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Critical Sound Damping: When Does Scaling Hold?
L. Benguigui, D. Collin, P. Martinoty
To cite this version:
L. Benguigui, D. Collin, P. Martinoty. Critical Sound Damping: When Does Scaling Hold?. Journal de Physique I, EDP Sciences, 1996, 6 (11), pp.1469-1476. �10.1051/jp1:1996158�. �jpa-00247259�
Critical Sound Damping: When Does Scaling Holà?
L. Benguigui (*), D. Collin and P. Martinoty (**)
Laboratoire d'Ultrasons et de Dynamique des Fluides Complexes (***), Université Louis Pasteur, 4 rue Blaise Pascal, 67070 Strasbourg Cedex, France
(Received 29 December 1995, received in final form 2 July1996, accepted 26 July1996)
PACS.64.60.Ht Dynamic critical phenomena PACS.64.70.Md Transitions in liquid crystals
PACS.43.35.+d Ultrasonics, quantum acoustics, and physical effects of sound
Abstract. Using the dynamic specific-heat theory, we show that exponent y, associated
with high-frequency damping at a second order phase transition (ôa ~J w~+Y), is frequency- dependent. This result indicates that the dynamic scaling-laws predicting that the ôa/à&o~
ratio is a homogeneous function of variable wT are never rigorously verified (7 is trie critical relaxation time). This calculation, which allows trie degree of departure from these laws to be
determined, is applied to various experimental situations.
Résumé. Nous montrons, en utilisant la théorie de chaleur spécifique dynamique, que l'expo-
sant y caractérisant l'atténuation haute-fréquence à une transition de phase du 2~~~ ordre
(à&o~ ~J w~+Y) dépend de la fréquence. Ce résultat indique que les lois d'échelle dynamiques
qui prévoient que le rapport ôa/ôao~ est une fonction homogène de la variable w7, ne sont en
toute rigueur jamais vérifiées (7 est le temps de relaxation critique). Ce calcul, qui permet de
déterminer l'importance des écarts à ces lois, est appliqué à différentes situations expérimentales.
Introduction
Ultrasound damping and velocity measurements provide important information on dynamic be- havior in the vicinity of a phase transition iii. The anomalies observed in the high-temperature phase are most often the result of a quadratic coupling between the ultrasound wave and order- parameter fluctuations. In this case, theones [2-5] based on the fluctuation-dissipation theorem
for the stress tensor predict that high-frequency cntical darnping is given by
à£im
+~ ~d~~~ Il)
High-frequency damping corresponds to the ~o7 » regime, where 7 is the critical relaxation time and ~o the angular measunng frequency. This regime occurs in the vicinity of transition temperature Tc because of the critical increase of 7. The exponent y = 0 for the transition
(*) Permanent address: Solid State Institute and Physics Department, Technion-Israel Institute of
Technology, Haifa 32000, Israel (**) Author for correspondence (***)URA 851 CNRS
@ Les Éditions de Physique 1996
1470 JOURNAL DE PHYSIQUE I N°11
in helium and y
= -o/zu for transitions characterized by a divergence of the specific-heat. a
is the specific-heat exponent and zu the dynamic exponent associated witu 7.
Analysis of tue ~o7 » 1 regime tuus enables tue scaling law given by Il) to be tested,
and gives us tue value of exponent y. Tuese tueories also predict tuat tue critical damping
associated witu tue uigu-temperature phase may be represented by tue scaling law ôa
i = ~i~°~~ 12)
wuere F(~OT) is a uomogeneous function of tue reduced variable ~OT. Equation (2) shows tuat
ail tue measurements must fit onto a single curve, wuicu determines tue form of tue scaling
function F(~OT).
Tuese cntical damping beuaviors would appear to be verified in a great number of cases:
tue liquid-gas critical point [6], binary mixtures ii, 8], and structural transitions [9,loi. On tue otuer uand, departures from scaling laws il) and (2) were observed in tue case of tue
transition in uelium il1,12]. Tuey can be identified by tue following features:
. exponent y > 0, wuereas it suould be zero;
. y bas diiferent values, according to wuetuer damping measurements are taken at uigu or low
frequency;
. ratio ôô/à£ice does not scale as a function of tue reduced frequency ~OT.
Tuese diiferences bave been explained by Ferrell and Buattacuarjee [12], wuo used a dynamic specific-ueat tueory to show tuat scalings il) and (2) are only respected wuen tue specific-ueat anomaly ôcp is low witu respect to tue regular part Cr~g. Tue problem of critical dynamics
bas also been addressed by Gurovicu et ai. [13], wuo bave suown tuat ultrasound damping does not, in general, exuibit scaling beuavior.
In tuis article, we propose a calculation of tue exponent y wuicu shows tuat scaling laws il
and (2) are never ngorously verified. Tuis calculation bas tue advantage of providing a simple
cnterion for determining tue conditions for wuicu departure from tuese laws is important (no scaling), or too sligut to be expenmentally observed (apparent scaling). Tue calculation will be applied in particular to tue Nematic-Smectic-A transition, for wuicu tue ratio ôcp/Cr~g varies
greatly from one compound to tue next, and will enable a certain number of predictions to be made conceming ultrasound beuavior at tuis transition.
Tue article is divided into two parts. Firstly, we calculate exponent y, and tuen tue result of tuis calculation is applied to various situations:
a) tue transition m uelium
b) transitions based on tue Ising mortel
c) tue N-SmA transition.
1. Calculation of Exponent y
Ferrell and Buattacuarjee [12] presented a very elegant metuod of calculating sound absorption
at tue superfluid transition in liquid uelium, usmg tue dynamic specific-ueat approacu. Tue starting-point is tue relationsuip between sauna velocity U and specific ueat Cp [14]
1 g
@ = K z 13)
wuere g and K are functions of serve tuermodynamic quantities wuicu are supposed to be
weakly dependent on temperature and volume. Cp can be written as tue sum of two terms:
Cp = Cr~~ + ôcp Ii)
In (4), ôcp is the critical part of the specific ueat, whereas Cr~g is tue regular part. Cr~g con
be taken as a constant because only temperatures near Tc are considered. For ôcp we use the renormalisation-group expression ils]
ôcp = cc + At~" là)
in which t is the reduced temperature (t
= (T Tc)/Tc), and Cc a constant. It is important
to note that A > 0 if a > 0 (divergence behavior) and A < 0 if o < 0 (cusp behavior).
Expression (4) can be written as
Cp = Go + At~" (6)
where Go is a positive constant equal to Cc + Cr~g.
Equation (3) shows that the velocity Uc at Tc is given by:
j
= K for a divergence Ii)
~
and ~
= K ~
for a cusp. (8)
U~ Go
Since U is not too diiferent from Uc, it is possible to rewrite equation (3) in ternis of the
expenmentally measured quantity )
1 c
~ Go +~At-" ~°~ ~ ~~~~~~~~~~ ~~~
Î~ j
Go +~At-" o ~°~ ~ ~~~~ ~~~~
In order to calculate ôoe, it is necessary:
1) to write Cp as a function of the critical relaxation frequency r
= rot~~
r -n/zv
Cp = Go + A (-) Ill)
~o
2) to use the dynamic scaling hypothesis, which consists in replacing r by -i~o when ~o > r _j~ -OE/zv
c = c~ + A (12)
~ ro
Specific heat is now a complex quantity. Velocity, related to Cp by equations (9, 10), is also a
complex quantity, and its imaginary part is related to the damping ~°",
which is wntten as
~o
~
-OE/ZV
~ ~
~°"
+~
~ ~o
~~~ 2 zu
~ cj ~ ~~~~ 1°
"~~~
~
qr a ~ ~J
~2"/zv (13)
~~ ~~ ~ ~~
~ ~ ~0
1472 JOURNAL DE PHYSIQUE I N°11
This form is valid whatever tue specific ueat beuavior (cusp or divergence). Since A and a are
always of tue saine sign, tue product A (sin gra/2zu) is positive. If a is small, cos(gra/2zu)
r~ 1
and equation (13) becomes:
~
~"/zv
ôdoe (ro~
Ù ~
~
-o/zv ~ ~~~~
~~ ~ ~ ~0~
It is possible to define an effective exponent y, as follows:
d
(ôdoe)
Y" ) à/j
(là)
àJ àJ
Equation (là) gives:
~
-n/zv
Go A (-)
~ ~ ~~
-OE/ZV ~~~~
Go + A ~o~°
Expression (16) can be mfde more convenient by separating tue cases wuere a > 0 and o < 0.
Taking B
= (A(/Co, we obtain for a > 0:
n/zv
1 B (Î)
~
~ ~~
n/zv ~~~~
~~
l + B (Î)
~o and for a < o:
-n/zv
+ B ~°
~ Î
-"/zv ~~~~
l B -)
ro
Formulae (17, 18) show tuat tue dynamic scahng laws Il) and (2) cannot be rigorously verified,
smce tue exponent y is frequency-dependent. Tuey also show tuat it is possible for systems belonging to tue same universality dass not to show tue same y values, smce tuis exponent depends, via terni B, on tue regular part of tue specific ueat, wuicu is a non-universal quantity.
Formula (17), corresponding to tue a > 0 case, shows tuat y varies from -a/zu for B
= 0
to +a/zu for B - cc, and cancels out for B
= (~o/ro)"/~~. Tuis beuavior is illustrated by Figure 1, obtained for a
= o-II (tue Ising mortel) and zu
= 2. Tue values of uJTo correspond
to tue uigu-frequency (~oTo "10~~) and low-frequency (~oTo
= 10~~) regimes.
Formula (18), corresponding to tue o < 0 case, shows tuat y presents a discontinuity wuen B = (~o/ro)"/~~ Tuis beuavior cornes from formula (13), wuicu shows tliat à£ice/~o tends towards infinity for tuis particular value of B. Tuis beuavior of ôôoe /uJ is not puysical, because it would correspond to a vanisuing specific ueat, and tuerefore tue discontinuity of y bas no
0.04
j GJTO=10~~
a =0.Il
0.00 ~
~ GJTO"10~~
-o.oz
-0.04
-0.06
0.00 0.20 0.40 0.60 0.80 1.00 1.Zo
B
Fig. 1. Variation of exponent y as a function of B for o
= 0. ii (Ising model) and zv
= 2. y presents different values depending on whether dampmg measurements are taken in the high (w% " 10~~) or
low (w% " 10~~) frequency regime (see text for details).
significance. It suould also be noted tuat tue v>lue of B cannot exceed a limit which can be deduced from tue ratio
~jj~ jOE/~i
~ ~
i
Cc
tue tueoretical value of wuicu is -1.057 [16]. Dl represents tue first scaling correction and Ai tue associated exponent. Witu Di
" o.241 iii], a = -7 x lo~3 and Ai " o-à, we obtain
(Dl("/~i = 1.02. Since Go " Cc + Cr~g, it is deduced tuat B < (R(/(Di("/~i
= 1.03.
Tue beuavior of y wuen B is less tuan 1 is given in Figure 2 in wuicu a
= -o.oo7 as in tue 3DXY mortel. Tuis figure shows tuat exponent y is very small (o.02) and virtually independent
of frequency for values of B ranging from o to o-G- For tuese values, tue scaling laws given by Il and (2) are more or less respected, and tue beuavior observed uere coula be referred to as
quasi-scaling.
Tue results tuus obtained will now be applied to various systems.
2. Comparison with Experimental Results
2.1. THE TRANSITION IN HELIUM. Exponent y was rneasured over a wide set offre-
quencies ranging from lo~ to lo~ Hz iii,18,19]. Tue results obtained show tuat y ~J o-là for frequencies below 35 MHz and
~J
o.33 for frequencies over 40 MHz [20]. Tue fact tuat
y is tuus frequency-dependent dearly shows tuat scaling dqes not apply in tuis case. Ferrell and Buattacuarjee [12] bave used tue dynamic specific-ueat approacu to explain tuis beuavior of y, assuming tuat tue specific ueat diverges logantumically. In wuat follows, we suait use
formula (18), m wuicu a
= -o.oo7 (3DXY mortel) to determine y, and show tuat variation of y witu frequency is in good agreement witu tue experimental results, tuereby validating our
approacu.
Tue values of A and Go, wuicu are necessary to determine y, show tuat (A(/Co ~ l [21], and comparison witu Figure 2 indicates tuat y is a function of ~o. Tue exact calculation using
formula (18), and the value of ro (ro
~
3 x la+~~ Hz) [18] grues y = o-là for f = lo~ Hz, and
y = o.32 for f
=
lo~ Hz, which is m good agreement with the experiments.
1474 JOURNAL DE PHYSIQUE I N°11
°'~°
a =-0.007
0.30
GJTO"ÎÙ ~
~ ~
Ù.2Ù
o.io
~GJT
~ ~~.50 0.60 0.70
0.80 0.90 1.00
B
Fig. 2. Same
as for Figure 1 but for o
= -7 x 10~~ (3DXY model) and zv
= 1.
2.2. ISING-LIKE TRANSITIONS. We shall consider 2 systerns (binary mixtures and normal- incommensurable transition) for which the specific-heat exponent is of the Ising type la o-il). =
Ultrasound damping in the 3-methylpentane-nitroetuane mixture was measured by Garland and Sancuez [8] and scaling laws Il and (2) were cuecked witu an imposed value of y
= -o.06 deduced from tue formula y
= -a/zu, in wuicu a
= o.Il and zu
= 1.93.
Tue specific-ueat measurements [22] show that A = 2.96 and Go = 17.72 which gives B
=
o.16. Use of this value for calculating y from formula (là) shows that y
= -o.03 for tue ultrasound frequencies u8ed (~oTo +~
lo~3 lo~~) Tuis value of y shows tuat scaling laws Il)
and (2) suould not be applied. Tuey are apparently respected, since tue value of y Iv
= -o.03)
is not far enougu from tue imposed value Iv = -o.06).
In tue case of tue normal-incommensurable transitions in NaN02 [9] and Rb2ZnC14 [loi, an
apparent scaling was obtained witu a value of y
= -o.l, corresponding to values of o.Il and 1 for a and zu respectively. According to our calculation, tuis implies tuat B suould be very
small.
2.3. THE N-SMA TRANSITION. Like the transition
m uelium, tuis transition belongs
to tue 3DXY universality dass. Tue 3DXY feature is not always apparent, uowever, as it is sometimes very close to a tricritical point. Tuis is wuy, depending on tue compound under
study, a 18 found to vary between -o.oo7 (3DXY) and o-à (tricritical point) [23, 24].
If we consider only tuose compounds for wuicu a
r~ -7 x lo~~, ratio B
= (A(/Co is found to vary from o.99 to o.40 [17,24,25]. It is dear from Figure 2 tuat y suould be strongly dependent
on frequency wuen B is close to 1, and suould not show any marked variation witu frequency
wuen B is smaller tuan o-G- Consequently, ultrasound damping suould bave quasi-scaling
beuavior for compounds for wuicu B is less tuan o.6.
Recent experiments carried out at tue N-SmA transition m TBBA [26] show tuat scaling laws Il and (2) are venfied, witu y m tue vicinity of zero and zu of tue order of1. Tue value of y, wuicu implies tuat a
r~ o, suggests tuat tue transition is of the 3DXY type, in which
case Figure 2 shows tuat B suould be less tuan o.6. Recent prelimmary measurements of tue specific ueat show tuat tue cntical part is small in companson witu tue background [2î]. Tuis
result is consistent witu tue small expected value of B.
0.35
°.~~
a =0.424
o.15 ' ~
GJTO"10_~
o.05
~ ~o.05 '
-o.15
jG~To"io~~
-0.35
-0.45
°°°°°~ ~°°°~
B °'°~
°'~
Fig. 3. Sartre as for Figure 1 but for a = 0.424 (mixture with X
= o-à of Ref. [24]) and zv = 1.
Trie B value
is deduced from trie specific-heat data analysis of reference [24] and is represented by trie vertical dashed line (see text).
Finally, we suait examine compounds wuicu are under trie influence of a tricritical point, sucu as tue mixtures given in reference [24], wuicu are cuaracterized by an a exponent of o.3
or o.4, and very low values of B(+~ 4 x lo~3). Figure 3, corresponding to the mixture with
an o exponent of o.424, shows that, in spite of the very low value of B, y varies strongly with
frequency [28]. Tuese mixtures should not, tuerefore, have scaling behaviors Il) and (2).
Conclusion
We bave determmed tue exponent y wuicu descnbes ultrasound dampmg beuavior m tue
~OT » 1 regime. This calculation shows that y is dependent on frequency, which in tum mdicates tuat tue simple scaling laws deduced from morte-coupling calculations suould not be
applied.
In tue case of binary mixtures and structural transitions, departure from tuese laws is so
sligut tuat it cannot be observed. Nor suould it be observed in lue
case of tue N-SmA transition for compounds witu a 3DXY-type a exponent and a (A(/Co ratio smaller tuan o.6. On tue
otuer uand, tuis departure suould occur m tue case of tue N-SmA transition for compounds wuicu, like tue À transition in uelium, bave an (A(/Go ratio of tue order of1. Tuus compounds belonging to tue same universality dass may or may not bave tue simple scaling beuavior given by equations Il) and (2). A departure from tuese laws suould also occur for compounds witu
a N-SmA transition in tue vicinity of a tricritical point. It would be interesting to test tuese
predictions by taking ultrasound measurements on ail the8e various compounds.
Acknowledgments
It is a pleasure to tuank Professor H. Brand for bis critical reading of tue manuscnpt.
1476 JOURNAL DE PHYSIQUE I N°11
References
iii See for example Garland C.W., m "Puysical Acoustics", vol. VII (Academic Press, N-Y-, 1970).
[2] Kawasaki K., Phys. Reu. A1 (1970)1750; Phys. Lett. A 31(1970) 165.
[3] Kroll D.M. and Ruuland J-M-, Phys. Lett. A 80 (1980) 45; Phys. Reu. A 23 (1981) 3îl.
[4] Swift J. and Mulvaney B-J-, J. Phys. Lett. IFance 40 (1979) 28î.
[Si Andereck B-S- and Swift J., Phys. Reu. A 25 (1982) lo84.
[6] Eden D., Garland C.W. and Tuoen J., Phys. Reu. Lett. 28 (1972) 726; Roe D.B. and
Meyer H., J. Low Temp. Phys. 30 (1978) 91.
[î] Sancuez G. and Garland C.W., J. Chem. Phys. 79 (1983) 3100.
[8] Garland C.W. and Sanchez G., J. Chem. Phys. 79 (1983) 3090.
[9] Hu J., Fossum J-O-, Garland C.W. and Wallace P-W-, Phys. Reu. B 33 (1986) 6331.
[loi Hu Z.. Garland C.W. and Hirotsu S., Phys. Reu. B 42 (1990) 8305.
[Il] Tozaki K. and Ikusuima A., J. Low. Temp. Phys. 32 (1978) 379.
[12] Ferrell R-A- and Buattacuarjee J-K-, Phys. Reu. Lett. 44 (1980) 403.
[13] Gurovicu E-V-, Kats E-I- and Lebedev V.V., JETP Lett. 52 (1990) 611, ibid. Sou. Phys.
JETP 73 (1991) 473.
[14] Ferrell R-A- and Buattacuarjee J-K-, Phys. Reu. B 25 (1982) 3168.
[15] Bagnuls C. and Bervillier C., Phys. Reu. B 32 (1985) 7209.
[16] Bagnuls C. and Bervillier C., Phys. Lett. A 107 (1985) 299; A ils (1986) 84.
[17] Garland C.W., Nounesis G. and Siine K-J-, Phys. Reu. A 39 (1989) 4919.
[18] Williams D. and Rudnick I., Phys. Reu. Lett. 25 (1970) 276.
[19] Carey R., Bucual Ch. and Pobell F., Phys. Reu. B16 (19îî) 3133.
[20] Ikusuima A., Jpn J. Appi. Phys. 19 (1980) 2315.
[21] Singsaas A. and Aulers G., Phys. Reu. B 30 (1984) 5103.
[22] Sancuez G., Meicule M. and Garland C.W., Phys. Reu. A 28 (1983) 1647.
[23] Thoen J., Marynissen H. and Van Dael W., Phys. Reu. Lett. 52 (1984) 204.
[24] Nounesis G., Garland C.W. and Suasuidar R., Phys. Reu. A 43 (1991) 1849.
[25] Garland C.W., Nounesis G., Young M.J. and Birgeneau R-J-, Phys. Reu. E 47 (1993)
1918.
[26] Sonntag P., Collin D. and Martinoty P., to be publisued.
[2î] Sonntag P., Private Communication.
[28] Formula Iii) cannot apply rigorously, smce it is only valid if exponent o is in the vicinity
of zero. When tue calculation is made witu uigu values of o la
= 0.3 or 0.4), it only bas
a very sligut eifect on formula Iii), wuicu tuus remains valid in practice.