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The effect of heat currents on the stability of the liquid solid interface
R. Bowley, P. Nozières
To cite this version:
R. Bowley, P. Nozières. The effect of heat currents on the stability of the liquid solid interface. Journal
de Physique I, EDP Sciences, 1992, 2 (4), pp.433-441. �10.1051/jp1:1992155�. �jpa-00246498�
Classification
Physics
Abstracts 68.45The effect of heat currents
onthe stability of the liquid solid interface
R. M.
Bowley (*)
and P. Nozi~resInstitut
Laue-Langevin,
BP156, 38042 Grenoble Cedex 9, France (Received 7 October 1991, accepted 6January
1992)AbstracL
Rapid changing
of the temperature of aliquid
inequilibrium
with its solid can lead to instabilities of the interface in two ways : thechange
in pressure, inducedby
a temperaturechange
at the interface, leads to a uniaxial stress which can cause a Grinfeldinstability
at thecapillary wavelength
a temperaturegradient
is set up which modifies the effectivegravity
at the interface. When the effectivegravity
becomesnegative,
the interface is unstable at verylong wavelengths.
For asuperfluid,
such as~He,
the situation is morecomplex.
If weignore
surfacedissipation,
there is still a small critical temperaturegradient
across the solid above which theinterface is unstable. However surface
dissipation
inparticular
thegrowth
resistancepushes
the
instability
to huge temperaturegradients,
ones which cannot be realisedexperimentally.
Theonly instability
that can be seen is causedby
uniaxial stress.Introduction.
Consider a solid in contact with its melt with the interface
perturbed
fromequilibrium
asillustrated in
figure
I. If the solid is heavier tuan theliquid,
bothgravity
and surface tensionare
stabilising
:tuey
act topush
rue interface back to theequilibrium position.
Atemperature gradient
across the interface can bedestabilising
if theliquid
issupercooled,
the solidsuperheated,
and the latent heat ispositive.
The solid would want to grow into colderliquid
uquid
(
Solid
Fig.
I. A disturbance of the interface between a solid and its melt.(*)
Present address :Depanment
ofPhysics, University
of Nottingham,Nottingham
NG7 2RD,G.B..
434 JOURNAL DE PHYSIQUE I N° 4
and so the
perturbation
would grow. Such aninstability
should bepresent
forordinary liquids.
Such a
temperature gradient
has been invoked in order toexplain
instabilities seenby
Bodensohn et al.
[I]
on the interface between solid andliquid ~He. They report
that, whenthey
cool theliquid,
itspontaneously
deforms withcorrugations
of the surface a distance of about 6 mm apart. This value is close to ruecapillary wavelength,
2 gr(y/g Ap
)~'~, wherey18
the surface stiffness and
Ap
is the difference indensity
between solid andliquid,
ps p~. This
interpretation
cannot be correct because theinstability
appears at muchlonger wavelengths
as we shall show. Ratherthey
saw the effect of the Grinfeld[2, 3] instability
caused
by
rue creation of a uniaxial strain. Such a strain arisespartly
from thechange
in theliquid
pressure at the interface : as the temperaturedrops
so the pressurechanges
so as tokeep
on themelting
curve. The strain also arises from the thermalexpansion
or contraction of the solid. Thisexplanation
of the observations of Bodensohn et al. wasrecently proposed by
Balibar, Edwards and Saam
[4].
In this paper we
analyse
theinstability
of a solid interface due to atemperature gradient,
For an
ordinary
material, the temperaturegradient
isequivalent
to achange
ingravity,
whichcan drive a standard
Rayleigh instability.
The situation iscompletely
different insuperfluid
~He.
In the absence of surfacedissipation,
the interface would be unstable if the temperaturegradient
exceeds a threshold lmK/cm. However,
the presence of surfacedissipation
increases the critical
temperature gradient by
a factor of 105 or more, so that it isimpossible
to observe the
instability
in 4Hecrystals.
A suddenchange
in temperature can lead to a uniaxial stain sufficient totrigger
the Grinfeldinstability;
we estimate the size of thetemperature change
which is needed.1.
Dynamics
of a solidliquid
interface in the absence of surfacedissipation.
Assume that a d-c- heat current
Jo
flowsthrough
thesteady
interface,implying
zeroth ordertemperature gradients Gs=-Jo/Ks, G~=-Jo/K~ (Ks
and K~ are the d-c- thermal conductivities in eachphase).
The interface isdisplaced by
an amount( =
e'~
e~'(1)
The
change
inliquid
pressure at the interface contains anhydrostatic part
p~gi (due
toexploration
of the zeroth orderprofile),
and an extra modulationAP~
which drives the flowthrough
theliquid.
If s«ck(c
= soundvelocity),
aquasistatic approximation
is valid :AP~
isharmonic,
such thatAP~
=e'~~~~~
Theequation
of motion at interface is thenk AP
L = k
(&pL
+ PLgf)
= PLIL
=(Ps PL)
f(2)
v~ is the normal
liquid velocity
atinterface,
ps and p~ arespecific
masses.(In writing (2),
weuse conservation of
matter). Similarly,
temperatures at the interfacechange by
amounts3T~
and3Ts
on each side. Each of them contains a termG(
due toexploration
of thezeroth order
gradient,
and an extra modulation that drives the heat currentthrough liquid
and solid. These heat currents, measured from solid toliquid,
may thus be written aszLJQL= 3TL-GLf -zsJos
=3Ts-Gsf (3)
where
Z~
andZs
areappropriate
a.c, thermalimpedances
for eachphase. J~~
andJ~s
in tum must ensure energy conservationJ~~ J~s
=
£ps
((4)
where £ is the latent heat per unit mass.
We now assume that there is no surface
dissipation.
Then3Ts
=3T~
= 3T
(no Kapitza resistance).
In the absence ofcapillarity, 3p~
and 3T must remain on thephase equilibrium
curve,
3p~
=
~~~
3T
=
~~~
~~3T.
(5)
dT
T(ps PL)
From
(3)
and(4)
we find 3T.Using (2)
and(5)
we obtain therequired dispersion
relation~ ~~ ~ ~
~~~ ~~~
k ~
Zj
+Zj
~~
PL dT K~
Z~
~KsZs
~
~~~
The
generalization
of(6)
to morecomplex
situations isstraightforward.
If we want to includecapillari~y,
we must add to(5)
the standard Gibbs correction. p~ g is thusreplaced by
p~ g +
yk2~ L~
= p~ g(k> (7>
s ~
where y is the surface energy
(as usual, gravity
is overtakenby capillarity
as kincreases).
In order to includesu~fiace dissipation,
we must allow for different temperatures at theinterface, 3T~
~3Ts,
thegrowth being
drivenby
the difference(~1~ ~ls).
This will be done in thenext section.
We rust consider a normal
liquid,
with finite thermal conductivities in bothphases.
Weassume ps ~ p~ the
liquid
is ontop
such as to ensure mechanicalstability. Jo
is orientedfrom solid to
liquid
:Jo
~ 0implies
that theliquid
issupercooled.
The thermalimpedances
arediffusive
(in
aquasistatic approximation
which holds nearthreshold)
:Z[~= K~k Zj~
=
Ksk.
The
dispersion
relation(6)
reduces to°
- PL ~ +
~Ps PL) I
Ii
+I ~
~p~~~[+ ~~~
~~1°~~
li~ (8)
When
Jo
=
0,
theRayleigh
waves aredamped
at lowfrequency by
thermaldissipation (this
limit is seldom achieved inpractice).
The effect of the d.c. heat current isjust
toreplace
gby
an
effective gravi~y
2
Jo dp~
~~~ ~
PL(Ks
+KL)
dT ~~~From now on, g is meant to be the combination g
(k )
defined in(7).
The interfaceundergoes
astandard
Rayleigh instability
if g~~~ becomesnegative,
which occurs for Jlarger
than a critical heat currentJc
= PL g
$
"~ "~(io)
(J~ depends
on the wave vector kthrough
g(k)).
Note thatJ~
ispositive
: heat must flow into thehigh
temperaturephase
in order to destabilise the interface. The situation would be436 JOURNAL DE PHYSIQUE I N° 4
reversed for water : the solid is then on top of the
liquid,
andJ~
isnegative
onceagain,
heat flows into asupercooled liquid.
The result
(8)
for « normal »liquids
isfairly
obvious. It is notquite
so forsuperfluid
~He.
In that case, the d.c.conductivity
K~ is infinite(I.e. G~
=
0)
the thermalgradient
existsonly
on the solid side. The a.c. thermalimpedance Z~
is monitoredby
thermal inertia ofsecond
sound,
zji
=
c~ Ml
~(ii)
s
where
C~
is thespecific
heat per unit volume of theliquid
and Mu the second soundvelocity.
Carrying (11)
into(6),
we finds2 lj dp~
2T/p~ Jo
sdp~
~ ~~ ~ ~
~~~ ~~~
k ~ dT
u( C~
+ sKsMl C~
+ sKs dT ~~~~Jo
is nolonger equivalent
to a merechange
in effectivegravity.
For small s, we canexpand equation (12)
in a power series in s. The terms in s ands~
are small.
Neglecting
them we get the dominant terms~2
PL g +
(Ps PL) j (I
+ B)
= 0(13)
where
B
=
~
~~~
~(14)
PL dT
C~ Ml
B describes the « thermal inertia » due to second sound in the
liquid,
Its behaviour as a function of T is shown infigure
2 ; it is dominant athigh temperatures,
B i
oi
~ Temp K ~
Fig.
2. The parwneter B(T) forsuperfluid
~He.Equation (13)
describes apurely oscillatory
mode with simaginary (= iso),
The termswhich have been
neglected
describe thedamping (or growth)
of the mode.Putting
s =
iso
+ 3s we get, aftersimple algebra,
3s
=
) ~~
~~~(15)
Mu
C~
where
Jc=PLg(k>~$ «s~~
~
(16)
is the critical heat current. For
Jo larger
thanJ~
the mode is unstable and it growsexponentially
since the real part of s ispositive. Equation (15)
is very similar to theexpression (10)
obtained for a normalliquid
with no second sound ; the main difference comes from the factorB/(I
+B).
But the nature of theinstability
is different : it occurs at finitefrequency
so instead of zero
frequency.
The
instability
appears first when g(k)
isminimal,
I-e- at k= 0. We can
readily
calculate the criticaltemperature gradient using
the data ofGrilly [5]
taken on themelting
curve, andusing
estimates of second sound velocities and otherquantities
from the tables of Brooks andDonnelly [6].
The result is shown infigure
3. Below 0.78 K the latent heat isnegative
so that the criticaltemperature gradient
isnegative
also. Thelargest magnitude
for thetemperature gradient
is 0.93mK/cm. Changing
the temperature of theliquid by
a few mK could have adestabilising
effect if this were acomplete description
of the system. But we haveignored
surface
dissipation
: we haveignored
both the resistance togrowth
at the interface which leads to a difference in chemicalpotentials
across theinterface,
and we haveneglected
theKapitza
resistance whichgives
rise to adiscontinuity
in thetemperature
across the interface.At first
sight
thisneglect
appears to be correct for surfacedissipation
leads to termsproportional
to s in thedispersion
relation. For normal fluids thesedissipative
processes do not influence the threshold ofinstability, only
the rate at which theinstability develops.
But forsuperfluid
systems, s ismainly imaginary.
Theinstability
due to heat currents comes froma
competition
between terms in s and ins~
in thedispersion
relation.Consequently
any term which is of order s canstrongly
affect thestability
of the interface.~
E- w a
t
° Temp K ~
Fig.
3. -The critical temperaturegradient
for solid ~He if there were no surfacedissipation.
2. The effect of surface
dissipation.
Let us first
neglect Kapitza
resistance. The thermal balance at interface is the same as before.But we allow for a resistance to
growth
: a finitevelocity ( requires
a chemicalpotential
bias(per
unitmass)
JIL J1s = A~ = ~
(17>
a is a
growth
coefficient.(For ~He,
it isusually
written as m~K~,
where m~ is the atom mass :K~
then has the dimension of avelocity). (17) implies
that theliquid
pressuredeparts
from thephase equilibrium
curvep~(T), by
an amountAp~=
~~~~ ~(18)
ps-p~a
438 JOURNAL DE PHYSIQUE I N° 4
The
dispersion
relation(13) acquires
an extra term~~~~j j (19)
s- ~
which is
dissipative
andstabilizing.
Such a contribution should becompared
to the otherdissipative
terms in(6).
For normal
materials,
thedispersion
relation reduces to(8). (19)
competes with the bulkdissipation
due to Ks and K~. The ratio of surface to volumedissipation
isequal
tok/k*,
wherek*
=
~~~ ~~~
T
~~~
~"
(20)
p~ p~ dT Ks + K~
Under
typical conditions,
k* is of atomic scale Ilk * if of order thephonon
mean freepath
in eitherphase).
On amacroscopic
scale, surfacedissipation
iscompletely negligible
ascompared
to bulkdissipation.
The situation is
opposite
forsuperfluid ~He.
Then(19)
should becompared
with the termJ~
Sdp~
u( C~
dTin
(12).
The ratio of surface to volumedissipation
isldT $ j2 (Ps -PL) B~
«sPs
~~~ l +B T " ~~~~
where B is defined in
(14). Using
values of agiven by
Bodensohn et al.ill,
we find this ratio muchlarger
than I at«high»
temperatures(above 0.8K)
: it is about105
at0.8K,
6 x 10? at 1.2 K and 4 x 109 at 1.6 K. The critical heat current and temperaturegradient
areaccordingly pushed
upby
a factor~10~,
up to 10K/cm,
a number
beyond
reach of anyexperiment.
We conclude that surfacedissipation
is herelargely
dominant : itprecludes
anysurface
instability
drivenby Jo.
As the temperature goes down, the
Kapitza
resistance becomessignificant
: one mustrely
on
coupled equations
for the mass flowthrough
the interface 3= p s (, and the energy flow
3~.
These areconveniently
written as[3]
3
= ps a
(A~I+
A ~~~(22)
AT=
R
~i~
Alin which
3~
=
3~ Ml
is the heat current, AR, AT are discontinuities across the interface, R is theKapitza
resistance and A is a cross coefficient thatspecifies
how entropy is sharedbetween solid and
liquid.
For agiven
pressure3p~
the interface temperature3T~
and3Ts
should be calculatedaccording
to these newboundary
conditions[3].
The result isequivalent
to a shin of a, which becomesj i
psRZ~(TS~-A)~+RZS(TSS-A)~+Z~ZS£~
j~
a
~ T
R+Z~+Zs
~~~~In the absence of surface
dissipation (R
=
0,
a= co
),
i ps
Z~ZS£~
~
T(Z~+Zs)
which is
just
the bulkdissipation
embodied in the first term in the bracket of(6).
Thegenuine
surfacedissipation
involves the excess toHo,
I.e. an effective a~~r.I I Ps R
[Z~(TS~ )
+Zs(TSS
A)]~
(
«~
T(R
+Z~
+Z~) Z~
+Zs
~~~~The thermal corrections to
(24)
becomeimportant
below 0.6K. Butthey
are somewhatuncertain as the values of R and A are not obvious. One
possible
choice is that of Andreev andKnizhnik
[7],
who assume an interfacecompletely impenetrable
tophonons
I.e.a = R
= co, A = 0. In the
long wavelength capillary limit,
s=
k~~i
k ~0,
it seems morereasonable to assume
Z~«R«Zs
in which case
= +
~ (TSS
A )~(25)
"eff " T
In any event, thermal corrections can
only
enhance surfacedissipation
: anyinstability
ispushed
up to verylarge
heat currents, well out of reach ofexperiment.
3. The effect of a Grinfeld
instability.
It was shown
by
Grinfeld[2, 3]
that a nonhydrostatic
stress near the interface could drive amelting instability
amelting freezing
waverelinquishing
some of the bulk elastic energy.Assuming
a one dimensional geometry in which the strainu~
=0,
theinstability
is monitoredby
the difference «~ «~~. It can be described as an additional term ing(k),
which becomesg(k>
= g +
Yk~
2~k
~~ ~~ ~~
~~~ (26)
~
=
(tr~ tr~~)~
~'E
(E
isYoung's modulus,
« is Poisson'sratio).
Whilegravity
andcapillarity
arestabilising,
the elastic term leads to aninstability
if g~~~w 0.In the absence of a heat current, the
instability
appears at thecapillary
wave vector k~ =~~~ ~~~
~ ~~~(27)
Y
when
p
exceed a thresholdPl= lgY(Ps-PL>i~~~ (28>
When
p
exceedsp),
one faces the usualwavelength
selectionproblem.
440 JOURNAL DE PHYSIQUE I N° 4
Assume now that a d-c- heat current
Jo
isapplied
to a normal material(with
finite«~,
«s).
g isreplaced by
Jo
g 1--
c~
where
J~
isgiven by (10).
The thermal and elastic instabilities compete : thecorresponding phase diagram
is shown infigure
4. Note that the wave vector at thresholdchanges
asJo
increases,k~ =
~~~ ~~~
~l
~~~
=
~~
(29)
Y
c Y
i~/1]
Fig. 4. The
stability diagram
for a normalliquid
as a function of heat current and uniaxial strain, denotedby
the parameter pgiven by equation
(26).As
Jo increases,
theinstability
moves tolarge wavelength. Conversely,
one couldapply
a heatcurrent in the reverse direction and cause a decrease in critical
wavelength, enabling
morewaves to appear across a
sample.
Such a
simple picture
nolonger
holds for~He,
sinceJo only
acts ondamping
of the wave.The Grinfeld
instability
is not affectedby
a d.c. heat flow ; italways
appears at thecapillary wavelength (27).
We now examine how these conclusions
apply
to theexperiments
of Bodensohn et al.[I].
They applied
a sudden decrease in temperature to theliquid, thereby setting
up a heatflow,
but also a nonhydrostatic
stress in the solid. The difference(«~ «~~)
arisespartly
from thermalexpansion
in the x and y directions(in
a vessel which we assume free ofexpansion), partly
from thechange
inliquid
pressure p~ needed in order to remain on thephase
equilibrium
curve. Mechanicalequilibrium implies
3«~~ = 3p~,leading
to a nonhydrostatic
stress if we
impose
the constraint3u~
=3u~
= 0. Moreprecisely,
we may writeEa s dT + « da
d«~
~~=
where a~ is the thermal
expansion
coefficient. We thus find~~~~~ ~~>
E« s dT
~i j
2«> dPL
-
(j~2j) dp~(i
gi(30)
Here we have introduced the dimensionless parameter gj =
Eas(dT/dp~)/(1-
2«)
whichexpresses the relative
importance
of thermalexpansion.
Fortypical
materials gj is small, butg
Temp K ~
Fig.
5. The variation of gj with temperature.for helium it is of order
unity
fortemperatures
about I K. The variation of gj withtemperature
is shown infigure
5. Here we have used the estimatesgiven by
Balibar et al.[4]
of E
=
3.05 x 10~
ergs/cm~
and «= 0.33.
The threshold for the Grinfeld
instability
is therefore a pressurechange, dp~, given by
Balibar et al.
[4]
:~
E(I ~r) (Ps PL)
gY~~~ ~31)
"
(l
+~r)(1-
2tr>~ (l gi)~
~ i
E
~
~ 01 ',
6. - he
We
can the pressure change either or through asmall
temperature, AT. Provided we work
away
fromthe
region
where
gj =I
wesmall. In this way we find the
variation
in
AT hownin 6. Above I. I K it
generate theGrinfeld
instability by changing the temperature.
References
ill
[2] GRINFELD M. A.,
Dokl. Akad. Nauk.
SSSR 290 (1986) 1358 [Sov. Phys. Dokl. 31 (1986) also University of innesota preprint IMA 819 (1991).
[3]
Noz#REs
P., Shapeand
growth of crystals,niversity Press,
1991).
[4]
BALIBAR S.,[5] GRJLLY E. R., J. Low Temp. Phys. ll
(1973) 33.
[6] BROOKS J. S. and
DONNELLY R. J., J. Phys. Chem.
DAMS E. D.,
Phys. Rev. Lett. 17 1966)290.
[7] A.