Physica C 330 Ž2000. 105–129 www.elsevier.nlrlocaterphysc
Vortex physics in confined geometries M. Cristina Marchetti ) , David R. Nelson Lyman Laboratory of Physics, HarÕard UniÕersity, Cambridge, MA 01238, USA Received 21 September 1999; received in revised form 16 November 1999; accepted 19 November 1999
Abstract Patterned irradiation of cuprate superconductors with columnar defects allows a new generation of experiments which can probe the properties of vortex liquids by forcing them to flow in confined geometries. Such experiments can be used to distinguish experimentally between continuous disorder-driven glass transitions of vortex matter, such as the vortex glass or the Bose glass transition, and non-equilibrium polymer-like glass transitions driven by interaction and entanglement. For continuous glass transitions, an analysis of such experiments that combines an inhomogeneous scaling theory with the hydrodynamic description of viscous flow of vortex liquids can be used to infer the critical behavior. After generalizing vortex hydrodynamics to incorporate currents and field gradients both longitudinal and transverse to the applied field, the critical exponents for all six vortex liquid viscosities are obtained. In particular, the shear viscosity is predicted to diverge as < T y TBG
1. Introduction In the mixed state of type-II superconductors the magnetic field is concentrated in an array of flexible flux bundles that, much like ordinary matter, can form crystalline, liquid and glassy phases w1–3x. The dynamics of the flux-line array determines the resistive properties of the material and has therefore been the focus of much theoretical and experimental work.
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Corresponding author. Physics Department, Syracuse University, Syracuse, NY 13244, USA. Tel.: q1-315-443-2581; fax: q1-315-443-9103. E-mail address:
[email protected] ŽM.C. Marchetti..
Of particular interest are the phase transitions connecting various forms of vortex matter. For example, a first order melting transition is now believed to connect the crystalline Abrikosov flux lattice to a melted flux liquid w1x. If the barriers to line crossings are sufficiently high, rapidly cooled vortex liquids can bypass the solid phase altogether and form an entangled polymer-like glass phase w4x. The transition to such a polymer glass would occur when the system gets trapped in a metastable state, much like the transition in ordinary window glass. Other types of glasses are also possible because of pinning in disordered samples. It was suggested some time ago that point disorder may drive a continuous transition from a vortex liquid to an isotropic vortex
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M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
glass state, with vanishing linear resistivity w5,6x. The existence of this transition is still in doubt, as many of the early experiments claiming to observe it w7,8x were in fact dominated by twin boundary pinning. The vortex glass remains, however, a credible candidate for the description of the disordered solid phase observed in untwinned crystals at high fields w9x. Correlated disorder, that is disorder that can pin vortex lines coherently along a specific direction, is also very important in many materials. It can be created artificially via the introduction of columnar damage tracks created by heavy ion irradiation — a procedure that was shown to result in dramatic improvement in the pinning of vortex lines w10–12x. It can also be present in the material in the form of families of parallel twin planes that pass completely through the sample w13,14x. In samples with columnar disorder there is a low-temperature ‘‘Bose glass’’ phase, in which vortices are trapped on columnar defects and the linear resistivity vanishes w15,16x. At high temperatures, the vortices delocalize in an entangled flux-line liquid. The high temperature liquid transforms into a Bose glass via a second order phase transition at T BG . Samples with single families of twin boundaries also exhibit continuous transitions to anisotropic glass phases w17–19x. The Bose glass transition is the one that is best understood and experimentally characterized. For this reason, we will use it in much of the following as our prototype of a disorder-driven continuous glass transition in vortex matter. It has been studied theoretically by viewing the vortex line trajectories as the world lines of two-dimensional quantum mechanical particles w4,15,16x. The thickness of the superconducting sample corresponds to the inverse temperature of the quantum particles. In thick samples the physics of vortex lines pinned by columnar defects becomes equivalent to the low temperature properties of two-dimensional bosons with point disorder. In the low temperature Bose glass phase the vortices behave like localized bosons. The entangled flux liquid phase is resistive and corresponds to a boson superfluid. For simplicity, we confine our attention here to fields less that the ‘‘matching field’’ Bf s n pin f 0 , with n pin the areal density of columnar pins and f 0 s "cr2 e the flux quantum. Although an exact theory of such continuous transitions from the Bose glass or from the vortex glass
Fig. 1. The two anisotropic disorder geometries discussed in the text and the corresponding diverging correlation lengths.
to the entangled flux liquid phase is not available, near the transition most physical properties can be described via a scaling theory in terms of just two undetermined critical exponents w6,15,16,20–24x. The low temperature disorder-dominated glass phase is characterized by a correlation volume whose size diverges at the transition. Anisotropic disorder, such as columnar defects or twin planes, results in an anisotropic correlation volume. The most complicated case is that of planar disorder, embodied for instance by a single family of parallel twin planes. In this case there are three correlation lengths that diverge at the continuous glass transition temperature, TG Žsee Fig. 1.. The growth of correlations in the boson order parameter 1 in the direction perpendicular to both the external field and the twin planes is described by the correlation length:
j H Ž T . ; < T y TG
Ž 1.1 .
A second diverging length, j˜H ŽT ., describes the extent of correlations in the direction perpendicular to the external field, but parallel to the plane of the twin boundaries:
j˜H Ž T . ; < T y TG
Ž 1.2 .
1 We stress that the relevant Bose glass correlations are the correlations in the boson order parameter, in a representation which is dual to that of the superconductor. We are not referring to the more traditional superconducting correlations that are relevant for instance in the context of the Ginzburg–Landau theory.
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
Finally, there is a diverging correlation length along the external field Žhere the z direction., which is aligned with the twin planes: z j I ŽT . ;j H ; < T y TG
Ž 1.3 .
with z the anisotropy exponent. For planar disorder z s 1 q n˜rn Žthis constraint follows from the finiteness of c11 at the transition..2 In materials with columnar pins aligned with the external field, the correlation volume is isotropic in the plane normal to the columns. Thus, j H s j˜H and there are two correlation lengths that diverge at the Bose glass transition transition temperature, T BG , characterizing correlations in the directions perpendicular Ž j H . and parallel Ž j I . to the linear defects. In this case the anisotropy exponent z has the value z s 2. The same results are expected to hold for a mosaic of twin boundary planes, all containing the field direction, on scales large compared to the mosaic size. Finally, for the case of point disorder controlling the transition to the vortex glass phase at T VG , the correlation volume scaling is assumed to be isotropic w6x. There is only a single diverging correlation length, j H , with z s 1, although it is hard to rule out different length scales parallel and perpendicular to the field direction. The correlation time controlling the relaxation of critical fluctuations is assumed to diverge as: z t;j H ; < T y TG
Ž 1.4 .
with z the dynamical critical exponent. The values of the critical exponents n and z of course depend on the type of disorder and differ for instance for the Bose glass and the vortex glass. For the Bose glass transition, the critical exponents have been determined via simulations to be n , 1 and z , 4.6 w22x. Scaling can then be used to relate physical quantities to these diverging correlation lengths and time. In particular, the linear resistivity r H ŽT . of the
2
By applying Josephson’s scaling to c11 one finds w24x c11 ; k B Tn20 j H j˜ H r j I Žsee also the discussion at the beginning of Section 3.. If c11 is finite at the transition, then z s1q n rn˜ follows.
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™
vortex liquid for currents applied in the ab plane is predicted to vanish as T TG from above as:
r H Ž T . ; < T y TG < n Ž zy z .
Ž 1.5 .
in bulk samples in three dimensions w6,15,16x. Although some predictions of the scaling theory have been tested experimentally, there are as yet no direct measurements of the transport coefficients usually associated with glass transitions in conventional forms of matter, such as the shear viscosity. In this paper we show that the liquid viscosities also exhibit strong divergences at a continuous disorderdriven glass transition of vortex matter. We make explicit predictions for the critical exponents controlling the divergence of the liquid viscosities and propose experiments that test our predictions. For instance, the behavior of the shear viscosity is found to be determined by the dynamical critical exponent z that controls the divergence of the relaxation time in the glass phase. A direct measurement of the shear viscosity would therefore provide a direct probe of the diverging relaxation time associated with glassy behavior w25x. A brief account of this work has been presented elsewhere w26x. As for ordinary matter, the shear rigidity of the vortex array can be probed by driving the vortices to flow in confined geometries w27,28x. The fabrication and use of such confined geometries was pioneered by Kes et al. w25,29,30x to study the shear rigidity of the two-dimensional vortex liquid near the freezing transition in thin superconducting films. More recently, patterned irradiation of cuprate superconductors with heavy ions has made it possible to create samples with controlled distributions of damage tracks that will allow for a new generation of experiments that may in fact provide a direct probe of viscous critical behavior near the Bose glass transition w31x. Specifically, by starting with a clean sample, at temperatures such that point disorder is negligible, it is possible to selectively irradiate regions of controlled geometry by covering the top of the sample with a suitable mask. Perhaps the simplest geometry that can be created is that of the channel shown in Fig. 2. This closely parallels an experimental setup proposed several years ago by us for measuring the shear viscosity of an entangled vortex liquid
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Fig. 2. A weakly irradiated channel where the flux liquid is sandwiched between two heavily irradiated Bose glass contacts. A current J applied across the channel yields flux motion along the channel. Vortex pinning at the boundaries propagates a length d into the channel, yielding a spatially inhomogeneous flow profile.
forced to flow in the channel between two parallel twin planes w27,28x. Now we propose that a similar geometry created by selective heavy ion irradiation may be used to probe the growing correlations at the Bose glass transition w26x. As shown in Fig. 2, the side regions of the samples have been heavily irradiated, and are characterized by a high matching field BfŽ2. and transition Ž2. curve TBG , while the channel is lightly irradiated with a lower matching field BfŽ1. - BfŽ2. and transiŽ1. Ž1. Ž2. tion curve TBG . When TBG - TBG - TBG , the flux array in the channel is in the liquid state, while the contacts are in the Bose glass phase. Flow in the resistive flux liquid region is impeded by the ‘‘Bose glass contacts’’ at the boundaries, as the many trapped vortices in these regions provide an essentially impenetrable barrier for the flowing vortices, due to their mutual interactions. As the temperature is lowered at constant field, so that the Bose glass Ž1. transition TBG of the liquid region is approached Ž from above Fig. 3. the Bose glass correlation length increases, forcing the pinning at the boundaries to propagate into the liquid channel and yielding a spatially inhomogeneous electric field profile which can be probed experimentally. We will show that the spatial inhomogeneity of the electric field occurs precisely on length scales given by the correlation length, providing an unambiguous prescription for extracting critical exponents from this type of transport measurements.
By controlling the disorder in the channel region, the same geometry can also be used to study the onset of rigidity in the vortex array near the vortex glass or the polymer glass transitions. In the former case the channel Žnow free of damage tracks. should contain a high concentration of point defects Žaugmented, perhaps, by proton irradiation w32x.. The polymer glass transition may take place when the channel is ‘‘clean’’, with only a low concentration of oxygen vacancies. A crucial difference between the polymer glass transition and the continuous disorder-driven glass transitions discussed above is that the former is a non-equilibrium phenomenon associated with the slowing down of the system dynamics on experimental time scales and does not exhibit universal critical behavior. For this reason, by testing for a divergent length scale, transport measurements in confined geometries may actually be used to distinguish experimentally between a continuous disorder-driven glass transition and the polymer glass transition w33x. As shown in Refs. w27,28x, the electrodynamics of vortex liquids is in general nonlocal due to interactions and entanglement, even away from phase transitions. Such nonlocalities may become very impor-
Fig. 3. A sketch of the Ž B,T . phase diagram for the flux array in Ž1. Ž . the weakly irradiated channel region. The heavy line, B BG T , denotes the continuous transition from the Bose glass to the Ž2. Ž . entangled liquid. Also shown is the location B BG T of the Bose glass transition line in the heavily irradiated contacts. When a Ž1. Ž . Ž2. Ž . field BBG T - B - B BG T is applied, the flux array in the channel is in the liquid state, while the contacts are in the Bose glass phase. By decreasing the temperature at constant field along the direction of the arrow, the Bose glass transition of the channel region is approached from above. When B, instead of H, is used for the phase diagram, the Meissner phase collapses to a line, as shown.
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
tant near a phase transition, particularly when the transition is continuous. A natural way of incorporating the nonlocality in the long wavelength description of vortex liquid dynamics is via a set of hydrodynamic equations where the effect of intervortex interactions appears as viscous forces. A complete set of hydrodynamic equations for the vortex liquid is given in Section 2. These equations incorporate driving forces from external current both parallel and transverse to the field H, as well as both compressional forces and pressure forces due to vortex segments that are not aligned with the z axis. They therefore generalize earlier hydrodynamic equations written down by us that only considered flow driven by currents in the ab plane w27,28x. The line nature of vortex matter yields to a proliferation of viscosity coefficients, much like in liquid crystals w34–37x. There are therefore six independent vortex liquid viscosities in these equations.3 The general equations are complicated and will be discussed in more detail below. The equation for the coarse-grained flow velocity zŽ r . of the vortex liquid in the channel geometry of Fig. 2 is, however, very simple, namely w27,28x: 2 yg H z q h =H zs
1
n f zˆ = J, Ž 1.6 . c 0 0 where g H is the friction coefficient that incorporates both the interaction of the vortex cores with the underlying ionic lattice and the pinning by material defects and h is the vortex liquid shear viscosity. The term on the right hand side of Eq. Ž1.6. is the Lorentz current due to an external current J applied 3
Questions about the validity of the hydrodynamic theory have been raised by the careful work of Mou et al. w35x and of Blum and Moore w36,37x. These authors calculated the viscosity coefficients using time-dependent Ginzburg–Landau theory and found some of them to be negative. Negative viscosity coefficients would yield instabilities and invalidate hydrodynamics. Both calculation apply, however, near the Hc 2 ŽT . line, while the nonlocal behavior of interest here occurs near a glass transition or possibly the melting line, well below Hc 2 ŽT ., in a region of the phase diagram where the viscosities may very well be positive, making hydrodynamics a viable approach. Simulations of the time-dependent Ginzburg–Landau equation by Wortis and Huse wR. Wortis and D.A. Huse, Phys. Rev. B 54, 12413 Ž1996.x suggest indeed that at least some of the components of the viscosity tensor which are negative near Hc 2 may change sign and become positive as the temperature is lowered.
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across the channel, with n 0 the areal density of vortices. Since the local electric field from flux motion is e Ž r . s Ž n 0 f 0 .rŽ c . zˆ = zŽ r ., Eq. Ž1.6. can be rewritten as a nonlocal version of Ohm’s law: 2 e s r H J, e y d 2 =H
Ž 1.7 .
where:
rH ŽT . s
n0 f 0
ž / c
2
1
gH ŽT .
Ž 1.8 .
is the in-plane linear resistivity in a bulk sample. The viscous length:
(
d Ž T . s h Ž T . rg H Ž T .
Ž 1.9 .
controls the importance of viscous drag. In a bulk sample and in the absence of strong inhomogeneities in the spatial distribution of disorder, the electrodynamic response is expected to be essentially local on large scales. Far from the boundaries in macroscopic samples, the viscous drag drops out from Eq. Ž1.7. and the linear vortex liquid resistivity is given by Eq. Ž1.8. and is controlled entirely by the friction coefficient, g H . In contrast, in a confined geometry viscous drag becomes dominant near a glass transition and the viscous length controls the flux liquid resistivity in this case. For continuous disorder-driven glass transitions, such as the vortex or Bose glass transitions, a dimensional analysis of the hydrodynamic equations, combined with the scaling hypothesis that the diverging correlation lengths j H and j I are the only relevant length scales in the problem, leads to the identification of the viscous length with the in-plane correlation length:
d Ž T . ; j H Ž T . ; < T y TG
Ž 1.10 .
Since the bulk resistivity vanishes at T BG according to Eq. Ž1.5., or equivalently the friction g H ŽT . diverges with the same exponent:
g H Ž T . ; < T y TBG
Ž 1.11 .
the identification of these two length scales immediately leads to the prediction that the liquid shear viscosity diverges at a continuous glass transition as: 2 hŽT . ;j H Ž T . g H Ž T . ; < T y TBG
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M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
At the Bose glass transition, where z s 2 and n , 1, the divergence of the shear viscosity is controlled by the dynamical exponent z. In contrast, there is no obvious diverging correlation length controlling the polymer glass transition proposed some time ago by one of us w4x as an alternative to the vortex glass scenario and a possible explanation for the irreversibility line observed experimentally at high fields. In this scenario a viscous vortex liquid with large barriers to line crossing, when cooled rapidly may drop out of equilibrium at a polymer glass transition temperature TPG , well before it has time to nucleate the equilibrium crystalline phase. The polymer glass is metastable and the transition is analogous to the glass transition conjectured in ordinary forms of matter. Disorder plays no role in the transition itself Žalthough it may have dramatic effects in controlling the dynamical response of the vortex array. and the vortex friction g H remains finite across the transition. The shear viscosity grows rapidly as T Tq PG and its temperature dependence might conceivably be described by the standard Vogel–Fulcher form Žsee, for instance, Ref. w38x.:
™
h Ž T . f h 0 e c rŽTyT PG . ,
Ž 1.13 .
which works very well for glass transitions in conventional forms of matter. Experiments capable of measuring both the friction coefficient g H Žwhich can be extracted from a bulk resistive measurements. and the viscous length d Žwhich can be obtained from resistive measurements in confined geometries. can therefore distinguish between a kinetic polymer glass transition and a continuous-disorder driven glass transition, as well as providing direct measurements of the critical exponents in the latter case w33x. At a continuous glass transition, both friction and viscosity will diverge with a characteristic critical exponent. At a polymer glass transition, the friction will remain finite and the viscosity is expected to exhibit the Vogel–Fulcher behavior given by Eq. Ž1.13.. As shown in Section 3, dimensional analysis of the general hydrodynamic equations yields predictions for the scaling exponents for all the six vortex liquid viscosities near a continuous glass transition. The results are summarized in the table given in Section 3 below.
We stress that the identification of the dynamical length scale d with the static correlation length j H is by no means obvious. It mirrors the corresponding result obtained in the theory of continuous melting in two dimensions, where the liquid shear viscosity scales as h ; 1rjd2 , with jd the average distance between unbound dislocations, which in turn diverges at the transition, yielding a corresponding divergence of the viscosity w39x. In this case, the precise relationship between static and dynamical properties is one of the outcomes of the theory of two-dimensional melting which occurs via successive dislocation and disclination unbinding. For the vortex or Bose glass transitions, the divergence of the correlation length is due to collective effects mediated by extrinsic quenched disorder. The assumption made here is that this growing correlations associated with disorder will also drive the divergence of dynamical properties in the liquid phase, namely the viscosities. This hypothesis has powerful implications. As shown in Ref. w26x and described in more detail in Section 4 below, by combining scaling in spatially inhomogeneous geometries with hydrodynamics we are able to obtain not just the scaling exponents for the transport coefficients, but also the full form of the scaling function for the linear resistivity of the vortex liquid in a constrained geometry. The precise form of the scaling function depends on the details of the geometry and was given in Ref. w26x for the channel and for the Corbino disk geometry ŽFig. 4. used recently by Lopez et al. w32x. Once the form of ´ the scaling function is known, a quantitative analysis of transport experiments can in principle be carried out to extract the critical exponents. The plan of the paper is as follows. In Section 2, we generalize the hydrodynamic equations of Refs. w27,28x to incorporate gradients and driving forces in both the directions parallel and transverse to the applied field. Upon neglecting the small transverse frictional forces responsible for the Hall effect, the hydrodynamic equations contain two friction coefficients and six viscosity coefficients. In Section 3, after briefly summarizing the scaling theory for the Bose glass transition in bulk, we discuss the dimensional analysis of the hydrodynamic equations and obtain the critical exponents for all the transport coefficients. In Section 4, we combine scaling in
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
==bs
4p
111
j,
c
Ž 2.2 .
where we have dropped the displacement current which is negligible at all but very high frequencies Ž v , crl ; 10 15 Hz. and j denotes the total current density, including the equilibrium response of the medium, in addition to any external current. In addition, the fields satisfy divergence equations:
Fig. 4. Top view of the Corbino disk geometry with Bose glass contacts. The magnetic field is out of the page. The vortex array is in the Bose glass state in the inner and outer densely dotted regions and in the flux liquid state in the weakly irradiated annular region. A radial driving current drives flux motion in the azimuthal direction.
spatially inhomogeneous systems with hydrodynamics to show how the full form of the scaling function can be obtained for specific geometries. The Corbino disk geometry is discussed in some detail. Finally, Section 5 generalizes both the scaling theory and the hydrodynamics to finite frequency to discuss the critical scaling of the linear response of the vortex liquid to AC drives at the Bose glass transition. Appendix A makes contact with the earlier work by Mou et al. w35x on nonlocal effects in vortex liquids. In Appendix B, we apply scaling ideas to the analysis of transport in the DC flux transformer geometry.
2. Hydrodynamics of flux-line liquids Here we generalize the hydrodynamics of flux-line liquids discussed earlier by us w27,28x to incorporate the effect of driving currents in arbitrary directions, with components both parallel and perpendicular to the external field H0 s zH ˆ 0 responsible for the onset of the vortex state. The resulting hydrodynamic equations contain the six viscosity coefficients discussed by Mou et al. w35x that control the nonlocal electrodynamic response of flux liquids. The electrodynamics of a type-II superconductor in the mixed state is described by Maxwell’s equations for the local fields bŽ r,t . and e Ž r,t .: 1 c
Et b q = = e s 0,
Ž 2.1 .
= P b s 0,
Ž 2.3 .
= P e s 4pr .
Ž 2.4 .
Both fields can be obtained from a vector potential A and a scalar potential f , according to b s = = A and e s y1rc Et A y =f . We work here with the Coulomb gauge, = P A s 0. The equations for the fields must be supplemented with a constitutive equation for the current j. In the linear ŽOhmic. regime this is simply given by a nonlocal generalization of Ohm’s law: ja Ž r . s
Hr S X
ab
Ž r ,rX . eb Ž rX . ,
Ž 2.5 .
where Greek indices a , b , . . . run over the values x, y, z and are used to denote Cartesian components in three dimensions and Sab is a nonlocal conductivity tensor. Below we will also use Latin indices i, j, . . . to denote Cartesian coordinates in the xy plane, i.e., Latin indices will only assume values x and y. Nonlocality must be incorporated when describing the mixed state of the cuprates where interactions and entanglement among the vortices can yield long-ranged correlations and large scale nonlocal electrodynamic response. It is useful for the following to rewrite Eq. Ž2.5. by separating the current in a coarse-grained contribution, J, and a rapidly fluctuating contribution, j,˜ or j s J q j,˜ with j˜s crŽ4 p .= = Ž b y H .. Eq. Ž2.5. can then be written as:
ž
Ja Ž r . y c = =
dF db
/
s a
Hr S X
ab
Ž r ,rX . eb Ž rX . , Ž 2.6 .
where y4p Ž d F .rŽ db . s b y H represents the local magnetization of the medium, with F ŽT,b . the
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
112
Helmholtz free energy of the superconductor in an external field, H. J is then the macroscopic transport current flowing in the sample. The second term on the left-hand side of Eq. Ž2.6. incorporates the static Meissner response of the material as well as the current due to local Magnus and pressure forces from the vortices. In this paper, we are interested in fluctuations in the b and e fields due to fluctuations in the vortices degrees of freedom. The relationship between the local supercurrent, js , and the vortex degrees of freedom is obtained by minimizing the Ginzburg– Landau free energy functional for fixed vortex configurations. Note that in general by using a two-fluid picture there will also be a ‘‘normal current’’ contribution to the fluctuating current, j˜s js q j n . We will not incorporate this normal part of the response here. In the London approximation, where the magnitude of the superconducting order parameter is assumed constant, and only fluctuations in its phase, u , are retained, one obtains the usual London equation:
l2 j s s y
c 4p
Ž A y f 0=u . ,
Ž 2.7 .
where l is the penetration length. For clarity, we discuss only the case of an isotropic superconductor. The equations are easily generalized to a uniaxial material. In addition to the field fluctuations described by Eq. Ž2.7., there are field fluctuations representing thermal deviations from the solution of London equation, which are neglected here. In the chosen gauge Ž = P A s 0. the longitudinal part of the supercurrent is simply determined by the phase in the usual way: = P js s
cf 0 4pl2
= 2u .
Ž 2.8 .
Vortices provide a source of vorticity for the supercurrent, as the curl of Eq. Ž2.7. gives: = = js s y
c 4pl2
Ž b y f0T . ,
Ž 2.9 .
where T is the vortex density vector: T Ž r ,t . s
1 2p
= = =u .
Ž 2.10 .
We note that the curl of =u is nonzero in the presence of vortices. By combining Eq. Ž2.9. with Eq. Ž2.2., we immediately obtain the London equation determining the field due to the vortices: b y l2 = 2 b s f 0 T .
Ž 2.11 .
To obtain the contribution to the electric field from the vortex degrees of freedom, we differentiate Eq. Ž2.7. with respect to time and use e s y1rc Et A y =f , with the result: e s y=f q
4pl2 c
2
Et j s y
f0 c
Et=u .
Ž 2.12 .
The vortex part of the electric field is then given by: e Õ y l2 = 2 e Õ s
f0 2c
eabg Qbg ,
Ž 2.13 .
where: 1 2
T
eabg Qbg Ž r ,t . s y Ž Et Ea u Ž r ,t . . .
Ž 2.14 .
The antisymmetric tensor Qbg as defined in Eq. Ž2.14. describes the vortex current. It coincides with the vortex flux tensor, as from the definition Ž2.14. it follows that the vortex density vector, T, satisfies the exact conservation law Žconservation of vorticity.: Et Ta q Eb Qa b s 0.
Ž 2.15 .
The focus of the present paper is on the flux-line liquid regime of vortex matter. In order to take advantage of the vast phenomenology developed for describing long-wavelength static and dynamical properties of dense liquids with particle-like or polymer-like degrees of freedom, we will focus our attention below on the vortex degrees of freedom, rather that on the fields b and e. When the z direction is chosen along the external field H, vortex configurations are conveniently parametrized in terms of a set of N single-valued functions rnŽ z ., which specify the position of the nth vortex line in the xy plane as it traverses the sample along the field direction. The three-dimensional position of each
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
flux line is then R nŽ z . s w rnŽ z ., z x and the vortex density vector and flux tensor are given by: N
T Ž r ,t . s
ER n
Ý ns1
Ez
d Ž r y rn Ž z ,t . . ,
Ž 2.16 .
Qa b Ž r ,t . s ea bg
We have explicitly linearized in the fluctuations as we are only interested in linearized hydrodynamic equations. Neglecting again nonlocalities on length scales ; l, Eq. Ž2.13. yields: eaÕ s
N
Ý Ž Ez R n = zn . g d Ž r y rn Ž z ,t . . , ns1
e Õz s
T s Ž t ,n . ,
Ž 2.18 .
where n is the local areal density of vortices and t describes the local tilt of vortex lines away from the z direction. Neglecting spatial inhomogeneities on scales F l, Eq. Ž2.11. gives: bz Ž r ,t . s f 0 n Ž r ,t . , b H Ž r ,t . s f 0 t Ž r ,t . .
Ž 2.19 .
Similarly, the vortex flux tensor Qab can be written as:
Qx x
Qx y
Qyx
Qy y
Qz x
Qz y
Qx z
0 Q y z s yn 0 V n0 Õx Qz z
0
n 0V 0 n0 Õy
yn 0 Õ x yn 0 Õ y , 0
0
Ž 2.20 . where z represent the flow velocity of vortices moving in the xy plane and n 0 V s Ž1r2. ´ i j Q i j is the number of vortex segments aligned with the x direction crossing an area normal to the y direction per unit area and per unit time, with: N
n 0 z Ž r ,t . s
Ý zn d Ž r y rn Ž z ,t . . ,
Ž 2.21 .
ns1 N
n 0 V Ž r ,t . s
Ý zˆ P Ž Ez rn = zn . d Ž r y rn Ž z ,t . . . ns1
Ž 2.22 .
f0 2c
ea bg Qbg ,
Ž 2.23 .
or
Ž 2.17 . with r s Ž r H , z . and znŽ z,t . s Et rn the vortex velocity. The three-dimensional vortex density vector is also often written as:
113
f0 2c
e iÕ s y
ei j Qi j s
f0 c
n0 f 0 c
ei j Q z j s y
V, n0 f 0 c
e i j Õj .
Ž 2.24 .
We are interested here in the long-wavelength properties of flux-line liquids on scales large compared to l and to the average intervortex spacing, a 0 s f 0rB0 , with B0 the equilibrium mean value of the field, ² b : s zˆ B0 . For this purpose we can abandon the description in terms of the microscopic vortex degrees of freedom R nŽ z . in terms of coarse-grained or hydrodynamic fields describing fluctuations in the conserved variables of the system and corresponding to those collective degrees of freedom whose relaxation rate vanishes in the long wavelength limit. For the vortex liquid the relevant conserved variables are the three components of the vortex density, T Ž r,t . s Ž t,n.. The coarse-grained vortex density is defined as in Eq. Ž2.16., with the d-function replaced by a smeared-out two-dimensional d-function, d BZ Ž r H ., with a finite spatial extent of the order of the inverse of the Brillouin zone boundary, k BZ s 4p n 0 ,
(
(
d BZ Ž r H . s
1 A
Ý
eyi q H P r H .
Ž 2.25 .
q HFk BZ
As discussed elsewhere, the long wavelength equilibrium properties of vortex liquids can be described in terms of a coarse-grained free energy that fully incorporates the nonlocality of the intervortex interaction. Such a free energy can be derived by explicit coarse-graining of the microscopic vortex energy w40x or can be written down phenomenologically using familiar ideas from liquid state physics. It takes the form of an expansion in the fluctuations of the hydrodynamic fields from their equilibrium val-
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
114
ues and of the corresponding gradients. Retaining only terms quadratic in the fluctuations, it is given by: 1 FL s 2 c LŽ r y rX . dn Ž r . dn Ž rX . X 2 n0 r r
HH
X
X
qc44 Ž r y r . t Ž r . P t Ž r . ,
Ž 2.26 .
where dn s n y n 0 and c L and c 44 are the nonlocal compressional and tilt elastic moduli of the flux liquid, given elsewhere w40x. The vortex density vector, T s Ž t,n., satisfies an exact conservation law, Eq. Ž2.15., or, in terms of n and t: Et n q = P n 0 z s 0, Ž 2.27 . Et t i q E j Q i j s E z n 0 Õ i ,
Ž 2.28 .
with the condition = P T s 0, or: Ez n q =H Pt s 0,
Ž 2.29 .
ensuring that flux lines do not start nor stop inside the sample. To obtain a closed set of hydrodynamic equations it is necessary to specify the constitutive equations that express the flux tensor Qab in terms of the density field and its gradients. Since the vortex dynamics is overdamped, the constitutive equation is simply obtained by requiring that the net force on each local volume of flux liquid vanishes. Its form is analogous to that of Eq. Ž2.6. and it is given by: d FL g˜mn , l r Ql r s h˜mn , a b , l r Ea Eb Ql r q Em dTn y En
d FL dTm
q
f0 c
emnl Jl .
Ž 2.30 .
The term on the left-hand side of Eq. Ž2.30. represents the frictional force per unit length on the vortex liquid, with g˜mnl r , a friction tensor. The first term on the right hand side of the equation describes viscous forces from intervortex interaction and entanglement, with h˜mn , a b , l r the viscosity tensor. The second and third terms contains Magnus and pressure forces arising from vortex density gradients and the last one is simply the Lorentz force due to an external current, J. Neglecting for simplicity transverse drag forces associated with the Hall effect, there are two independent components of the friction tensor and six viscosity coefficients. It is useful to rewrite the
constitutive equations in terms of the in-plane vortex flow velocity z and the tilt current V: 2 g H z s h =H q hz Ez2 z q h b=H Ž =H Pz .
ž
y hx Ž zE ˆ z = = H . V y n 0 =H y
n0 f 0 c
d FL dn
y Ez
zˆ = J,
d FL dt
/
Ž 2.31 .
2 g I V s h t =H q hzt Ez2 V y hx zˆEz P Ž =H =z .
ž
q n 0 zˆ P =H =
d FL dt
/
q
n0 f 0 c
Jz .
Ž 2.32 .
The constitutive Eqs. Ž2.31. and Ž2.32. are now written in terms of forces per unit volume. The coefficients g H and g I have dimension of friction per unit volume, as usual, and h , hz , h b , h t , hzt and hx have dimensions of fluid viscosities. The six viscosity coefficients appearing in Eqs. Ž2.31. and Ž2.32. are related to the six components of the nonlocal conductivity discussed by Mou et al. w35x. The precise relationship is displayed in Appendix A. Eqs. Ž2.27–2.29. and Ž2.31,2.32. provide a closed set of hydrodynamic equations to describe the response of vortex liquids to external currents and fields. These equations generalize equations written down earlier by us w27,28x and by others w34,35x. by incorporating all pressure forces, including those from vortex segments that are not parallel to the external field direction, all nonlocal viscous forces, as well as external forces due to driving currents aligned with the external field. In the next section we will show how predictions for the singular behavior of the six viscosities near a continuous phase transition from the vortex liquid to a glassy state can be obtained by simple scaling arguments.
3. Scaling theory The divergence of pinning energy barriers for vanishing driving currents underlies both the theories of the Bose glass and the vortex glass transitions, which are expected to be continuous. The properties near the transition have therefore been described by a scaling theory in terms of divergent lengths and time scales. A scaling theory for the transition from a
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
vortex liquid to an isotropic vortex glass was developed by Fisher et al. w6x and then adapted by Nelson and Vinokur w15,16x to the transition to the anisotropic Bose glass. Here we summarize this scaling theory in a unified way that applies to both transitions by keeping track of the anisotropy exponent z that has value z s 2 for the Bose glass and z s 1 for the vortex glass. Of course, the values of the other critical exponents are also different in the two cases. The ŽGibbs. free energy density g of the vortex array is a function of temperature T and external field, H s zˆ H I qH H , with g s g ŽT, H H , H I .. Here H I s H0 q d H I , where H0 is the field responsible for setting up the vortex state and the flux lines are on average aligned with the z direction. The singular part of the free energy density, g s , is assumed to obey a homogeneity relation at the transition where temperature and the external fields are rescaled by different factors,
s lyŽ dy1q z . g s Ž l 1r n t ,l lH H H ,l lI d H I . ,
Ž 3.1 .
for arbitrary length rescaling parameter, l. Here t is the reduced temperature t s < T y TG
Ž 3.2 .
dH
and therefore scales according to: b H ; lyŽ dy1q zq l H . , b I; l
yŽ dy1q z q l I .
The longitudinal and transverse components of the response function are:
d i j Ž 1 q 4px H . s
1 q 4px I s
d 2 gs d H I2
d 2 gs d HH i d HH j s
n20 f 02 c11
s di j
,
n 20 f 02 c 44
,
Ž 3.5 .
Ž 3.6 .
where x H and x I are the components of the magnetic susceptibility and c 44 and c11 the tilt and compressional elastic moduli of the vortex array. The scaling of the susceptibilities is then given by:
x H;
x I;
1 c 44 1 c11
; lyŽ dy1q zq2 l H . ,
Ž 3.7 .
; lyŽ dy1q zq2 l I . ,
Ž 3.8 .
At the vortex glass transition the response of the vortex array is rotationally invariant and both susceptibilities are expected to remain finite. This requires:
g s Ž t , H H ,d H I .
b s y4p
115
.
VG lVG H s l I s y Ž d y 1 q z . r2.
The scaling of the local fields at the vortex glass transition is then: b H ; b I;
1 Ž dy1.r2 1r2 jH jI
; t 3n r2 ,
Ž 3.10 .
where the last equality applies for d s 3. At the Bose glass transition, in contrast, the tilt modulus is expected to diverge as c 44 ; l z , while c11 remains finite. In this case, the response of the system is anisotropic, with:
lBG H s y Ž d y 1 . r2,
Ž 3.11 .
lBG I s y Ž d y 1 q z . r2,
Ž 3.12 .
and the fields scale as: b H;
Ž 3.3 . Ž 3.4 .
Ž 3.9 .
b I;
1 Ž dy1.r2 jH jI
; t 3n ,
1 Ž dy1.r2 1r2 jH jI
; t 2n ,
Ž 3.13 .
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
116
where again the last equality in each of Eq. Ž3.13. applies for d s 3. To determine the scaling of fields and currents that control the resistive properties of the vortex array, we note that gauge invariance of the Ginzburg–Landau theory requires that the fluctuating vector potential scales according to:
the linear flux liquid resistivity vanish as the transition is approached from the liquid side, according to:
rH ŽT . s
Ž 3.14 .
The scaling of currents and fields is immediately obtained from their definitions, J s E frEA and E s y Ž1rc . E ArEt, where we denote by E the macroscopic Žspatially averaged. field from vortex motion. It is given by: 2y d y1 JH; j H jI , 1y d J I; j H ,
Ž 3.15 .
and: qz . E H ; jyŽ1 , H yz E I ; jy1 I jH .
Ž 3.16 .
A scaling ansatz for the IV characteristic can be written down based on the structure of the RG flows as w6x: yŽ1qz .
EH Ž T , J H . s l
ž
EH l
1r n
t,
l Ž dy 2q z . J H ck B T
/
,
2
ž / c
1
gH ŽT .
zq3yd . ; j I jyŽ ; < T y TBG < n Ž3qzydq z . , H Ž 3.21 .
A H ; jy1 H , A z ; jy1 I .
n0 f 0
rI ŽT . s
n0 f 0
ž / c
2
1
gI ŽT .
yŽ zq1yd . ; jy1 ; < T y T BG < n Ž1qzydq z . . I jH Ž 3.22 .
Equivalently, Eqs. Ž3.21. and Ž3.22. give the scaling exponents controlling the divergence of the longitudinal and transverse friction coefficients, g I ŽT . and g H ŽT .. Dimensional analysis of the hydrodynamic equations now allows us to extract predictions for the scaling of the six viscosity coefficients at the transition. The scaling dimension of the fluctuating density and tilt fields n and t is the same as that of the components of the local field b and therefore is obtained immediately from Eqs. Ž3.10. and Ž3.13. for the vortex and Bose glass, respectively. We scale all length and time scales in the hydrodynamic equations with the correlation lengths j H and j I , using the scaling dimensions just discussed for the various physical quantities appearing in these equations. By requiring the equations to be scale invariant near the
Ž 3.17 .
ž
E I Ž T , J I . s lyŽ zqz . E I l 1r n t ,
l dy 1 J I ck B T
/
.
Ž 3.18 .
With the choice l s tyn ; j H ŽT ., we obtain: . " E H Ž 1, J H . s jyŽ1qz EH H
yz " E I 1, J I s jy1 I j H EI
Ž
.
ž
ž
dy 2 jH j I JH
ck B T
dy 1 jH JI
ck B T
/
,
/
,
Ž 3.19 . Ž 3.20 .
" where E H ,I are scaling functions. From these, one can obtain various results described in the literature. In particular, by linearizing Eqs. Ž3.17. and Ž3.18. in the ohmic regime, one finds that both components of
Table 1 A summary of the critical exponents for the friction and viscosity coefficients near a continuous glass transition at TG in three dimensions. Each transport coefficient diverges at TG as ; tya , where t s < T yTG
gH gI h hb hz ht hzt hx
n Ž zyz . n Ž z y2q z . n Ž z q2y z . n Ž z q2y z . n Ž zqz . n Ž zqz . n Ž z y2q3z . n Ž zqz .
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
transition, we can then read off the critical scaling of the viscosity coefficients: 2 zq 5yd h;j H g H; j H rj I , 2 zq 5yd hb ; j H g H; j H rj I , zq 3yd hz ; j I2 g H ; j H jI , 2 zq 3yd ht;j H g I; j H jI , zq 1yd 3 hzt ; j I2 g I ; j H jI , 2 zq 3yd hx ; j H g I ; j I2 g H ; j H jI .
Ž 3.23 .
The critical exponents for all the friction and viscosity coefficients for d s 3 are summarized in Table 1.
4. Scaling and hydrodynamics in confined geometries The flow of vortex liquids in confined geometries provides a powerful experimental tool to probe the shear resistance of vortex matter. Experiments of this type have been carried out by the group of Peter Kes in thin superconducting films w25,29,30x. In this two-dimensional case the vortex array is expected to melt from a solid into a liquid via the dislocation unbinding mechanism w39x. The shear modulus of the lattice vanishes continuously at the transition and is replaced by a shear viscosity in the liquid phase. The shear viscosity diverges as the transition is approached from the liquid side. In order to probe this behavior, Theunissen et al. w25x studied the flow of a two-dimensional vortex solid through narrow channels in a double-layer device, consisting of a weakly pinning amorphous Nb 3 Ge bottom layer, covered with a strongly pinning NbN thick layer. Using nanolithography, parallel channels were etched through the NbN layer into the NbGe layer. By applying a current normal to the direction of the channels, vortices where then forced to flow along the weakly pinning channels, while the NbN regions provide the strong-pinning boundaries w25x. By fitting their data to the form for the flux-flow resistivity of a vortex liquid in a channel obtained earlier by us via a simple hydrodynamic model w27,28x, these authors were able to extract the temperature dependence of the shear viscosity near melting, finding a behavior in agreement with the predictions of the theory of two-dimensional melting w39x.
117
As discussed in the Introduction, patterned irradiation of cuprate superconductors with heavy ions allows for experiments similar in spirit to the one carried out by Theunissen et al. w25x. These experiments can probe the growing shear viscosity of the vortex array near a continuous glass transition and may shed some light on the connection between static and dynamical properties of these glassy systems. Scaling theory can again be used to determine the temperature dependence of fields and currents in this spatially inhomogeneous situation arising from the confined geometry. A generalized homogeneity relation for the local electric field e H perpendicular to any correlated disorder from flux motion at position x in a channel of thickness L takes the form: eH Ž T , JH , x , L. yŽ1qz .
sl
ž
EH l
1r n
l n Ž 1q z . J H f 0 x L t, , , , ck B T l l
/
Ž 4.1 . n Ž . By choosing again l s ty H ; j H T we obtain:
eH Ž T , JH , x , L. . s jyŽ1qz EH H
ž
j H j I JH f0 ck B T
,
x
,
L
jH jH
/
.
Ž 4.2 .
In the entangled flux liquid the response is linear at small current. Upon expanding the right hand side of Eq. Ž4.2., we obtain for J H 0: eH Ž JH
™ 0, x , L.
0 ,rH
jH
ž / a0
™
2y z
J H F Ž xrj H , Lrj H . ,
Ž 4.3 .
0 0 . where r H s Ž n 0 f 0rc . 2 Ž1rg H is the Bardeen– Stephen resistivity of noninteracting flux lines, with 0 gH a bare friction. A scaling form for the resistivity r H ŽT, L. s DVrŽ LJ H ., with DV the net voltage drop across the channel, is easily obtained by integrating Eq. Ž4.3., with the result:
r H Ž T , L . s r H Ž T . f Ž Lrj H .
Ž 4.4 .
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M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
x r2 Ž . with f Ž x . s 1rxHyx r2 du F u, x a scaling function and r H ŽT . the bulk flux liquid resistivity given in Eq. Ž1.5.. Here g H is the renormalized friction coefficient that incorporates the growing Bose glass 0 Ž correlations near T BG , g H s g H j H ra0 . zy 2 , and diverges at the transition as g H ; < T y TBG
ity is obtained by integrating Eq. Ž4.5., with the result:
r H LŽ T , L . s r H Ž T . 1 y
2j H L
tanh
L
ž / 2j H
.
Ž 4.6 . If j H < L, we recover the bulk result given by Eq. Ž3.21.:
r H LŽ T , L . , r H Ž T . ; t n Ž zy z . .
Ž 4.7 .
Near the transition, however, j H 4 L, and the resistivity depends on the channel width and is controlled by the shear viscosity, with:
r H LŽ T , L . ,
s
r H L2 2 12 j H
n0 f 0
ž / c
2
L2 12h Ž T .
; L2 t n Ž zq2y z . .
Ž 4.8 . The strong divergence of the viscosity implicit in Eq. Ž4.8. is precisely the kind of behavior expected at a liquid–glass transition. The Bose glass transition is an example of a glass transition that is well understood theoretically and where precise predictions are available. 4.2. Corbino disk
4.1. Channel geometry The solution of the hydrodynamic equation for the simple channel geometry sketched in Fig. 2, with a homogeneous current J s yxˆ J H applied across the channel has been given elsewhere w26–28x and is displayed here for completeness. It is given by:
eH Ž x , L. s r H JH 1 y
cosh Ž xrj H . cosh Ž Lr2 j H .
.
Ž 4.5 .
Upon comparing Eq. Ž4.5. to Eq. Ž4.3., we identify the quantity in square brackets in Eq. Ž4.5. with the scaling function F. The scaling form for the resistiv-
Experiments in patterned geometries near the Bose glass transformation provide an exciting opportunity to probe viscous behavior near a second order glass transition. Other patterned geometries can be designed and used to probe some or all of the other viscosity coefficients. Of particular interest is the Corbino disk geometry, recently used by Lopez ´ et al. w32x for defect-free materials to reduce boundary effects in the flux flow measurements. This geometry was briefly discussed in Ref. w26x and is sketched in Fig. 4. In Ref. w26x we proposed the fabrication of a Corbino disk with Bose glass inner and outer contacts. The annular region corresponding to R 1 F r F R 2 is in the vortex liquid state. A constant current I is injected at the inner boundary of the cylindrical
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
119
flux liquid region and extracted at the outer boundary. The resulting current density is radial, with: Js
rˆ
I
, Ž 4.9 . 2p W r with W the thickness of the Corbino disk. This current induces tangential flow of the vortices, which in turn yields a radial voltage drop that can be probed by a suitable set of voltage taps, placed as sketched in Fig. 4. If the intervortex spacing a0 in the flux liquid is small compared to the size R 2 y R 1 of the annular channel where flux flow occurs, the flow can be described by the hydrodynamic Eq. Ž1.7.. Using cylindrical coordinates with the z axis directed along the direction of the external field H I c, the vortex flow velocity is in the azimuthal direction, z s Õf Ž r . fˆ , corresponding to a radial field, e r Ž r . s Ž n 0 f 0rc . Õf Ž r .. The nonlocal Ohm’s law takes the form: 2 jH
1 d
r
d
r dr dr
ž
er Ž r . y 1 q
2 jH
r
2
/
er Ž r . s y
aL gHr Ž 4.10 .
where a L s n 0 f 0 IrŽ2p Wc . controls the strength of the Lorentz force. The general solution of Eq. Ž4.10. is given by: rHI jH er Ž r . s q c1 I1 Ž rrj H . 2p Wj H r qc2 K 1 Ž rrj H . ,
Ž 4.11 .
Fig. 5. The electric field profile for the Corbino disk geometry, with R1 s 2 mm and R 2 s12 mm, with an annular width R 2 y R1 s10 mm. The vertical axis represents the reduced field 2p e r Ž r .rŽ r H I . in mm. The dashed line is the electric field for vanishing viscosity, e r0 Ž r . s r H Ir2p W Ž1r r .. The shaded regions represent the Bose glass contacts.
The field nonlocality arising from the growing correlation length near the Bose glass transition can be probed experimentally by measuring the voltage profile across the annular channel. A series of equally spaced contacts are placed radially, as shown in Fig. 5, at positions rn s R 1 q nd, for n s 1,2, . . . , N. For the magnetic fields and temperatures of interest, the spacing d of the contacts is large compared to the intervortex spacing a 0 , so that hydrodynamics can be applied. The voltage drop across two successive contacts is obtained immediately by integrating Eq. Ž4.11. and it is given by: DV Ž rnq 1 ,rn . s
Hr
rnq1
dre r Ž r . s
n
where I1 and K 1 are Bessel functions. The constants c1 and c 2 are determined by requiring the liquid flow velocity, and therefore the electric field, to vanish at the boundaries with the Bose glass regions, e r Ž R 1 . s e r Ž R 2 . s 0, with the result: c1 s c2 s
K 1 Ž r 2 . rr 1 y K 1 Ž r 1 . rr 2 K 1 Ž r 1 . I1 Ž r 2 . y K 1 Ž r 2 . I1 Ž r 1 . I1 Ž r 1 . rr 2 y I1 Ž r 2 . rr 1 K 1 Ž r 1 . I1 Ž r 2 . y K 1 Ž r 2 . I1 Ž r 1 .
,
Ž 4.12 .
,
where r 1,2 s R 1,2rj H . As in the channel problem, spatial inhomogeneities are controlled by the in-plane correlation length j H . The field profile for a few values of j H in a micron-scale sample is shown in Fig. 5.
rHI 2p W
ln Ž rnq1rrn .
qc1 I0 Ž rnq1rj H . y I0 Ž rnrj H . yc2 K 0 Ž rnq1rj H . y K 0 Ž rnrj H .
4 . Ž 4.13 .
The temperature dependence of the correlation length can then, in principle, be extracted by fitting the measured voltage to Eq. Ž4.14.. For comparison it is useful to discuss the limiting cases of very small and very large correlation length. Away from the Bose glass transition, where j H < R 1 , R 2 ,d, viscous forces are negligible and the boundary condition of vanishing flow velocity at the Bose glass boundaries cannot be satisfied. The field from vortex motion is simply: e r0 s
rHI 1 2p W r
.
Ž 4.14 .
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
120
The voltage drop across each pair of contacts is then given by: DV0 Ž rnq1 ,rn . s
rHI 2p W
ln Ž rnq1rrn .
Ž 4.15 .
and is controlled by the bulk flux flow resistivity r H given in Eq. Ž1.8.. In this limit, the vortex liquid only has very short ranged correlations; the local electric field is simply proportional to the local current and decreases as ; 1rr. As a result, the voltage across every successive pair of contacts decreases monotonically at all temperatures as one moves from the center to the outer perimeter of the Corbino disk, i.e., V0 Ž r 2 ,r 1 . ) V0 Ž r 3 ,r 2 . ) . . . ) V0 Ž rnq1 ,rn .. Near the transition, when the correlation length becomes comparable to the channel width, viscous effects are dominant and the field profile can be approximated by: e`r Ž r . s
rHI 2 4p Wj H
b2
b1 r y
r
y r ln Ž rrj H . ,
Ž 4.16 . with b 1 ,b 2 ) 0 given by: R 22 ln Ž R 2rj H . y R 12 ln Ž R 1rj H .
b1 s
R 22 y R 12 R 12 R 22
b2 s
R 22 y R 12
,
Ž 4.17 .
ln Ž R 2rR1 . .
The voltage drop across two successive contacts is then given by: DV`Ž rnq1 ,rn . s
rHI 2 4p Wj H
½
2 b1 q 1 4
2 2 Ž rnq 1 y rn .
yb 2 ln Ž rnq1rrn . y yrn2 ln Ž rnrj H .
5
.
1 2
2 rnq1 ln Ž rnq1rj H .
Ž 4.18 .
The first term on the right hand side of Eq. Ž4.16. can be easily understood as it corresponds to the field resulting from the rigid body rotation of a vortex solid at an angular frequency v s n 0 f 0
Fig. 6. The voltage drop across a series of equally spaced contacts located radially at rn s R1 q nd, for ns1,2, . . . ,5. The vertical axis represents the voltage across two neighboring contacts scaled by the corresponding voltage obtained for j H < d, i.e., Vnq1, n s DV Ž r n q 1 , r n . r DV 0 Ž r n q 1 , r n . , where DV Ž r n q 1 , r n . and DV0 Ž rnq1 ,rn . are given by Eqs. Ž4.13. and Ž4.15., respectively. We have chosen R1 s d and R 2 s6 d. The voltage is plotted as a function of d r j H which increases with temperature, as discussed in the text.
IrŽ8p cWh .. In this rigid body limit the electric field grows with r w43,44x. As a result, the voltage across two successive contacts increases at all temperatures as one moves from the center to the outer perimeter of the Corbino disk, i.e., V0 Ž r 2 ,r 1 . - V0 Ž r 3 ,r 2 . . . . - V0 Ž rnq1 ,rn .. In general, as the temperature is decreased towards the Bose glass transition, one will observe a crossover from liquid-like Ž e r ; 1rr . to solid-like Ž e r ; r . response of the vortex array. The voltages across each successive pair of five contacts are plotted in Fig. 6 as functions of drj H ŽT .. The correlation length j H ŽT . increases with temperature as the Bose glass transition is approached from above. The figure therefore displays the growth of the voltage with increasing temperature. At high temperature, where j H < d, the voltage is given by Eq. Ž4.15., which is scaled out, and all curves approach 1. The scaled voltage drop across successive pair of contacts is no longer a monotonic function of temperature. Rather it first increases as then decreases as one moves from the center towards the outer border of the disk. 5. Response at finite frequency The scaling theory of continuous glass transitions in bulk superconducting samples is easily general-
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
ized to a finite frequency v , as described in Refs. w6x and w41x. It is simply obtained by adding another scaling combination ; v l z to the scaling functions of Eqs. Ž3.17. and Ž3.18. and it has been tested experimentally w42x. Finite-frequency scaling at the Bose glass transition in bulk was worked out in Ref. w20x. Similarly, we can generalize to finite frequencies the scaling theory for spatially inhomogeneous flow in constrained geometries. For simplicity we refer again to the channel geometry of Fig. 2 and only discuss the response of the vortex liquid to a spatially homogeneous current of finite frequency v applied across the channel in the ab plane. The generalized scaling ansatz based on a renormalization group flow for the spatially inhomogeneous field from flux motion is:
Conversely, we can approach the transition along the frequency axis by letting T s T BG and using a finite frequency to tune the distance from the critical point. In this case, we fix l by choosing v˜ Ž l ) . s 1, v which gives j H ; l ) s vy1 r z. If the transition is approached along the T s TBG line, the scaling ansatz becomes: e H Ž TsT BG , J H , v , x , L . v sŽ jH .
=´v
y Ž1qz .
žŽ j
v n Ž1q z . JH H
.
with t 0 a microscopic time scale. The flow diagram is sketched in Fig. 7. Clearly, the behavior near the critical point depends on how the transition is approached in this plane. For v s 0 we fix the length l as before by choosing t˜Ž l ) . s t l )1r n s 1, which gives j H ŽT . ; l ) s tyn and yields the temperature dependence discussed earlier for the DC response near the transition. The same analysis should hold at finite, but low frequencies, provided at l ) we have t˜Ž l ) . 4 v˜ Ž l ) ., with v˜ Ž l . s vt 0 l z. This corresponds to z the condition v < 1rt ŽT ., with t ŽT . ; j H the relaxation time of critical fluctuations.
v ,Ž j H .
v x ,Ž j H .
y1
L .
/
As before, we are interested in the response in the vortex liquid phase, where the current–voltage characteristic is linear at small currents and we can write: e H Ž T s T BG , J H 0 srH
v jH
™ 0, v , x , L.
2y z
ž / a0
v v J H Fv Ž xrj H , Lrj H ..
Ž 5.3 .
By integrating the field across the channel, we immediately obtain the net voltage drop and the corresponding AC resistivity as: v r H LŽ TBG , L, v . s r H Ž TBG , v . fv Ž Lrj H .,
Ž 5.4 .
where: 0 r H Ž TBG , v . s r H
v jH
ž / a0
2y z
; Ž iv .
1y2rz
.
Ž 5.5 .
is the AC resistivity in bulk samples w20x. Both real and imaginary parts of the linear frequency-dependent resistivity vanish as v 0 with the same critical exponent, as obtained earlier in Ref. w20x. The scaling function in Eq. Ž5.3. is simply fv Ž x . s r2 Ž1rx .Hqx Ž . yx r2 du Fv u, x . For x 4 1, the AC resistivity in the channel must reduce to the bulk result, which requires fv Ž x 4 1. s 1. To determine the form of the scaling function we assume again that at long wavelengths the local field from flux motion is described by the hydrodynamic equations discussed in Section 2. The use of hydrodynamics for describing the AC response of currentdriven vortex liquids has been discussed in Refs. w45,46x. Both friction and viscosity coefficients are in
™
Fig. 7. A sketch of the flow diagram in the Ž v˜ ,t˜ . plane for a few initial values of vt 0 r t n z .
y1
Ž 5.2 .
eH Ž T , JH , v , x , L. s lyŽ1 qz . e H Ž l 1r n t ,l n Ž1q z . J H ,l zvt 0 ,ly1 x ,ly1 L . , Ž 5.1 .
121
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
122
general frequency-dependent. For the simple channel geometry, there is again only one hydrodynamic equation for the Fourier components of the the flow velocity at frequency v , given by: yg H Ž v . z q h Ž v . = 2 z s
1 c
n 0 f 0 zˆ = J Ž v . .
Ž 5.6 . Determining the frequency dependence of the friction and viscosity coefficients requires a microscopic calculation that is beyond the scope of the present paper. However, their scaling with frequency at the transition can be readily obtained. The hydrodynamic Eq. Ž5.6. defines a frequency dependent viscous length, h Ž v . rg H Ž v . . It is natural to identify this length with the diverging Bose glass correlation length:
(
v jH ;
(
hŽ v. gH Ž v.
.
Ž 5.7 .
The complete scaling function defined by Eq. Ž5.3. is then readily obtained by solving Eq. Ž5.6. for no slip boundary conditions and it is found to have the same functional form as that obtained for the DC response. The AC resistivity for the channel geometry if given by:
r H LŽ TBG , L, v . s r H Ž TBG , v . 1 y
v 2j H
L
tanh
L
ž / v 2j H
,
Ž 5.8 .
where r H ŽTBG , v . is the bulk AC resistivity given in Eq. Ž5.5.. As for the DC case, one obtains the following behavior:
r H LŽ TBG , L, v . f
ž /
1y 2rz
n0 f 0
2
ž / c
v ; L2 Ž j H . v for j H 4 L.
1
v The condition j H ; L defines a sample-dependent crossover frequency v L s Ž a 0rL. zrt 0 ; Lyz below which the channel geometry becomes important and r H L ; i v L2 . These results describe a Meissner-type response of the superconductor that arises because the vortices are pinned and immobile in the Bose glass phase. The behavior observed as the critical point is approached along an arbitrary line in the Ž v ,t . plane depends on the location of that line. In general, we expect that the v s 0 scaling results apply for v < 1rt ŽT . ; t z , while the scaling for T s T BG will apply for v 4 1rt . The various regions for the expected scaling of the AC response are sketched in Fig. 8. Here the temperature scale t L is defined by j H ŽT . ; L, with t L ; Ž a0rL.1r n . For t ) t L the vortex array is insensitive to the confined geometry and the response is that of a bulk sample. For temperatures below t L , the geometry becomes important.
gH Ž v.
c
; Ž iv .
r H LŽ TBG , L, v . f
2
n0 f 0
Fig. 8. A sketch of the scaling behavior expected for the AC response in various regions of the Ž v ,t . plane. The solid line is a plot of v s1rt ŽT . s t z n rt 0 . The frequency and temperature scales v L and t L represent the scales below which the confined vL sample geometry becomes important. They are defined by j H s L, or v Lt 0 s Ž a 0 r L. z , and by j H ŽTL . s L, which gives t L s Ž a 0 r L.1r n . The AC resistivity r H LŽ v , T . is expected to scale as follows deep in each of the four regions sketched in the figure: region I, r H L ; L2 t n z ; region II, r H L ; L2 Ž i v .; region III, r H L ; Ž i v .1y 2r z ; region IV, r H L ; t n Ž zy2..
,
v for j H < L, Ž 5.9 .
L2 12h Ž v .
yz
; L2 Ž i v . ,
Ž 5.10 .
Acknowledgements This work was supported by the National Science Foundation at Syracuse through Grants No. DMR9730678 and DMR98-05818 and at Harvard through Grant No. DMR97-14725, and by the Harvard Materials Research Science and Engineering Center through Grant No. DMR98-09363.
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
123
Appendix A. Comparison with the hydrodynamic formulation of Mou et al.
over the two values x and y. The friction tensor is given by:
Mou et al. have used time-dependent Ginzburg– Landau theory to evaluate the nonlocal DC conductivity tensor Ýmn Ž r,rX . defined in Eq. Ž2.5.. Assuming nonlocal effects are slowly varying on the length scale of interest, one can expand the right hand side of Eq. Ž2.5. retaining terms up to quadratic in the gradients of the electric field. At long wavelengths, the nonlocal relation between fields and currents then takes the form:
g˜mn , l r s
jm Ž r . s smn Ž 0 . en Ž r . y Sm a bn Ea Eb en Ž r . ,
Symmetry under rotations about the z direction also restricts the number of independent components of the viscosity tensor and the related tensor Sma bn to six. The tensor Sma bn is given by:
Ž 6.1 .
where smn Ž0. is the usual long-wavelength conductivity and the tensor Sma bn describes the effect of nonlocality to quadratic order in the gradients. This fourth order tensor has six independent components that were evaluated in Ref. w35x. Upon comparing Eq. Ž6.1. to Eq. Ž2.30. and recalling the relationship between the fields and the vortex densities and fluxes given by the long-wavelength limit of Eqs. Ž2.11. and Ž2.13.: b s f0T ,
em s
f0 c
Sga bs s
c
emn j Qn j ,
Ž 6.2 .
egmn g˜mn , l r el rs ,
c2
e h e . 2 gmn ˜mn , a b , l r l rs
f0
Ž 6.3 . Ž 6.4 .
with:
sx x Ž 0 . s
c
2
ž / n0 f 0
gH ,
sz z Ž 0 . s
2
c
ž / n0 f 0
gI .
Ž 6.7 .
H H Sma bn s S x x x x dmn da b q Ž S x y y x y S x x x x . H H H da b y 12 Ž dmHa dbnH qdmHb dan = dmn . H q S x z z x dmn da z db z q S z x x z daHb dm z dn z
H H qdb z dn z daHm qdb z dm z dan qda z dn z dbm ..
Ž 6.8 . The viscosity tensor is given by: 1 2 n20
H a b emng H eg H l r
½ hd
qh b daHb emng H eg H l r y 12 Ž emn a H eb H l r q emnb H ea H l r . qhz da z db z emng H eg H l r
Neglecting Hall voltages, the local conductivity tensor is diagonal and has only two independent components, due to the rotational symmetry in the plane normal to the applied field Ž xy plane., sx x Ž0. s sy y Ž0. and sz z Ž0., which gives:
sab Ž 0 . s sx x Ž 0 .
Ž g H emn a H ea H l r q g I emn z ea l z . , Ž 6.6 .
h˜mn , a b , l r s
2
f 02
2 n 20
q S z z z z dm z da z db z dn z q S x x z z Ž da z dm z dbnH
we see immediately that the local conductivity tensor smn Ž0. and the tensor Sm a bn are simply proportional to the friction and viscosity tensor, respectively, according to:
sgs Ž 0 . s
1
daHb qsz z
Ž 0 . da z db z ,
H qh tdab emn z e z l r
qhzt da z db z emn z e z l r q 12 hx da z Ž emn z eb H l r q emnb H e z l r .
Ž 6.5 .
where d H ab s da H , b H s da b y da z db z and the labels with a H subscript, e.g., a H , b H , . . . , only run
qdb z Ž emn z ea H l r q emn a H e z l r .
5, Ž 6.9 .
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
124
with: Sx x x x s
Sx z z x s
2
c
ž / ž /
h,
n0 f 0 c
2
hz ,
n0 f 0
Ž Sx y y x y Sx x x x . s Sz x x z s
Sz z z z s
Sx x z z s
c
ž / n0 f 0
2
hb ,
2
c
ž / ž / ž /
h t,
n0 f 0
2
c
n0 f 0
1
c
2
n0 f 0
hzt , 2
hx .
Ž 6.10 .
Mou et al. w35x and, more recently, Blum and Moore w36,37x evaluated the lowest order fluctuation contribution to the components of the tensor Sma bn for a vortex liquid using a time-dependent Ginzburg–Landau. They found that some of the coefficients are negative near the Hc2 line where their calculation applies, indicating that hydrodynamics may no longer be applicable at such high fields.3
Appendix B. DC flux transformer experiments DC flux transformer experiments have been used as probes of the nonlocal resistive response of vortex liquids. In particular, by comparing transport measurements in twinned and untwinned YBCO, Lopez ´ et al. w47x argued that in the twinned crystal, where the liquid transforms into a solid via a continuous glass transition, measurements in the transformer configuration may provide a direct probe of the longitudinal correlation length near the transition. Here we reconsider the analysis of such experiments in the context of hydrodynamics following earlier work by Huse and Majumdar w34x. The role of nonlocality in the DC flux transformer geometry was also reconsidered more recently by Phillipson et al.
w48x. Our objective is to make the connection between the measured voltages and the diverging correlation lengths more precise. As pointed out by Huse and Majumdar, explicit calculations of the current and voltage patterns have to be carried out for each specific sample geometry by solving a fourth order partial differential equation with rather complicated boundary conditions. Here we reformulate the problem discussed in Ref. w34x incorporating all relevant viscosity coefficients, then discuss the solution in terms of diverging length scales. We also correct Eq. Ž7. of Ref. w34x where some boundary terms were left out. We are interested in discussing DC transport experiments in finite materials of specified geometry, where the current is injected and withdrawn via contacts placed at the materials’ boundaries. As discussed by Huse and Majumdar, in the bulk of the sample in steady state the total current satisfies = P j s 0 and the electric field is irrotational, = = e s 0. The relationship between current and field is given by the nonlocal Ohm’s law, Eq. Ž2.5., which at long wavelength takes the form given in Eq. Ž6.1.. The field e can be written in terms of a local voltage as: e s y=F ,
Ž 7.1 .
and the nonlocal Ohm’s law transforms into a fourth order differential equation for the voltage, F :
smn Ž 0 . Em En y Sm a bn Em Ea Eb En F s 0.
Ž 7.2 .
The sample boundaries separate a region where the local field or vortex flow velocity can have spatial gradients due to viscous forces among the vortices from the outside region where no such spatial gradients occur. Neglecting nonlocalities on length scales of the order of the penetration length, the first spatial derivatives of the field e Žor equivalently of the vortex flux tensor Qmn . can therefore exhibit jump discontinuities at the sample boundaries. Such discontinuities correspond to d-function contributions to the local current, denoted by j d. Considering a local coordinate system with an s axis normal to the sample boundary, located at s s 0, and directed in-
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
125
wards, the nonlocal Ohm’s law at the boundary takes the form: jm Ž r . q jmd Ž r . s smn Ž 0 . en Ž r . y Sm a bn Ea Eb en Ž r . y d Ž s . Sm s sn En en Ž r .
s
™0
q
,
Ž 7.3 .
where the subscript s is not summed over. The last term on the right hand side of the equation equals the d function contribution to the surface current. Such contribution must be flowing within the surface of the sample, i.e., its component normal to the boundary must vanish: j sd s S s s sn w Es en x s™ 0qs yS s s sn w Es En F x s™ 0qs 0.
Ž 7.4 .
This provides the first set of boundary conditions for Eq. Ž7.2.. The second boundary condition is obtained by requiring that the d-function part of the divergence of the current at the surface equals the total current Is Ž s . injected at that point of the surface: d Ž = P j . s = P j ds y d Ž s . Sm H s sn Em H En en Ž r .
s Is Ž s . ,
s
™0
q
Ž 7.5 .
where again the index s is not summed over and m H only runs over the two components perpendicular to the surface. This requires that the voltage at the surface satisfies:
ssn Ž 0 . En F y S s a bn Em Ea Eb En F y Sm H s sn Em H Es En F y2Sm H n s s Em H Es En F
ss 0 q
s Is Ž s . .
Fig. 9. The DC flux transformer geometry.
Ž 7.6 .
The last term in square brackets on the left-hand side of Eq. Ž7.6. was absent in Ref. w34x. The specific transformer configurations of interest are shown in Fig. 9. We neglect spatial inhomogeneities in the x direction Žparallel to the flow. and reduce the problem to a two-dimensional one. The sample has finite extent W in the y direction and thickness L in the external field direction. Current is injected and withdrawn at the contacts shown placed on the upper and lower surface of the sample. Therefore, no current is injected at the boundaries normal to the y direction. In order to discuss the role of the various viscosity coefficients in controlling the nonlocal response of the vortex
array, it is useful to return to our hydrodynamic equations in terms of vortex densities and fluxes. In the geometry of interest, there are two nonvanishing components of the electric field from flux motion, related to the corresponding components of the vortex flux tensor as: e y Ž y, z . s e z Ž y, z . s
n0 f 0 c n0 f 0 c
Õ x Ž y, z . , V Ž y, z . .
Ž 7.7 .
From Eq. Ž2.15. in a steady state vortex current is conserved, which requires: Ez V s E y Õ x ,
Ž 7.8 .
This condition is equivalent to the requirement that = = e s 0 and implies that the components of the vortex flux tensor can be derived by a potential, FÕ , according to: Õ x Ž y, z . s E yFÕ , V Ž y, z . s EzFÕ ,
Ž 7.9 .
where FÕ is simply proportional to the voltage defined in Eq. Ž7.1., FÕ s yŽ crn 0 f 0 .F . The hydro-
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
126
dynamic equations governing vortex flow in the transformer geometry shown in Fig. 9 are: c 44 g H Õ x s Ž hE 2y q hz Ez2 . Õ x q hx E y Ez V q E t n0 z x q
n0 f 0 c
Jy ,
Ž 7.10 .
with the boundary conditions:
g H E yFÕ y hz Ez2 E yFÕ g I EzFÕ y hz E 2y EzFÕ
ys0,W
zs0, L
s 0,
s"
c n0 f 0
Iz Ž y," Lr2 . .
Ž 7.15 .
g I V s Ž h tE 2y q hzt Ez2 . V q hx E y Ez Õ x y
c 44 n0
Ey t x q
n0 f 0 c
Jz .
Ž 7.11 .
By differentiating Eq. Ž7.10. with respect to y and Eq. Ž7.11. with respect to z and making use again of the fact that the total current is divergence-free in bulk, we immediately obtain the equation for the potential FÕ :
g H E 2yFÕ q g I Ez2FÕ y hE 4y q Ž hz q h t q 2hx . E 2y Ez2 qhzt Ez4 FÕ s 0.
hzt Ez2FÕ
ys0,W
s 0,
zs0, L
s 0,
`
Ý i n" cos Ž np yrW . .
I Ž y, z s "Lr2. s
Ž 7.16 .
ns0
Ž 7.12 .
This fourth order differential equation has to be solved with the boundary conditions:
h E 2yFÕ
The solution for an arbitrary distribution of current sources and sinks has been given by Huse and Majumdar w34x. Simply translating their results into our notation, we write the current sources at the top and bottom of the sample as:
The integral of the current injected or withdrawn over the entire sample surface must vanish. This y requires iq 0 s yi 0 . Making use of the boundary conditions at x s 0,W, the voltage is then written as: `
g H E yFÕ y hE 3yFÕ y Ž hz q 2hx q h t . Ez2 E yFÕ
ys0,W
F Ž y, z . s
Ý Un Ž z . cos Ž np yrW . ,
Ž 7.17 .
ns0
s 0,
g I EzFÕ y hzt Ez3FÕ y Ž hz q 2hx q h t . E 2y EzFÕ s"
c n0 f 0
ž
Iz y, z s "
L 2
/
.
zs0, L
Ž 7.13 .
To proceed, we follow Huse and Majumdar and neglect viscous drag associated with h and hzt Žthe bulk viscosity h b drops out of the problem for linear incompressible flow.. This amounts to dropping the terms ; E 4y and ; Ez4 compared to the fourth order cross derivatives in Eq. Ž7.12.. Letting h˜ z s hz q h t q 2hx ,4 the equation simply reduces to:
g H E 2yFÕ q g I Ez2FÕ y hz E 2y Ez2FÕ s 0,
4
Ž 7.14 .
In Ref. w34x, only the viscosity coefficient hz was retained from the outset in the hydrodynamic equations.
where: U0 Ž z . s C0 q S0 z , Un Ž z . s Cn cosh Ž K n z . q Sn sinh Ž K n z . , n ) 0, Ž 7.18 . with:
Kns
np W
ž
gH ŽT . gI ŽT .
= 1q
1r2
/
hz Ž T . gI ŽT .
y1 r2
Ž nprW .
2
.
Ž 7.19 .
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
The coefficient C0 sets an arbitrary zero for the voltage. We will let C0 s 0 below. The other coefficients are given by: S0 s r I iy 0 , Sn s
q r H Ž iy n y i n . K n Ž Wrnp .
2
Cn s y
rH Ž
2
, n ) 0,
j I2 s hz Ž T . rg H Ž T . .
2
We begin by discussing the case of vanishing viscosity. Then K n is simply given by:
. K n Ž Wrnp . , n ) 0. sinh Ž K n Lr2 . Ž 7.20 .
Now we use this solution to discuss the experimental finding of Lopez ´ et al. w47x in twinned and untwinned samples of YBCO. These authors have carried out two sets of measurements. The first consists in injecting current at the left contact at the top of the sample and extracting it at the right contact, as shown in Fig. 9. The voltages VTOP and V BO TTOM across the two central contacts at the top and bottom of the sample are then measured as functions of temperature. For this choice of current q sources, iy n s 0, for all n, and i 0 s 0. The voltage at the top and bottom of the sample is then given by:
` 1 W s y r H Ý iq n cos Ž np yrW . K n 2 np ns1
cosh Ž K n Lr2 . sinh Ž K n Lr2 .
"
sinh Ž K n Lr2 . cosh Ž K n Lr2 .
gI ŽT . hz Ž T . gI ŽT .
s
s
g I0
.
jI
hz0 g I0
jH a0
gI
; t 2 n Ž zy1. ,
Ž 7.22 .
2
; t 2n ,
W
(
rI rH
; t 2 n Ž zy1. .
Ž 7.25 . It vanishes therefore at the Bose glass transition Ž z s 2., but it remains finite at the isotropic vortex glass transition Ž z s 1.. Choosing for simplicity a q current distribution with iq 1 / 0 and i n s 0 for all other values of n, the voltage for h˜ z s 0 is given by:
F 0 Ž y," Lr2 . 1 sy
(r 2
q I r H i 1 cos Ž p yrW .
cosh Ž K 10 Lr2 . sinh Ž K 10 Lr2 .
F 0 Ž y," Lr2 . f yr H
"
W
2
ž / p
sinh Ž K 10 Lr2 . cosh Ž K 10 Lr2 .
,
Ž 7.23 .
W2
p 2L
iq 1 cos Ž p yrW . ,
Ž 7.27 . and the voltage at the top and bottom of the sample are equal. Conversely, if K 10 L 4 1, we find:
(
F 0 Ž y,q Lr2 . f y r I r H F 0 Ž y,y Lr2 . f 0,
2
ž / ž /
(
np s
with K 10 given by Eq. Ž7.25. for n s 1. Close to the glass transition where K 10 ; t 2 n Ž zy1. we can use K 10 L < 1 to obtain:
The temperature dependence of the voltages is controlled by that of the inverse length K n , given in Eq. Ž7.19., which in turn depends on the friction and viscosity coefficients which diverge near the vortex glass and the Bose glass transitions with the critical exponents discussed earlier. In particular, we recall that:
jH
W
gH
Ž 7.26 .
Ž 7.21 .
0 gH
np
Ž 7.24 .
2
ž /
gH ŽT .
K n f K n0 s
=
F Ž y," Lr2 .
=
where we have extracted the divergence by rewriting all transport properties in terms of their bare values Ždenoted by a superscript ‘‘0’’., which depend only weakly on temperature at the transition. The longitudinal correlation length will be defined as:
2
cosh Ž K n Lr2 . q iy n qin
127
W
p
iq 1 cos Ž p yrW . ,
Ž 7.28 .
with corrections to the above expressions decreasing 0 exponentially as ; eyK 1 L. In this case, the vortices behave like uncorrelated pancakes and the bottom voltage is much smaller than the one at the top. In other words, there is a crossover at K 10 L ; 1, corre-
M.C. Marchetti, D.R. Nelsonr Physica C 330 (2000) 105–129
128
sponding to r I L2r4 ; r H W 2rp 2 , from a regime where the top voltage exceeds the bottom voltage to one where both voltages are the same. Near the Bose glass transition, where K 10 ; t 2 n , this crossover is sharp and occurs at a temperature that depends on both the width W and the thickness L of the sample 0 and is given by t )n ; Ž2Wrp L. g I0 rg H . In contrast, near the vortex glass transition where z s 1, K 10 is weakly temperature dependent and no sharp crossover is expected. Consider now the response in the case where the viscosity hz is very large, with Žhzrg I .ŽprW . 2 4 1, so that for all values of n:
(
K n f K `n s
(
gH hz
1 s
jI
.
Ž 7.29 .
In this case, the top and bottom voltages for the first experiment ŽFig. 9. are given by:
F`Ž y," Lr2 . fy
1 r H cosh Ž Lr2 j I . 2 jI
sinh Ž Lr2 j I .
`
=
Ý
iq n cos
Ž np yrW .
ns1
" W
sinh Ž Lr2 j I . cosh Ž Lr2 j I . 2
ž / np
.
Ž 7.30 .
The crossover is now controlled by the length j I ; tyzn . If Lr2 j I 4 1, the voltage reduces to:
rH jI
`
Ý iqn cos Ž np yrW . ns1
W
2
ž /
,
np
F`Ž y,y Lr2 . f 0,
Ž 7.31 .
F`Ž y," Lr2 . rH L
`
Ý ns1
iq n cos Ž np yrW .
W
ž / np
2
.
`
s iy 0 rILq2 rH
Ý iyn cos Ž np yrW . ns1
=K n
W
ž /
DF Ž y . s iy 0 r IL
i.e., voltages are uncorrelated well above the glass transition. As the glass transition is approached and Lr2 j I < 1, we obtain:
fy
DF Ž y . ' F Ž y, Lr2 . y F Ž y,y Lr2 .
np
2
tanh Ž K n Lr2 . .
Ž 7.33 .
For simplicity, we assume the currents injected at the top and withdrawn at the bottom are uniform in y, q y q i.e., iy 0 s yi 0 s constant, and i n s yi n s 0 for n / 1. The voltage is then simply:
F`Ž y,q Lr2 . fy
Their vanishing at the transition is controlled by the vanishing of r H . We find a sharp crossover from a high temperature region where the top voltage exceeds the bottom voltage to a low temperature region where the two voltages are equal. the crossover temperature T U depends on the sample thickness and is given by j I ŽT U . ; Lr2. It is therefore expected to decrease with sample thickness according to T U ; T BG Ž Lra0 .y1 r zn , consistent with the observations of Lopez ´ et al. in twinned samples. For T - T U the voltages are the same and decreasing with decreasing temperature, vanishing at T BG as r H ; t n Ž zy z .. The second set of measurements carried out by Lopez ´ et al. consists of injecting a current at the top surface and extracting it at the bottom surface, while measuring the voltage across two contacts at z s "Lr2 and at the same y position, as sketched in Fig. 9. The corresponding distribution of current y sources and sinks corresponds to iq n s yi n , for every n. The voltage difference between top and bottom is given by:
Ž 7.32 .
In this case, the top and bottom voltages are the same and they are both reduced by a factor j IrL compared to the top voltage at high temperature.
Ž 7.34 .
and for all values of y it is controlled by the c-axis resistivity i I , which vanishes at the glass transition.
References w1x G.W. Crabtree, D.R. Nelson, Phys. Today 50 Ž1997. 38, and references therein. w2x G. Blatter et al., Rev. Mod. Phys. 66 Ž1994. 1125. w3x G.W. Crabtree, W.K. Kwok, U. Welp, D. Lopez, J.A. ´ Fendrich, in: S. Bose, R. Kossowski ŽEds.., Proceedings of the NATO Advanced Study Institute on the Physics and Materials Science of Vortex States, Flux Pinning and Dynamics, Kluwer Academic Publishers, 1999. w4x D.R. Nelson, Phys. Rev. Lett. 60 Ž1988. 1973.
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