comes from
expanding p(T, P)
in theperturbations T
andP.
For the energy
equation
one getsOne notices that with such a
straightforward
methodwe
drop
the convective terms from eq.(3 .11 b)
and(3.12b).
This is to beexpected
as for theexample
given
in section 2above,
one has thefollowing
esti-mates
However these convective terms remain in
Mihaljan’s
first order
approximation.
On the other handf3V3
appears in eq.
(2.12b).
Thus this latter methoddeveloped
here is not consistent with dimensionalanalysis
of theproblem.
Nor is it consistent withan actual numerical estimate of the contributions.
From this
point
of viewMihaljan’s analysis
whenadequately supplemented
with a reference a.h.f. is a more suitableapproach.
The inherent difficulties referred to above still remainthough.
For this reasonwe now tum our attention to an
analysis developed by
Malkus
[7].
4.
Analysis
of a schemeproposed by
Malkus(1964).
- In this section we discuss the
approach developed by
Malkus[7]
for a dilute ideal gaslayer.
We shallagain
get theBoussinesq equations.
But we shallalso
gain insight into
theprocedure
to be followed in ageneral description given
in section 6.The
starting pqint
isagain
the set ofhydrodynamic
eq.
(2.4)
to(2.6)
but based on thefollowing equations
of state
(M :
molecularweight, Ro :
gases universalconstant)
Malkus
proceeds
to define a reference a.h.f.through
the differential
equations
This amounts to a local adiabatic condition
imposed
upon the
equation
of state. From eq.(4.3)
and(4.4)
one gets the relations ’
The
following
relation holdsOne now assumes that the unknown fields are local
perturbed
fields upon the a.h.f. of reference. Thus weconsider
again
eq.(3.3)
and(3.4) together
with thecorresponding equation
for p.Upon
substitution of theperturbed quantities
into eq.(2.4)
to(2 , 6)
one gets a differential system for the tildedquantities
interms of the a.h.f. variables. One then introduces
scaling
units as done in section 2. Thelength
arescaled with L ; velocities with an upper bound for
buoyant
verticalvelocity V
=(gL AI/T^)1/2;
timewith
L/ V
andviscosity
with po =u(To).
Needless tosay the
only viscosity
here considered is the shearviscosity !
As done before we denote the new dimensionless
quantities
withprimes.
With the a.h.f. the vertical temperature difference across thelayer
ofheight
z’ =
1, is
Eq. (4. 8)
defines fi. The valueAT.
isindependent
of theactual temperature difference 9 between boundaries.
In fact this temperature difference can be
thought
of asa
perturbation
upon the a.h. temperature ; one hasAlready
the a.h. fields can be recast intoprimed quantities by using
themonomial il
defined above.One has
where a second monomial has been introduced
S = R/cp.
Po
V2 ;
Pressure can be scaled with po
V2 ;
temperature withTo
e(where
8 *ATITO)
anddensity
with po e.The reason for these last three scales is to have all dimensionless numbers bounded
by unity.
Thus we have nine parameters
and in the context here
according
toBuckingham’s pi-theorem
we are allowed to havefive independent pi-monomials.
Introducedalready
are il, s and e.Two more are
straightforwardly
obtained.They
areFor later convenience one also defines
In terms of these parameters and the dimensionless fields the
hydrodynamic
eq.(2 . 4)
to(2 . 6)
now becomeNow Malkus uses e
and il
as the twoperturbative
parameters. Thus up to the first non trivialapproxi-
mation one gets
These are indeed the
Boussinesq equations (see
ref.
[3] Chap. 2).
Now a few comments are
pertinent
here to diffe-rentiate Malkus’s
approach
from that ofMihaljan.
Firstly
we notice that for standard fluids sayair,
both parameters q and a are of
nearly
the same orderof
magnitude.
Thisfact, together
with the fact that allprimed quantities
are boundedby unity, justifies
consideration of
higher
order corrections. Inthis,
Malkus’s choice is fortunate.
Secondly
from Malkus’s scheme we get adeeper analysis
of theBoussinesq approximation,
restrictedhowever to dilute ideal gases
only.
We see thatdrop- ping higher
order terms we getequations
for theperturbations
to the a.h.f. alone. The solutions of these newequations
added to the reference a.h.f.correspond
to solutions of theBoussinesq approxi-
mation. This
is just
the scheme that we havegeneralized
in section 6 below.
However we may note that the field defined
by
eq.
(4. 3)
and(4. 4)
above is not the bestpicture
for.thephysical description
of a thin gaslayer
at rest underthe adverse thermal constraint.
Shortly
we will intro-duce a different and more suitable a.h.f.
Yet,
however different the two a.h.f. may be both will lead to same first non trivialapproximations.
From the discussion that follows will also emerge thejustification
ofselecting
anarbitrary, perhaps unphysical,
a.h.f. togenerate these same
equations together
with relevanthigher
order corrections in a self-consistent scheme.To fix ideas let us think in terms of a helium gas
layer.
This is indeed taken as an ideal gas under normal conditions. We introduce the mostgeneral
a.h.f.
through
eq.(3.1) (3.2)
and(4. 1)
and letFor a
hard-sphere
gas a = 0.5. From eq.(3. 1)
and(3.2)
we getNotice that
(20132013)
0. We shall dénote Noticedz o
0 O. We shall dénoteNow solutions
(4.24)
and(4.25)
areincompatible
with the system
(4.3) (4.4)
and(4.5).
On the otherhand
comparing
solutions(4.5)
and(4.6)
with solu-tions
(4.24)
and(4.25)
shows that their second order terms are différent. Thus in the first orderapproxi-
mation the
perturbative
schemegenerated
from(4.24)
(4) Using Malkus’s parameters applied to the field (4.24) and (4.25) one gets at the first order approximationwhere a new monomial has been used ( =- gM/R Uo.
and
(4.25)
with(2.4)
to(2.6)
will be different from the similarapproximation
that arises from(4.20) (4.21)
and
(4.22) (4).
Let us prove thatthey
do in fact corres-pond
to the same order ofapproximation.
Let us start
by defining
two different a.h.f. denotedby subscripts i
=1,2 ; Tai, Pai
and Paie Let T, P and pnow be
quantities satisfying
thegeneral hydrodynamic
eq.
(2.4)
to(2.6).
For sake ofsimplicity
we shallconcentrate our discussion on the temperature field
only.
Let tildedquantities
beperturbations
upon the a.h.f. of reference. We have thefollowing
identitiesHere
To
is somearbitrary
reference temperature held fixed. Let us nowexpand Tl
and12
in two parameters q and e,assuming
both to be of same order ofmagnitude.
We get
Thus up to the first non trivial order of
approximation
one has :
together
withThus both
(4.32)
and(4.33)
differ in first order termsin il
or eonly.
In order to get theBoussinesq approxi-
mation one
neglects higher
order terms therefore oneconcludes that no matter what a.h.f. is
actually used,
the first non trivial
approximation gives
the sameanswer.
5. A first and
straightforward generalization
ofMihaljan’s
scheme and its inhérent difficulties. - In this section weclarify
the roleplayed by
the apriori
restrictions
imposed by Mihaljan
upon theequations
of state and material
parameters.
Such restrictions arein fact unnecessary and even more
destroyed
theself-consistency
ofMihaljan’s
scheme even at thelevel of the
Boussinesq approximation.
In theapproach
to be
given
now some of these restrictions are natural consequences of a well definedgeneral perturbative
scheme. We will however stay as close as we can to
Mihaljan’s
line ofreasoning.
Once more the
starting equations
are thegeneral hydrodynamic equations
to be taken now in theform
(2.4) (2 . 5)
and for the heatequation
No restrictions are
imposed
upon the temperatureand/or
pressuredependence
of the material parame- ters. Reference values arePo,
the pressure at the bottom of the fluidlayer,
and some temperature valueTo, assuming
for convenience anhypothetical
isothermal
hydrostatic
field(i.h.f.) throughout
thelayer.
Then we will refer the actual fluid temperature and pressure fieldsthrough
thelayer
to this i.h.f. asThus 7T and 8 are
perturbations
upon the i.h.f. Units of scale are :We shall refer
lengths
to L and take as unit of tem-perature 0 =
T2 - Tl,
the temperature differenceacross the
layer.
Velocities are measured with V-Ko/ L,
pressure / with 7to == Po
K2IL 2
and times withL 2/xo - L/ V.
Hereagain
xo -k.1p,
co anddenote
respectively
thermaldiffusivity
and kinematicviscosity.
Thus we have ten parameters
Buckingham’s pi-theorem predicts
then six inde-pendent pi-monomials
andfour
basicquantities.
We take
As in other occasions above R is
Rayleigh
dimension-less temperature difference.
Again denoting
the dimen-sionless fields with
primed quantities
thegeneral
hydrodynamic equations
become :where
To fix ideas relevant values of the parameters are
given in table 1 :
TABLE I
Water
layer
under standard adverse thermalgradient.
When
unspecified
the valuesof
parameters aregiven
in C.G.S. units.
Notice that E1, 82 « 1 and now e1 ~ e2, in contrast to the situation discussed earlier in this paper. The Jacobian of the transformation
{ L, 0 1 --+ { F-1, 92 }
is not
vanishing.
We thus choose el and 82 as pertur- bativeparameters
for theexpansion.
Notice also that derivatives ofp’
are of first order in both el and 82.Again
asdeveloped
before we obtain at the first nontrivial
approximation (viz. e? 8% terms)
theBoussinesq-
like
equations,
that we shall not write anymore(see
section 2
above).
A few
important
remarks arepertinent. Firstly
theterm
containing
the bulkviscosity
does not show up at the level of the firstapproximation.
Thus there isno need of any a
priori
elimination of this parameter.This
implies
that the apriori assumption
ofquasi- incompressibility
is not needed.Secondly
the scheme is validirrespectively
ofwhether the fluid be a
liquid (incompressible)
or a gas(ideal
ornot).
Inthe
limit of a dilute ideal gas oneindeed recovers Malkus’s results
given
in section 4above.
Thirdly,
as theequations
obtained here are similar to thosegiven
in section 2 above we still have found theBoussinesq-like approximation
but notstrictly
the
Boussinesq equations (see
ref.[3]
or[8]).
Thematerial parameters must
arbitrarily
be set constant.Thus we need a condition
ranging
outside the pro-posed perturbative
framework. Eventhough
ourapproach
doesgeneralize Mihaljan’s perturbative
scheme and overcomes one of the inherent difficulties that arises from the choice of the
expansion
parameterswe still have difficulties in
properly accounting
forthe
Boussinesq approximation.
For this very reasonwe tum our attention to a
generalization
of the a.h.f.concept
introduced in earlier sections.6. An
appropriate a.h.£,
theBoussinesq approxi-
mation and a
general perturbative analysis.
- Let{ Ta, Pa, p. 1
define a suitable a.h.f.satisfying
thedifferential system
Here it is assumed that at z = 0 one has
Ta
=To, à
=Po,
Pa = Po. Thesubscript
on theremaining quantities
denote reference values taken at theTo, Po thermodynamic
state. ,Solutions of
(6 .1 )
to(6.3)
arewhere p
denotes anunspecified
but constant adversethermal
gradient.
The easiestspecification
will be tochoose p corresponding
to theRayleigh
number forthe onset of convective
instability.
But this need notnecessarily
be so.Let us now define the
following
dimensionless monomialsThus eq.
(6.4)
to(6.6)
for theprimed
fields become in dimensionless formHere as usual z’ =
zip
andNow for the
general
fluiddynamics
we write theequations
in terms ofperturbed
fields(3.3) (3.4)
upon the reference a.h.f.
Let us now define new dimensionless
quantities
where
At
denotes the différence in1
betweenhigher
and lower parts in the fluid
layer. Eq. (6.19)
alsodefines 0153. One now writes
-
and as usuai the
primed quantity
is dimensionless.Again velocity
is scaled withEq. (6.21) provides
an estimated value of thevelocity
field for a maximum
buoyancy
effect taken at the upperboundary.
Pressure is scaled withAn estimate of
p
can also begiven.
LetAP
denotedensity
contrast betweenhigher
and lower parts in the fluidlayer.
ThenAp/po
is of order r¡ 1. ThusNow
A
Taylor
seriesexpansion gives
and
Notice that under standard conditions both
Cl
and62
are much smaller than
unity.
For instance for the waterlayer
of Table 1Ci - 10-2
andC2 - 10-5.
Thus one is led to the
following
scaleWith this unit one estimates V and po
Y2.
One hasand
As in
previous
occasionsLI V, Ko,
co, ao and xo define theremaining scaling
factors. Thus we have twelve parametersBuckingham’s pi-theorem
leaveseight pi-monomials only.
As yet we have defined{
111’ 112,C1, 62, 4>,
cv}.
We will also have u
(Prandtl number)
and R(Rayleigh number).
With the use of theseparameters
and thescaling
units one has thefollowing
set of differentialequations
In eq.
(6.17b)
and(6.18b)
we have used vo =po/po,
Ko =kolpo co, R
=gL3 el n1/Ko
vo and u =volko.
A
general
and well definedtwo-parameter expansion
is obtained in terms of Il and n2. For the waterlayer
of Table I above estimated values are
il, - Il 2 -10-3 . Again the Jacobian of the transformation (L, fi) ---> (n1,, n2)
does not vanish. Thus up to the first non trivial
approximation
one has in dimensionless form :Eq. (6.28)
to(6.30)
define the correct non linearBoussinesq approximation. Compare
for instance the results ofMihaljan [6].
His eq.(4.6) corresponds
term
by
term to our eq.(6.29)
here. Each separateterm does not however
give
the samephysics
in bothpapers. There is also an obvious différence between
our eq.
(6.30)
andMihaljan’s
eq.(4.6).
The differencecomes from our
original
definition of the reference a.h.f. Thecomparison
with Chandrasekhar’s[3]
eq.
(56),
p. 19 is however almoststraightforward.
Forif one linearizes out eq.
(6. 30)
then goes back to theoriginal
fields anddrops
all pressuredependence
inthe
equation
of state, and also makes the transforma- tion from the variables here to those of Chandrasekharone gets his eq.
(56), p. 19.
It is thus clear that theonly
differences are matters of
convention, approximation,
and indeed of the
physical meaning
ascribed to theunperturbed
reference fields.The eq.
(6.28)
to(6.30)
have been obtained as afirst order
perturbation
upon the reference a.h.f.defined
by
eq.(6.4)
to(6.6).
Since the materialparameters
and theequations
of state are almostunrestricted in our
description
the results obtained in this section constitute a non trivialgeneralization
of
Mihaljan’s
results[6] although
atfirst sight
it ispurely
formal. In ouropinion
ithelps
tounderstand
the
Boussinesq-Oberbeck approximation
on adeeper
basis. Our results also
provide
a naturalgeneralization
of results
already
obtained for dilute gasesby
Malkus
[7].
It shouldfinally
be mentioned that anintuitive derivation of
Boussinesq equations, though
not a valid method to generate
higher
order correc-tions,
has beengiven by Spiegel
and Veronis[11].
Acknowledgments.
- Part of this work was done while one of the authors(M.G.V.)
wasvisiting
theInstitutt for Teoretisk
Fysikk, University
of Trond-heim-N.T.H., Norway.
Hegratefully acknowledges
the
hospitality
received there from Professor H. Wer-geland
and his group. He also wishes to acknow-ledge
thehospitality
at theSaclay
Center. Both authorsacknowledge correspondence
with Professor W. V. R. Malkus and access to hisunpublished
lecturenotes.
References
[1] BOUSSINESQ, J., Théorie analytique de la chaleur (Paris : Gau- thier-Villars) 1903, vol. 2, p. 172.
[2] OBERBECK, A., Sitzb. K. Preuss. Akad. Wiss, 1888, 383-95 and 1129-38. Translated by C. Abbe in Smithsonian Misc.
Coll. (1891).
[3] CHANDRASEKHAR, S., Hydrodynamic and Hydromagnetic Sta- bility (Clarendon Press : Oxford) 1961, chap. 2.
[4] JOSEPH, D. D., J. Fluid Mech. 47 (1971) 257.
[5] HOARD, C. Q., ROBERTSON, C. R. and ACRIVOS, A., Int. J.
Heat Mass Transfer 13 (1970) 849.
[6] MIHALJAN, J. A., Astrophys. J. 136 (1962) 1126.
[7] MALKUS, W. V. R., 1964, Course Lectures, Summer Study Program in Geophysical Fluid Dynamics, Woods Hole Oceanographic Institution (unpublished).
[8] VELARDE, M. G., in Hydrodynamics, Proceedings 1973. Les
Houches Summer School, R. Balian, editor (Gordon and Breach, N. Y.) to appear in 1975.
[9] PALM, E., J. Fluid Mech. 8 (1960) 183.
[10] SEGEL, L. A. and STUART, T. S., J. Fluid Mech. 13 (1962) 289.
[11] SPIEGEL, E. A. and VERONIS, G., Astrophys. J. 131 (1961) 142.
See also for corrections VERONIS, G., Astrophys. J. 135 (1962) 655.