CONDUCTANCE OF SUPERCONDUCTOR-NORMAL METAL...
Transcript of CONDUCTANCE OF SUPERCONDUCTOR-NORMAL METAL...
CONDUCTANCE OF SUPERCONDUCTOR-NORMAL METAL CONTACT JUNCTIONBEYOND QUASICLASSICAL APPROXIMATION
BY
VLADIMIR LUKIC
BSc, University of Belgrade, 1997
DISSERTATION
Submitted in partial fulfillment of the requirementsfor the degree of Doctor of Philosophy in Physics
in the Graduate College of theUniversity of Illinois at Urbana-Champaign, 2005
Urbana, Illinois
CONDUCTANCE OF SUPERCONDUCTOR-NORMAL METAL CONTACT JUNCTIONBEYOND QUASICLASSICAL APPROXIMATION
Vladimir LukicDepartment of Physics
University of Illinois at Urbana-Champaign, 2005Anthony J. Leggett, Advisor
The subject of this thesis is a study of the superconductor-normal metal (SN) contact
junction by systematically treating the corrections of the order ∆/EF in momentum and
conductance. We isolated the effects that are already present in the original formulation of
Blonder-Tinkham-Klapwijk (BTK) model, but were neglected as the small quantities of the
order ∆/EF .
The corrections studied are: non-equal momenta of various particles in the system, self-
consistent finite gap onset length scale, non-exact retro-reflection in Andreev process of the
particles with finite energy, non-trivial renormalization of the barrier potential due to the
non-equal momenta at finite incidence angle, and effects due to an anisotropy of the systems
in contact. The main question is what is the interplay of these effects, and can they con-
structively add to produce the effect of the order 1. The answer required treatment of all the
effects from the outset at the same level, and incorporation of these effects in a self-consistent
calculation. To achieve that, a new method for self consistent calculation of the behavior
of gap at the SN contact is developed, which does not use the quasiclassical approximation,
but rather finds solution to the Bogoliubov - De Gennes equations in a simplified, step-wise
constant, model of the gap. The conductance is calculated using the same method, thus
guaranteeing the same accuracy.
A study of self-consistently obtained solution shows that these corrections often have an
effect opposite to each other, or have the same target states, which limits the overall effect.
As a consequence even for large ∆/EF the overall correction is still relatively small, and the
conductance of the system does not differ much from the simple BTK model. We have thus
shown the reason for robustness of BTK model, and gained a better view of what might be
the cause of larger discrepancies between this simple model and experiment.
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Acknowledgments
Thanks to my advisor Tony Leggett, for his patience while I was trying to find myself in
physics (and world in general), and for the innumerable sound advices he gave me during
all these years. Thanks to Jim Eckstein and Laura Greene, who taught me how to perceive
physics from the experimental side. Thanks to my friends and collegues - Joseph Jun,
Geoffrey Warner, Vivek Aji, Carl Tracy, Argyrios Tsolakidis, Julian Velev. Thanks to to my
family - Veljko, Milica and Natasa, for everything. Thanks to Pero, Momir, Zarija, Tijana,
Dimitrios, Nemanja, Sale...to all my friends. Most of all, thanks to Maki.
I acknowledge financial support from the National Science Foundation under grants NSF
DMR 03-50842, NSF DMR 99-86199, NSF DMR 96-14133, NSF DMR 91-2000COOP, from
MRL DOE grant, and from the Department of Physics, University of Illinois.
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Table of Contents
List of Figures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . viii
Chapters
1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1.1 Superconductor-Normal Metal Contact Junctions and Andreev Reflection . . 2
2 The Bogoliubov-De Gennes Equations and the Blonder-Tinkham-Klapwijk Model 8
2.1 Bogoliubov - DeGennes Equations . . . . . . . . . . . . . . . . . . . . . . . . 8
2.2 The Model of Blonder, Tinkham and Klapwijk . . . . . . . . . . . . . . . . . 10
3 The Nature of Gap Edge Conductance Peak, Subgap Conductance and Zero-Bias
Properties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
4 Corrections to the BTK Conductance . . . . . . . . . . . . . . . . . . . . . . . . . 28
4.1 Finite Gap Onset Length and Exact Momenta . . . . . . . . . . . . . . . . . 30
4.2 Non-exact Retro-reflection . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32
4.3 Angle Dependence of Effective Barrier Strength . . . . . . . . . . . . . . . . 36
4.4 Corrections Not Taken into Account . . . . . . . . . . . . . . . . . . . . . . 44
5 Calculation of the Conductance . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47
5.1 Particle with Perpendicular Incidence Angle . . . . . . . . . . . . . . . . . . 47
5.2 Finite Incidence Angle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 56
6 Self-consistent Gap Calculation . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60
6.1 Quasi-classical Self-consistent Gap Calculations . . . . . . . . . . . . . . . . 61
6.2 Improvement on Quasiclassical Approach . . . . . . . . . . . . . . . . . . . . 64
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7 Results and Interpretation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73
7.1 Effects of Finite Gap Onset Length . . . . . . . . . . . . . . . . . . . . . . . 76
7.2 Effects of Mismatch and Anisotropy on Fermi Surface . . . . . . . . . . . . . 82
7.3 Effects of Non-exact Retro-reflection . . . . . . . . . . . . . . . . . . . . . . 83
7.4 Effects of Self-consistence . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
8 Conclusions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86
Appendix
A Quantum Mechanical Ramp Barrier . . . . . . . . . . . . . . . . . . . . . . . . . . 88
A.1 Exact Solution of the Tunneling Problem . . . . . . . . . . . . . . . . . . . . 88
A.2 Numerical Results and Comparison of the Solutions . . . . . . . . . . . . . . 90
B Basic Quasiclassical Equations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 94
C Definition and Calculation of Gap . . . . . . . . . . . . . . . . . . . . . . . . . . . 96
References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 98
Author’s Biography . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 100
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List of Figures
1.1 SN (A) and SIN (B) junction. Dashed regions are occupied states.Grey block
is an interface barrier. Single particle states are not allowed inside the gap. . 3
1.2 Four processes occurring at SN interface: specular reflection (A), Andreev
reflection (B), transmission as an electron (C), transmission as a hole (D).
Arrows point in a direction of the velocity of the particle, and abbreviations
for the directions are: eR - a right moving electron, eL - a left moving electron,
hR - a right moving hole, hL - a left moving hole. Electron trajectories - full
line, hole trajectories - dashed line. . . . . . . . . . . . . . . . . . . . . . . . 6
2.1 Energy spectrum of BdG equations. Four types of particles with the given
energy E are marked by the dots: left moving electron-like (eL), right moving
hole-like (eL), left moving hole-like (hL), right moving electron-like (eR). . . 10
2.2 Visualisation of the BTK problem. The properties of N and SC are uniform,
and there is a δ-function potential at the boundary. . . . . . . . . . . . . . 12
2.3 The BTK conductance normalized to a high voltage value, for values of Z
(top to bottom curve): 0, 0.3, 0.6, 1.0, 2.0. . . . . . . . . . . . . . . . . . . 15
2.4 The BTK conductance normalized to a normal state conductance of a system
without barrier for values of Z (top to bottom curve): 0, 0.3, 0.6, 1.0, 2.0. . 15
2.5 The conductance contributions from the individual components, Z = 0, EF =
1eV , ∆ = 20meV : (upper row) a - transmission without branch crossing, b
- transmission with branch crossing, (lower row) c - Andreev reflection, d -
specular reflection. The coefficient b and c are zoomed up to a larger scale to
stress that they are exactly zero in BTK. . . . . . . . . . . . . . . . . . . . . 17
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2.6 Contribution to the conductance from the individual components, Z = 2,
EF = 1eV , ∆ = 10meV : (upper row) a - transmission without branch cross-
ing, b - transmission with branch crossing, (lower row) c - Andreev reflection,
d - specular reflection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
2.7 Temperature dependence of s-wave BCS gap, and the smearing factor ∂f/∂V . 19
2.8 Temperature dependence of the BTK conductance given for Z=0 (left) and
Z=0.5 (right). Curves from the bottom correspond to T=0, 0.2Tc, 0.4Tc,
0.6Tc, 0.8 Tc, Tc. Each curve is offset by +1 from the previous one. We use
µ = 1eV , ∆ = 10meV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
2.9 The plots of a zero bias conductance as a function of temperature, normalized
to a high voltage value, for different values of Z - from top: Z=0, 0.3, 0.6, 0.9,
1.2, 1.5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
3.1 SN junction with a displaced barrier. Three processes represent possible tra-
jectories after AR at the SC interface. The barrier position is a vertical line
with T,R, interface is at the gap onset. . . . . . . . . . . . . . . . . . . . . . 24
4.1 Point contact conductance between Au and c-axis of CeCoIn5, from [14]. . . 29
4.2 A comparison of the BTK conductance (full line) to the similar calculation
with gap onset length ξ, and µ = 1eV , ∆ = 10meV , Z = 0 (left) and
Z = 0.367 (right). Note that y-axis doesn’t start at zero. . . . . . . . . . . . 31
4.3 Andreev reflection for a particle above Fermi surface. . . . . . . . . . . . . . 33
4.4 Particles on the outside of the space limited with lines AB and CD cannot
AR (momenta k1 and k2). Particle k3 is allowed to AR. Left hand side is a
case kFSC > kFN , right side kFSC < kFN . . . . . . . . . . . . . . . . . . . . . 34
4.5 The effect of limited tunneling due to the non-exact retro-reflection in a system
with µ = 1eV , ∆ = 10meV , T = Tc/2 = 33K in a dirty limit (lower curve)
compared to the finite temperature BTK calculation (upper curve). . . . . . 35
4.6 Limit on retro-reflection as given by (4.4) - kmax =√
2kF . . . . . . . . . . . 36
4.7 A contact of two metals with different Fermi wavevectors. Tunneling to (and
from) regions above the line AB and below CD is forbidden. Note that k‖ is
conserved. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38
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4.8 Angle dependence of Zeff for Z0 = 0, m1/m2 = 5 and values of EF1/EF2, from
the bottom curve: 2, 1, 1/2, 1/5, 1/8, 1/10. . . . . . . . . . . . . . . . . . . 39
4.9 Zeff as a function of incident angle, for a system with m1/m2 = (1 + 4 cos θ)
and ratio EF1/EF2 (from the left): 20, 10, 5, 3, 2.5, 2. . . . . . . . . . . . . . . 41
4.10 Zeff as a function of incident angle, for a system with m1/m2 = (1 + 4 cos θ)
and ratio EF1/EF2 (from the left): 2, 1, 1/2, 1/5, 1/10, 1/20. . . . . . . . . . . 42
4.11 Effect of the proper inclusion of the angle dependent Z, for a system with Z0
= 0.1, rk = 2/3. Dots: calculation with correction taken into account; full
line - BTK calculated with corresponding Zeff = 0.367. . . . . . . . . . . . . 43
5.1 Schematics of approximation of a real potential by a piecewise constant model
potential. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48
5.2 One segment with corresponding particle amplitudes. . . . . . . . . . . . . . 50
5.3 Components of the conductance for a system with step-function gap and exact
momenta retained throughout the calculation, with Z = 0, µ = 1eV , ∆ =
0.2eV (upper row): a-transmission without branch crossing, b - transmission
with branch crossing, (lower row) c - Andreev reflection, d- specular reflection.
Note a different scale in parts c and d. Compare with Fig.2.5 to see an effect of
exact momenta. Vertical axes - current, normalized to the incoming particle;
horizontal axes - energy, in units 0.1meV . . . . . . . . . . . . . . . . . . . . 54
5.4 Distribution of the current in space for each component eR, eL (upper row),
hR, hL (lower row), normalized to the incoming eR current. Z = 0.7, µ = 1eV ,
∆ = 0.1eV . An electron is incoming from the right, position of the barrier is
at the mark 50. Length ξ is 10 divisions on x axis. . . . . . . . . . . . . . . . 55
5.5 Schematics of the change of incident angle for a sequence of segments, due to
the increase of gap at the barrier, as calculated in (4.12) . . . . . . . . . . . 58
6.1 Boundary conditions for a SN contact: an electron incoming from the left (A)
and a hole outgoing to the right (B). Full line - electron, dotted line - hole.
Arrows point in the direction of propagation. N metal is on the left side of
the interface in both figures. . . . . . . . . . . . . . . . . . . . . . . . . . . . 65
x
6.2 Processes (A) and (B) from the Fig.6.1 drawn to include AR along the tra-
jectory (left). Contributions to the gap from two trajectories at every point
in space (right). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
6.3 The unnormalized contribution to the pair correlation function (6.5) from the
particles of one energy and along one incident angle for Nb, Z=0, T=0 (E ≈ ∆
(left), E ≈ 3∆ (right)). Units on x-axis are 1/10ξ, and contact is at the mark
100, N is to the left, SC to the right of it. . . . . . . . . . . . . . . . . . . . . 69
6.4 The unnormalized contribution to the pair correlation function from particles
at an incident angle θ = 0 (left) and integrated over all angles (i.e. after
complete first iteration) for Nb, Z=0 (E ≈ ∆ (left), E ≈ 3∆ (right). Units
on x-axis are 1/10ξ, and contact is at the mark 100. . . . . . . . . . . . . . . 70
6.5 The calculated gap in each iteration (top to bottom) (right) and the unnor-
malized pair correlation function after three iteration loops (left) for Nb, Z=0
. Units on x-axis are 1/10ξ, and contact is at the mark 100. . . . . . . . . . 70
6.6 Self-consistent gap and normalized pair correlation function for T = 0.95Tc,
all parameters are the same as in other figures. . . . . . . . . . . . . . . . . . 71
6.7 Self-consistent gap and normalized pair correlation function for barrier para-
meter Z = 4.0, T = 0, all parameters the same as in other figures. . . . . . . 71
6.8 Self consistent gap after 4 iterations for EF = 1eV and ∆ = 0.1eV (left) and
∆ = 0.2eV (right) at T=0, Z=0. . . . . . . . . . . . . . . . . . . . . . . . . . 72
7.1 Evolution of the conductance curve formSC/mN = (1+4 cos θ) and EFSC/EFN
1/5, 1/2 (upper row), 2, 3 (lower row). EF = 1eV , ∆ = 10meV , Z0 = 0. Full
line is BTK curve, fitted to the high energy values, dotted line is this cal-
culation. Vertical axis is a conductance, normalized to a perfect contact,
horizontal - energy, in units 1/100∆. . . . . . . . . . . . . . . . . . . . . . . 74
7.2 A conductance curve for mSC/mN = (1+4 cos θ) and EFSC/EFN - 2 (left)and
3 (right) . Z0 = 0, EF = 1eV , ∆ = 100meV (upper row) and ∆ = 200meV
(lower row). Full line is BTK curve, fitted to the high energy values, dotted
line is this calculation. Vertical axis is a conductance, normalized to the
perfect contact, horizontal - energy, in units 1/100∆. . . . . . . . . . . . . . 75
xi
7.3 A comparison of the self-consistent calculation of the gap for a system with
mSC/mN = (1 + 4 cos θ) and EFSC/EFN - 0.2 (dots) and 3 (full line), after
four iterations. Vertical axis is gap in eV , horizontal is distance in units 1/10ξ
- contact at 50. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75
7.4 Evolution of the subgap structure with incident angle, Z=1.3, Ef = 1eV , ∆ =
1meV : full line - BTK, dots - this calculation, normalized so that conductance
at high voltage without barrier is σ0 = 1. Consequence of this normalization
is that subgap conductance σSN(E) = 2 means that particle at that energy
does not feel the presence of the barrier. . . . . . . . . . . . . . . . . . . . . 77
7.5 The schematics of the model of slowly varying gap. N - normal side, SC -
superconducting side (with gap ∆). Region R is either superconducting (with
gap ∆ < ∆SC), or normal (∆ = 0). . . . . . . . . . . . . . . . . . . . . . . . 78
7.6 The schematics of the condition (7.6): (A) - side view (distance vs. energy),
(B) - view from the above. A thick vertical line is a surface barrier, a thin
line is the position where Andreev reflection occurs . . . . . . . . . . . . . . 81
7.7 Conductance at very large incident angle θ > 88o, Z = 1.3, Ef = 1eV ,
∆ = 1meV . Full lines are BTK formula. Dots are calculation without (left)
and with (right) k = kf approximation. The normalization is the same as
above. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 82
A.1 Ramp potential in standard quantum-mechanical problem. We set V0 = 0.01eV . 89
A.2 The reflection coefficient of a ramp potential for U = 0.01eV , and values of
L = 0, 10, 20, 40, 80, 160, 320, 640A (descending curves). . . . . . . . . . . . . 90
A.3 A numerical approximation to the real potential form Fig. A.1 (steps), and
the ramp potential (straight line), for n = 10 steps. . . . . . . . . . . . . . . 91
A.4 Fitting the conductance on the energy scale of a gap. Full line - the exact solu-
tion of the ramp potential problem, dots - the numerical solution. U=0.01eV,
L=10A (upper curve) and L=320A (lower curve) . . . . . . . . . . . . . . . 92
A.5 Fitting the conductance on a very small scale - energy axis is offset so that
gap energy is at zero. Note that R-axis shows details smaller than Fig. A.4.
Full line - the exact solution, dots - the numerical solution. U=0.01eV, L=320A 93
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Chapter 1
Introduction
Transport phenomena in a point contact junction between superconductor and normal metal
are dominated by Andreev reflection, a process that transforms an electron into a hole that
retraces the path of an incoming particle. Theoretical description of the conductance of this
system is given by Blonder, Tinkham and Klapwijk, in a theory that is usually referred to as
BTK. Their approach is very simple, requires a single fitting parameter, yet it is extremely
successful. There are many corrections to this equation, but they usually do not produce
significant departures from BTK, and are therefore neglected.
In cases when BTK description is not satisfactory, one may try adding additonal fitting
parameters, such as quasiparticle lifetime. Addition of an extra fitting parameter adds new
fitting curves to the BTK family, but it is not always physically justified. One would natu-
rally like to avoid addition of a new free variable to the data fit.
There is a class of corrections to BTK that does not introduce a new physical effect to the
problem. One can study the physics already there with a higher accuracy. These corrections
do not introduce a new fitting parameter, but they do change family of functions described
by it. In essence, they provide a better fitting functions than BTK for same problem. The
purpose of this work is study of such one-parameter corrections.
The basic problem is that we know of several corrections to BTK of the order ∆/EF ,
and none of them has significant effect...but how do they act together? Do they add inde-
pendently, do they mutually enhance, or suppress? In particular, for a system with ∆/EF
1
of the order several percent, can these corrections add to produce a result of the order 1? To
answer, we will have to treat all corrections on the same level from the beginning and account
for them self-consistently. The answer turns out not to be spectacular - the corrections tend
to cancel each other out, but we can answer how does it happen, and the reasons for it are
interesting. To some extent, we managed to explain why is the BTK so robust and effective.
The motivation for this topic was real life problems of the experimental groups in Urbana.
Point contact junctions conductance data often look surprisingly similar to BTK, but they
are not exactly the same - and the discrepancy cannot be accounted for easily. Depending
on the geometry of the device, ordinary BTK can be twisted into an unrecognizable form. I
cannot say that I managed to describe said experiments well, but it was a great inspiration
for the work, and a pointer to what type of result is interesting to find.
The outline of the thesis is as follows: in the rest of Chapter 1 we will discuss phenom-
enological aspects of Andreev reflection without a quantitative approach. Chapter 2 is a
review of BTK, which we will use as a standard for comparison of all results. Chapter 3 is
a study of the origin of various aspects of BTK. Chapter 4 is a discussion of the corrections
introduced, and isolated effects of each correction separately. Chapter 5 is a discussion of
the algorithm used to calculate the conductance with a given gap profile. Chapter 6 is a
self-consistent calculation of the gap profile using a similar algorithm. Chapter 7 gives results
for the combination of effects and a discussion of their influence on each other, and Chapter
8 is a brief conclusion.
1.1 Superconductor-Normal Metal Contact Junctions and Andreev
Reflection
Contact between superconductor and normal metal can be in two different regimes - a tunnel-
ing junction (also called SIN junction) and a contact junction (SN junction). The difference
between them stems from the properties of the interface. A clean interface (one with no
potential barrier or impurities), which is considerably harder to make, results in a contact
2
Figure 1.1: SN (A) and SIN (B) junction. Dashed regions are occupiedstates.Grey block is an interface barrier. Single particle states are not allowedinside the gap.
regime - particles ballistically propagate between two metals. Interface with a potential
barrier - an insulating layer (therefore SIN)- produces junction in a tunneling regime. An
insulating barrier is usually consequence of a naturally occuring oxide at a metal surface, but
it can also be artificially produced. In a tunneling junction (Fig.1.1 (B)), normal metal (N)
and superconductor (SC) are largely independent of each other, their wave function overlap
is exponentially small and can be treated as a perturbation in a standard method called the
tunneling Hamiltonian approach [1]. In this regime the internal states of SC and N are to a
large extent unaffected by a system on the other side of a junction (though there are situa-
tions where it can be very important, e.g. [2]), and we usually observe how does the given
state influence a particle tunneling from the other side. We find, e.g., that a particle with
energy E smaller then a SC gap ∆ cannot penetrate the SC side, since there are no available
final states for it. Until we give a particle sitting at the Fermi surface enough energy (as an
electric potential offset V ) to reach the gap, there is no charge transfer between two systems
(in case of s-wave SC), and conductance σ = dI/dV = 0. Only for V > ∆ does transport
occur, and we find that conductance measurements effectively map the density of states of
a SC system.
3
In a contact junction (Fig.1.1 (A)), on the other hand, two systems are in a direct physical
contact, and overlap of the wave functions is large. One cannot apply perturbation theory,
but rather has to match the wave functions and solve the problem of two systems in contact
simultaneously. Influence of two systems on each other is much larger than in the SIN case,
and the state of a system near the contact is significantly different from that of an isolated
sample. The mutual effect of SC and N system in SN junction is called the proximity effect.
To study the transport of SN contact properly, one takes into account not only the influence
of a, say, SC state on a particle incoming from a N side, but also the other way around -
effect of the particles from N on the ground state of SC system. It is this problem that we
shall study in the present work.
The dominant effect in a subgap transport (energies E < ∆) in an SN contact junction
and the main cause of proximity effect is Andreev reflection. Andreev reflection (AR) is a
process in which the incoming electron gets reflected as a hole, nearly retracing the trajectory
of the electron. This type of reflection is also called retroreflection. Opposite conversion,
hole into electron, is also possible, but to be definite we shall discuss electron to hole AR
only. Minor differences between two processes will be addressed later.
AR is a process typical of superconducting state, and most prominent in area around an
SN contact. Its overall effect is the transfer of a pair of electrons from N to SC side. Since
only pairs exist in SC at energies E < ∆ and T = 0, this is the only transfer mechanism in
that energy range. An incoming electron with momentum k and E < ∆ can be transfered
to SC, only if it finds a single electron of the opposite momentum −k and forms a Cooper
pair. Since free electrons are not available in SC at that energy, the pairing electron must
come from the N side, leaving behind a hole with the momentum −k.
This effect was first studied by Andreev [3] in order to explain the anomalous heat con-
duction properties at SN contact. Saint-James [4, 5] was the first to study its influence on
transport of charge in SN junction, independently of Andreev’s work. Sometimes the An-
dreev effect used in this context is called Andreev-Saint-James effect [6].
4
If there is a finite barrier at SN interface, a particle can also get specularly reflected
with E < ∆. The particles with energy E > ∆ can be transmitted as electron- or hole-like
quasiparticles into SC. While details of these processes will be given later in Sec.2.2, we can
now note how these processes change perpendicular (v⊥) and parallel (v‖) components of
the velocity (relative to the interface) for two systems in contact with the identical Fermi
surfaces, the same Fermi energy EF and the same effective mass m. These four processes
exhaust all possibilities. In Fig.1.2 we see that these changes are:
• specular reflection : v⊥ → −v⊥, v‖ → v‖
• Andreev reflection : v⊥ → −v⊥, v‖ → −v‖
• transmission as an electron : v⊥ → v⊥, v‖ → v‖
• transmission as a hole : v⊥ → v⊥, v‖ → −v‖
Process of transmission as a hole might look counterintuitive, but one should bear in mind
that the parallel component of the momentum has to be conserved, and it is conserved in
all four processes listed here - by virtue of the fact that the momentum of a hole is opposite
to its direction of propagation.
While the presence of a gap is crucial for the AR, it should be noted that it works only for
a SC gap. A particle entering the region with semiconducting gap will be only specularly
reflected. The reason for this is in the very nature of a SC state. An electron entering a
semiconductor will have its wave function matched to that of a corresponding state in the
gap - which is just an exponentially decaying electron wave function. The hole wavefunction
does not play a role, since neither N nor semiconducting state mix electrons and holes. The
eigenstates of the SC are the coherent mixtures of electron and hole parts. Thus, an electron
entering a SC will have its wave function matched to a decaying part that has both electron
and hole in it. But, then, the hole part on the SC side has to be matched too, and the only
way to do it is to produce a hole wave function on the N metal side. That is the essence of AR.
The transfer of a pair into the SC by AR has the spectacular consequences for the
low-energy electrical transport properties of an SN contact. If an electron along the given
5
Figure 1.2: Four processes occurring at SN interface: specular reflection (A),Andreev reflection (B), transmission as an electron (C), transmission as a hole(D). Arrows point in a direction of the velocity of the particle, and abbrevia-tions for the directions are: eR - a right moving electron, eL - a left movingelectron, hR - a right moving hole, hL - a left moving hole. Electron trajecto-ries - full line, hole trajectories - dashed line.
6
trajectory is transmitted with the energy E > ∆, it carries a charge e to the other side.
Along the same trajectory an electron with E < ∆ is AR - thus transferring a charge 2e to
a SC. The conductance below the gap is increased by a factor 2! This is in great contrast
to a tunneling junction, where there is no charge transfer at all below the gap. There are
no single particle states available at E < ∆, but the pair states are available. Since AR
is a two-particle tunneling process, it is greatly suppressed in a SIN junction, since it is a
higher-order process compared to single particle tunneling. Note that this is in contrast to
an SIS junction - a pair tunneling in that case is a process of a same order as single par-
ticle tunneling (which is the basis of the Josephson effect). An SIS junction has correlated
systems on both sides of the barrier, and tunneling of one electron in a pair automati-
cally ensures tunneling of the other. It is not so in the SIN case - electrons on the N side
are uncorrelated, and they have to tunnel separately, making it a higher order process. The
barrier plays little role in an SN contact, since by definition it is orders of magnitude smaller.
It is this factor of 2 that plays a central role in the study of SN junctions. The method we
employ is simply shooting the electrons toward the barrier one by one at various angles and
energies, and calculating the probabilities for each of the processes listed above. While below
the gap the matter is simplified by the fact that no transmission is allowed (to the extent
that we can get BTK results without actually performing a microscopic calculation), above
the gap we have to take into account properly the combination of all possible processes. The
resulting solutions for the conductance are drastically different in the two energy ranges.
an If for a certain system every trajectory that is transmitted in an NN junction gets Andreev
reflected in SN contact - the overall conductance will have an increase by a factor 2 after the
SC transition. Our main task will be tracing the trajectories that are not Andreev reflected,
and in particular studying the factors not included in the original BTK that can change the
conditions for Andreev reflection. For that we will need a microscopic theory, which we shall
study in the following section.
7
Chapter 2
The Bogoliubov-De Gennes Equations and the
Blonder-Tinkham-Klapwijk Model
This section reviews briefly the Bogoliubov - DeGennes (BdG) equations, used to describe
a superconducting system near the boundaries and the inhomogeneities, and the theory by
Blonder, Tinkham and Klapwijk (BTK) that uses these equations to describe conductance
of a superconducting-normal metal (SN) contact. We will need only the simplest solution of
the BdG, that for an isotropic system.
2.1 Bogoliubov - DeGennes Equations
The Bogoliubov-De Gennes equations [7] are the mean-field equations for a superconducting
system. They are obtained as the equations of motion for the mean-field approximation
to BCS Hamiltonian. In their final form, they are coupled system of the two second-order
differential equations and the two self-consistence conditions:
Enfn(r, t) =
(− h2
2m
∂2
∂r2− µ(r) + U(r)
)fn(r, t) + ∆(r)gn(r, t)
Engn(r, t) = −(− h2
2m
∂2
∂r2− µ(r) + U(r)
)gn(r, t) + ∆(r)fn(r, t)
∆(r) = V Σnfn(r, t)g∗n(r, t) ∗ (1− 2n(En)) (2.1)
U(r) = ΣnU(r)|fn(r, t)|2 ∗ n(En) + |gn(r, t)|2 ∗ (1− n(En)))
8
where n = (1 + exp(−β(E − µ)) is the Fermi occupation factor, β = 1/kBT na inverse
temperature, µ a chemical potential (which, in principle, can be position dependent), U(r)
a single particle potential calculated in the normal metal, ∆ - BCS gap, and u and v - the
wave functions for an electron and a hole.
As written this system is impossible to solve in the general form. For a homogeneous,
clean system it yields the usual BCS value of the gap and the wavefunctions:
E2 = ∆2 + ε2q
fq = eiEt−qr ∗ u0
gq = eiEt−qr ∗ v0 (2.2)
u20 =
1
2
(1 +
√E2 −∆2
E
)v2
0 =1
2
(1−
√E2 −∆2
E
)BdG equations have the solutions for both positive and negative E, connected by (f, g)T (E) =
(−g∗, f∗)(−E). Since these are not independent, we will always deal with the positive en-
ergy solutions only, and therefore all the sums run over the positive values of energy unless
explicitly stated otherwise. For a given energy E we have four solutions propagating along
the direction r. The momentum q corresponding to these solutions is given by:
q± =
√2mSC
h2
√µ±
√E2 −∆2 (2.3)
The particles and their momenta are given in Fig.2.1. The names electron-like and hole-like
are referring to the corresponding solutions in ∆ → 0 limit, whereas in the SC state they
are really mixture of an electron and a hole component - a property explicitly captured in
the spinor representation (an electron component in the first row, a hole in second):
ψeR =
u0
v0
eiq+r;ψeL =
u0
v0
e−iq+r (2.4)
ψhR =
v0
u0
e−iq−r;ψhL =
v0
u0
eiq−r
Later, we will be interested in solving (2.1) in a more complicated case.
9
Figure 2.1: Energy spectrum of BdG equations. Four types of particles withthe given energy E are marked by the dots: left moving electron-like (eL),right moving hole-like (eL), left moving hole-like (hL), right moving electron-like (eR).
2.2 The Model of Blonder, Tinkham and Klapwijk
Blonder, Tinkham and Klapwijk [8, 9, 10] used the BdG equations to describe the nature of
the excess current observed in some SN contact junctions. The idea that this is caused by the
Andreev reflection has been around for a while [11], but BTK put it in its most useful and
most often quoted form. A geometry of the problem is simple. BTK models a SC-N interface
as a flat surface with a normal metal (N) on one (say, left) side, and a superconductor (SC)
on the other. The SC side is characterized by the mass mSC , the Fermi energy EFSC and the
order parameter ∆. The order parameter is assumed to be constant everywhere on the SC
side, up to the interface. The N side is characterized by the mass mN and the Fermi energy
EFN . Fermi energy is measured from the bottom of the conduction band. Both sides have
perfectly quadratic dispersion relations, and no band effects beyond the effective mass; they
are treated as free electrons, apart from the SC gap. The interface potential is modeled by
a delta-function potential H. The particles are moving in the direction perpendicular to the
contact, which is chosen as a z-axis.
10
They then consider an incoming particle from the N side. Upon incidence on the in-
terface, it undergoes the reflection (either as a particle or a hole) or the transmission (also
as a particle or a hole). The transmission is such that it does conserve the current, thus a
right-going particle on the N side will produce only a right going particles on the SC side.
We solve the BdG equations (2.1) separately on the SC and the N side, with the appropri-
ate parameters on each side and match the boundary conditions. Bogoliubov quasiparticles
on the SC side have weight u0 in the particle channel and v0 in the hole channel, while
particles on the N side have only one component (either particle or hole). The definition of
the particle momenta in the problem is:
k+ =
√2mN
h2
√EFN + E
k− =
√2mN
h2
√EFN − E
q+ =
√2mSC
h2
√EFSC +
√E2 −∆2 (2.5)
q− =
√2mSC
h2
√EFSC −
√E2 −∆2
where k+ is momentum of an electron on the N side, k− momentum of a hole on the
N side, q+ momentum of an electron-like quasiparticle on the SC side, and q− momentum
of a hole-like quasiparticle on the SC side. We solve the BdG equations separately in two
regions, and match the boundary conditions (see Fig.2.2): 1
0
eik+z0 + C
1
0
e−ik+z0 +D
0
1
eik−z0 = A
u0
v0
eiq+z0 +B
v0
u0
e−iq−z0
(2.6)
where on the left hand side (LHS) we have an incoming particle with the amplitude 1 (and
thus the probability equal to 1), and a reflected electron and a hole with the probabilities
C and D, both moving toward the left. On the right hand side (RHS) we have an outgoing
electron- and a hole-like quasiparticles with the amplitudes A and B, both moving to the
11
Figure 2.2: Visualisation of the BTK problem. The properties of N and SCare uniform, and there is a δ-function potential at the boundary.
right. For the derivatives, we have:
h2
2mN
ik+
1
0
eik+z0 − ik+C
1
0
e−ik+z0 + ik−D
0
1
eik−z0
= (2.7)
h2
2mSC
iq+A
u0
v0
eiq+z0 − iq−B
v0
u0
e−iq−z0
+
H ∗
A
u0
v0
eiq+z0 + B
v0
u0
e−iq−z0
where z0 is the position of the barrier, in the original problem z0 = 0, but this more general
form will be useful for the comparison with the later results.
The system (2.6), (2.7) is a system of four equations with four unknown variables - A,
B, C, D. Their physical meaning is that they are the amplitudes for:
• - a right going electron-like quasiparticle on the SC side: the amplitude for the trans-
mission without branch crossing (A)
• - a right going hole-like quasiparticle on the SC side: the amplitude for the transmission
with branch crossing (B).
12
• - a left going electron on the N side: the amplitude for the specular reflection (C)
• - a left going hole on the N side: the amplitude for the Andreev reflection (AR) (D)
’Branch crossing’ is the name we use for a tunneling process where the particle crosses
from an electron-like to a hole-like branch of the energy spectrum. In that sense the An-
dreev reflection is also a branch crossing process, but we shall exclusively use that name for
a transmitted particle.
The major simplification that BTK use to solve the system (2.6, 2.7) is setting k+ =
k− = kFN and q+ = q− = qFSC (though we will write these terms explicitely in the formulas
(2.10 - 2.14), in order to facilitate comparison with the corrections of the following chapters).
This induces the error of the order δk/kF =√E2 −∆2/2EF , thus of the order ∆/EF . Using
vSCF = hkFSC/mSC and vFN = hkFN/mN , we define Z0 = H/h
√vFN ∗ vFSC , and
Z2 ≡ Z2 = Z20 + (1− rv)
2/4rv
rv = vFN/vFSC =
√EFNmSC
EFSCmN
(2.8)
By using Z instead of Z0, we can set EFN = EFSC and mN = mSC . If the contact is
perfect (H = Z0 = 0) the effect of difference of the masses mSC and mN and the Fermi
energies EFSC and EFN is absorbed into the renormalized barrier strength Zeff through a
single parameter rv. Note that Zeff is insensitive to the exchange mSC ↔ mN , so it retains
the properties of a real barrier. To get the actual transmission coefficients for every branch
we have to take into account the difference in momenta and weight of a hole and a particle
part of the wavefunction. Thus we get:
a =(|A|2 ∗
(u2
0 − v20
)) q+SC
k+N
b = |B|2 ∗(u2
0 − v20
) q−SC
k+N
(2.9)
c = |C|2 d = |D|2 ∗ k−N
k+N
The solution of the system (2.6, 2.7) is very different in two regions E < ∆ and E > ∆,
13
as expected:
a(E) =
0 ; E < ∆
(u20−v2
0)u20(1+Z2)
γ2 ; E ≥ ∆b(E) =
0 ; E < ∆
(u20−v2
0)v20Z2
γ2 ; E ≥ ∆(2.10)
c(E) =
1− d = 4Z2(1+Z2)(∆2−E2)E2+(∆2−E2)(1+2Z2)2
; E < ∆
(u20−v2
0)Z2(1+Z2)
γ2 ; E ≥ ∆d(E) =
∆2
E2+(∆2−E2)(1+2Z2)2; E < ∆
u20v2
0
γ2 ; E ≥ ∆
where we defined γ = u20 + (u2
0 − v20)Z
2.
Knowing A, B, C and D, we can calculate the differential conductance of SC-N junction as:
σSC−N(E) = 2∗|D|2∗ k−N
k+N
+(|A|2∗(u20−v2
0))q+SC
k+N
+|B|2∗(u20−v2
0))q−SC
k+N
= 2∗d(E)+a(E)+b(E)
(2.11)
Since the total current through the junction has to be conserved (and equal to the current
carried by the incoming particle), the following condition is satisfied:
|C|2 + |D|2 ∗ k−N
k+N
+ (|A|2 ∗ (u20 − v2
0))q+SC
k+N
+ |B|2 ∗ (u20 − v2
0))q−SC
k+N
= a+ b+ c+ d = 1 (2.12)
and we have the alternative expression for the conductance:
σSC−N(E) = 1 + |D|2 ∗ k−N
k+N
− |C|2 = 1 + d(E)− c(E) (2.13)
To get these formulas normalized to the high-voltage value (i.e. to the normal state
conductance σN−N), we need to divide them by the same formulas in the limit E →∞. It’s
not hard to see that the normalization coefficient is just (1 + Z2).
The essence of these formulas is following: as we increase the voltage between two sys-
tems by an infinitesimal amount δV , a new particle at the energy E = µ+ V + δV becomes
available for the tunneling. It carries a charge and participates in the total current. The
differential conductance σ = dI/dV is equal to the current carried by that particle. In an
NN junction we get σN(V ), which is constant on the energy scale we are interested in (of
the order ∆). In the superconducting state a particle can undergo the Andreev reflection,
which effectively carries over 2 electrons to a SC. If a particle with energy E gets completely
AR, we get σSC(E)/σN = 2. If it has a finite chance of specular reflection off the barrier, we
have σSC(E)/σN < 2.
14
Figure 2.3: The BTK conductance normalized to a high voltage value, forvalues of Z (top to bottom curve): 0, 0.3, 0.6, 1.0, 2.0.
Figure 2.4: The BTK conductance normalized to a normal state conductanceof a system without barrier for values of Z (top to bottom curve): 0, 0.3, 0.6,1.0, 2.0.
15
This is an one-dimensional problem, but the same rationale applies to a three dimen-
sional system. In that case for every given energy there will be number of particles hitting
the barrier at various angles. In three dimension the ratio σSN/σNN = 2 means that every
single trajectory that was transmitted in a normal state, got reflected in an SN junction.
Saying that certain effect reduces the SN conductance, means that some of the trajectories
are disallowed to undergo AR.
The plots of the conductance are shown in Fig.2.3 for several values of Z. The curves
are normalized to a conductance at a high value of voltage, equivalent to a normal state
conductance σN = σSC(V ∆). The figure 2.4 has different normalization: the curves
are normalized to a conductance of system without a barrier. This normalization has a
nice property that the value σ(E) = 2 means that a particle incoming with energy E is not
affected by a presence of the barrier. Two normalizations are different by the factor (1+Z2).
The contributions to a total conductance from the individual components is given in
Fig.2.5 for Z = 0, and in Fig.2.6 for the case Z = 2.0. We see several interesting features. In
the BTK problem there is no specular reflection and no branch crossing transmission for the
system with the clean contact (Z = 0) (Fig.2.5 b, c)). The branch crossing processes have
a very small probability, negligible everywhere except at the energies E → ∆+ (Fig.2.6, c).
For a system with a strong barrier specular reflection dominates everywhere except close to
the gap, where the AR peak occurs.
To get the current we simply integrate the conductance:
INS =1
R0
∫(1 + d(E)− c(E))dE (2.14)
and at a finite temperature we get:
INS =1
R0
∫(1 + d(E)− c(E)) (f(E − V )− f(E)) dE (2.15)
Where R0 is given by the normal state resistivity, and is as such a fitting parameter. However,
this expression will not be used extensively. Often defined quantity is the excess current
Iexc = (INS − INN)|E∆.
16
Figure 2.5: The conductance contributions from the individual components,Z = 0, EF = 1eV , ∆ = 20meV : (upper row) a - transmission withoutbranch crossing, b - transmission with branch crossing, (lower row) c - Andreevreflection, d - specular reflection. The coefficient b and c are zoomed up to alarger scale to stress that they are exactly zero in BTK.
17
Figure 2.6: Contribution to the conductance from the individual components,Z = 2, EF = 1eV , ∆ = 10meV : (upper row) a - transmission withoutbranch crossing, b - transmission with branch crossing, (lower row) c - Andreevreflection, d - specular reflection.
18
Figure 2.7: Temperature dependence of s-wave BCS gap, and the smearingfactor ∂f/∂V .
Finally, by differentiating 2.15 we get the finite temperature conductance as (using ∂f∂E
=
∂f∂V
):
σSC−N
σN−N
=
∫ ∞
−∞(1 + d(E)− c(E))
(− ∂f∂E
∣∣∣∣E−eV
)dE =
∫ ∞
−∞σ(E)
(− ∂f∂E
∣∣∣∣E−eV
)(2.16)
Clearly,∫ −∞
+∞∂f∂EdE = 1. In practice the limits of integration in (2.16) are ±20T .
There are two effects of the finite temperature - smearing the features by mixing the con-
tributions from different momenta with weight ∂f/∂E, and change of a gap magnitude with
temperature, given by the gap self-consistency equation (2.1) (we assume all features of SC
are of the BCS kind). Fig.2.7 illustrates these two factors. The results of calculation (2.16)
are given in Fig.2.8. We see that finite temperature smears the sharp features prominent at
T = 0. For that reason we shall restrict ourselves mostly to a study of the case T = 0, where
any new features should be clearly visible.
For a study of finite temperature effects, more useful plot is one of the zero-bias con-
ductance as a function of temperature. We simply perform calculation (2.16) for V = 0
over a relevant range of temperatures. The results are given in Fig.2.9. Again, same factors
as above determine the shape of these curves. System with different Z produce strikingly
diverse plots, and this plot is most convenient way to determine Zeff for the contact junction.
19
Figure 2.8: Temperature dependence of the BTK conductance given for Z=0(left) and Z=0.5 (right). Curves from the bottom correspond to T=0, 0.2Tc,0.4Tc, 0.6Tc, 0.8 Tc, Tc. Each curve is offset by +1 from the previous one.We use µ = 1eV , ∆ = 10meV .
Figure 2.9: The plots of a zero bias conductance as a function of temperature,normalized to a high voltage value, for different values of Z - from top: Z=0,0.3, 0.6, 0.9, 1.2, 1.5.
20
Chapter 3
The Nature of Gap Edge Conductance Peak,
Subgap Conductance and Zero-Bias Properties
An obvious question to ask is why is there a conductance maximum at the gap edge? One
is tempted to argue that it is a density of states effect, as in the tunneling Hamiltonian
calculations. But BTK is explicitly an one particle calculation, and there is no density of
states factor appearing anywhere in the formulas. While there is no doubt that the origin of
the effect in BTK and tunneling calculation is the same (by the fact that BTK with large
Z reproduces the tunneling formalism calculations result of SIN junction [8]), a question re-
mains how does it appear in the BTK framework. The answer, as we will now see, is related
to the other properties of the subgap conductance in BTK, and in particular to the apparent
paradox of suppression of the normalized gap conductance for a finite barrier strength.
The nature of this paradox is following. In a BTK-type SN system without the barrier
every electron with E < ∆ is Andreev reflected. Since that process transfers two elec-
trons from N to SC, the normalized conductance for that (and every other) trajectory is
σSS/σSN = 2.
In an NN junction with a barrier, let’s say that the fraction T of all electrons gets
transmitted, and the fraction R reflected (since we shall study only the zero temperature
case, we can use this notation without the possibilily of confusion). T and R are reflection
21
and transmission coefficients, and T +R = 1. In terms of the BTK parameter Z, they are:
R =Z2
1 + Z2;T =
1
1 + Z2(3.1)
The reflected particles do not participate in the conductance, and we are really interested
only in probability of an electron going through the barrier. We have σnn ∝ PNN(eR →
eR) ∝ T .
Since the SC transition does not change the barrier properties, one would naively expect
that in SN junction, exactly the same fraction R of electrons gets reflected, and since for
E < ∆ there is no transmission, the fraction T gets AR. Each of the AR electrons con-
tributes two times the amount of charge transfer compared to the NN case, so we expect
that σSN ∝ 2T , and the normalized conductance is σSN/σNN = 2, regardless of the barrier
strength.
It is not so. Normalized subgap conductance decreases with the increasing barrier
strength, as we can see in Figs. 2.3, 2.4 and 2.8.
The microscopic BTK calculation doesn’t give us much insight into why this happens.
The reason for this, and the nature of the gap edge peak will be demonstrated more clearly in
somewhat unphysical situation presented below. BTK is a special case of this, more general,
argument.
But first we have to observe ∆φ - the change of a phase of a hole wavefunction compared
to that of an incident electron after AR. To isolate this effect let us study a particle with
energy E < ∆, and let us observe penetration of a wave function inside the gapped region
at z = 0 (so that we have no accumulation of phase difference due to the distance traveled).
Then the wave functions at this point are:
ψeR(z = 0−) = e−i∆φ/2
1
0
;ψhL(z = 0−) = ei∆φ/2
0
1
;ψeR(z = 0+) =
ui
vi
(3.2)
Here we explicitly write the amplitudes as complex numbers of the norm 1, since we already
know that under these conditions an electron is completely converted into a hole. Here ui
22
and vi are given by (2.2). On the SC side, for E < ∆, ui ad vi are complex conjugates, and
we included that into the ansatz of the phase of wave function (though that ansatz is in no
way crucial for the final result). To calculate the difference of phases of ψeR(z = 0−) and
ψhL(z = 0−) we seek the difference of phases of an electron and a hole component of the
wave function. We get:
∆φ = arg(ui)− arg(vi) = arg (ui/vi) = arg(E/∆ + i√
∆2 − E2/∆) ⇒
∆φ = arccos(E/∆) (3.3)
We see that AR itself creates the initial phase difference between an electron and a hole. At
E = 0 that phase difference is π/2, and at E = ∆ it is zero. For AR of the particles above
the gap there is no phase change. For the transfer of the incoming hole into the outgoing
electron, the same result is still valid. This is because the matching function on a SC side is
(v, u)T , so the argument is exactly the same.
Going back to a SN system with the barrier, let us displace the barrier from the SN
interface by a distance d, so that we have situation given in Fig.3.1.
For an electron incident from the N side the following processes can occur:
• specular reflection back to N at the barrier - probability 1− T
• Fig.3.1, P1: transmission at barrier (probability T ), AR, transmission (T ) - total
probability for the process T 2
• Fig.3.1, P2: transmission at barrier (T ), AR, specular reflection at the barrier (1−T ),
AR, transmission (T ) - total probability T 2 ∗ (1− T )
• Fig.3.1, P3: transmission (T ), AR, specular reflection (1− T ), AR, specular reflection
(1− T ), AR, transmission (1− T ) - total probability T 2 ∗ (1− T )2
• process with N + 1 AR - probability T 2 ∗ (1− T )N .
Processes with the odd number of ARs, result in transfer of a hole back to the N side,
and are thus akin to a simple AR (total charge transfer 2e). Processes with the even number
of AR, result in transfer of an electron back to the N, and have an overall effect of specular
23
Figure 3.1: SN junction with a displaced barrier. Three processes representpossible trajectories after AR at the SC interface. The barrier position is avertical line with T,R, interface is at the gap onset.
reflection. It is only processes that of the former kind that contribute the conductance.
Thus, of T electrons that get through the barrier, not all of them are reflected back as holes!
Obviously, the conductance will not have zero voltage value equal to 2, as naively expected.
We shall be able to quantify this result.
Just for a purpose of making the intention clear, let us observe what would the result be
if these processes could be considered separately. Then for probability that incident electron
resulted in outgoing hole we would have:
Pincorrect(eR → hL) = T 2 + T 2(1− T )2 + T 2(1− T )4 · · ·
T 2∑∞
n=0(1− T )2n = T 2/(1− (1− T )2) = T/(2− T ) (3.4)
This is not the right thing to do, since wave functions of the outgoing holes should be added
first, and then squared - i.e. in the process of reflection we should be operating with the
wave function amplitudes, not with the probabilities. Recalling that in simple scattering
model with same masses on two sides of the barrier reflection and transmission coefficients
are given by the squares of the amplitude of reflected and transmitted wave, we define
24
r =√R exp(i∆φ) and t =
√T , and with prescription R→ r and T → t we apply the same
recipe for the amplitudes. Factor exp(i∆φ) in definition of r is taking care of change of phase
upon the Andreev reflection. Then we have the amplitude A of an electron resulting in a
backtracing hole, as:
A(eR → hL) = t ∗ t+ t ∗ (r)2 ∗ t+ t ∗ (r)4 ∗ t+ t ∗ (r)6 ∗ t+ · · ·
= t2∑∞
n=0(r)2n = t2/(1− r2) (3.5)
To find the probability we square A, and get:
P (eR → hL) = |A|2 =∣∣t2/(1− r2)
∣∣2 = T 2/∣∣1− e2i∆φR
∣∣2 (3.6)
Where we used property of complex numbers |z−1| = |z|−1. For a particle at E = 0 the
phase change is ∆φ = π/2 and therefore:
P (eR → hL) = T 2/(2− T )2 = 1/(1 + 2Z2)2 (3.7)
and for the normalized conductance we have:
σSN
σNN
= 2 ∗ PSN(eR → hL)/PNN(eR → eR) = 2T/(2− T )2 (3.8)
or in terms of BTK constant Z:
σSN
σNN
= 2 ∗ (1 + Z2)/(1 + 2Z2)2 (3.9)
which is smaller then 2 for a finite Z. Thus for a displaced barrier the SN conductance is
indeed smaller than the clean contact value 2, provided this result is valid in limit d→ 0 (see
below). The reason is that not only the incoming electrons, but also the outgoing holes can
get specularly reflected off the barrier potential. Visualising this effect in the limit d → 0
is much harder, and not accounting for it was a mistake which led us to the naive conclu-
sion that normalized conductance does not depend on presence of the potential. Note that
formulas (3.7) and (3.9) give exactly the same value for conductance as (2.10) and (2.11) in
the limit E → 0, where normalization to the normal state conductance produces the factor
(1+Z2) . One can now plug in various values of Z in (3.9), and make sure that we are really
getting ZB conductance values from figures 2.3 and 2.8.
25
This procedure does not depend on the displacement distance d, as long as the wave func-
tions of an electron and a hole are of the same wave length, so that their scattering properties
in the region of size d change in the same way (so that T is same for both particles). Thus,
for a realistic system it is, strictly speaking, valid only for the particles at Fermi energy.
Zero voltage bias (ZB) conductance at zero temperature is the quantity determined by such
particles only. The resulting formula (3.9) is exact for dependence of ZB SN conductance on
barrier strength.
However, in the framework of BTK it has even wider range of validity, since that proce-
dure sets k+ = k− = kF , and therefore there is no phase accumulation even for the non-zero
energy particles. Let us now consider the equation (3.6) in the limit E → ∆. In this case
the phase change is ∆φ = 0 and we get:
P (eR → hL) = T 2/(1−R)2 = 1 (3.10)
and for normalized conductance at E = ∆ we get:
σSN
σNN
= 2/T = 2(1 + Z2) (3.11)
which is exactly the result we have already seen in Fig.2.4 - conductance at the gap
edge reaches value 2 regardless of the barrier strength, or alternatively, renormalized by a
factor (1 + Z2) we get values from Fig.2.3. We can now see that the gap edge conductance
maximum occurs because of the interference of the exponentially decaying wave functions of
AR holes and electrons in the region of SC to near the barrier.
After considering two special cases, let us now try to see what can we get for the arbitrary
subgap energy E < ∆. We start from Eq.3.6, and get (using expressions for R and T in
terms of Z):
P (eR → hL) = T 2/∣∣1− e2i∆φR
∣∣2 = T 2/ |(1−R) cos 2∆φ− iR sin 2∆φ|2 =
=((1 + Z2 − Z2 cos 2∆φ)2 + Z4 sin2 2∆φ
)−1(3.12)
Now we substitute cos ∆φ = E/∆ ⇒ cos 2∆φ = 2E2/∆2−1, and after some basic algebra
we get:
P (eR → hL) =∆2
E2 + (∆2 − E2)(1 + 2Z2)2(3.13)
26
which is exactly the same expression as that for the probability of AR in equation (2.10)!
We were, thus, able to derive the complete BTK for energies E < ∆ without microscopic
considerations in terms of wave-functions. The only parameter that we used is a phase shift
upon AR for the particle of given ratio E/∆. We therefore conclude that it is that shift that
completely determines subgap conductance in BTK approximation by controlling interfer-
ence of multiple components of Andreev reflected hole wave functions.
Beenakker has shown using similar method in more general and abstract terms that for-
mula similar to the equation (3.7) is valid for ZB conductance of a multichannel SN contact
with impurities [13]. While the results of this section are not novel, the application of this
method to the finite energies and in particular to BTK is. We have been able to point out
exactly what part of BTK is causing the subgap behavior of the BTK conductance.
As explicitly stated, this solution is valid in d→ 0 limit only if there is no phase difference
accumulation between electron and hole along the path. While beyond BTK (k+, k− 6= kF )
it still remains valid for zero temperature ZB conductance, conclusion related to the finite
energies are not. In particular, conclusion that conductance peak has to occur at E = ∆ is
not valid, and as we’ll see later, the peak indeed occurs at different energies.
27
Chapter 4
Corrections to the BTK Conductance
Since the assumptions of BTK are very restrictive, one would expect that various corrections
make it of little practical use. Every restrictive assumption is supplemented by a correspond-
ing correction. BTK is, however, surprisingly robust, and despite obvious deficiencies is still
most useful tool for a description of NS contact. We will now isolate several corrections, in
particular those that are completely determined by the geometry of a problem and do not
induce additional fitting parameters. Later on, we’ll see how these corrections influence each
other, and how they enter the self-consistent calculation.
A motivation for this study was the experiment by Wan Kyu Park and Laura Greene,
on CeCoIn5 in point contact with Au[14]. Their conductance measurements do show many
trends of BTK, but are often off by a large numerical factor. E.g. normalized conductance
reaches only 1.13, but there are no ’coherence peaks’ at E = ∆ (Fig.4.1). CeCoIn5 is a heavy-
fermion superconductor, with ratio ∆/EF of the order several percents. This compound is
very anisotropic, with ratio of the effective masses mz/ma ≈ 80, and as such a perfect choice
for a system where large angle tunneling effects dominate the transport in contact - an effect
that leads to the strange features that will be discussed later. As we will see later, large
part of the renormalization of mass in CeCoIn5 is irrelevant for the tunneling experiments,
and we will use smaller numbers. General belief is that this compound is d− wave SC, but
we will use s-wave model, with an aim to isolate the effects of ’one-parameter’ corrections
only. Once we have developed the method, it is easy to extend to any symmetry of the order
28
Figure 4.1: Point contact conductance between Au and c-axis of CeCoIn5,from [14].
parameter.
Corrections studied here are contained in the starting formulation of the BTK problem,
and then neglected as being small (of the order ∆/EF ). They are:(i) taking into account
the exact momenta of the particles (ii) a finite gap onset length - at the SN contact gap
is not a step function, it falls off on a length scale ξ; (iii) non-exact retro-reflection: BTK
assumes that an electron and AR hole travel along the same trajectory, which is true only
for particles with energy E = 0 and (iv) angle and energy dependence of the effective barrier
strength - an effect that makes the solid angle integration non-trivial, and especially so for
a problem with non-isotropic Fermi surface.
A very important feature of a correction is its discrimination against Andreev processes.
A correction that has same influence on both SC and N state will not affect the normalized
SN characteristic. Normalization is basically counting how many electron trajectories that
are transmitted in the NN contact, get AR in the SN case. Each trajectory that does so,
brings the factor 2 in conductance. The most interesting correction is one that disallows
some trajectories to undergo AR. However, as we have seen in Sec.3, even a simple change
29
in effective barrier potential (which does not disallow AR) changes ratio of AR and normal
reflection.
We will now review the one-parameter corrections and explain how are they dealt with
in the standard treatment with accuracy (∆/EF )0.
4.1 Finite Gap Onset Length and Exact Momenta
The effects of finite gap onset length (FGOL) have been studied immediately after original
BTK by van Son et al.[12]. They studied the non-self consistent gap. Later on, when meth-
ods for the self-consistent calculation became available (see Sec.6.1) Nagai and Hara [43]
calculated conductance with use of the self-consistent gap for a simple system, and Bruder
[47] for a d-wave SC. However, their extension of BTK was somewhat naive, and it does not
capture the relevant physics at the accuracy level ∆/EF .
The effects of a finite length scale are anticipated in analogy with a quantum mechanical
problem of particle incident upon the ramp barrier. That example is worked out in details
in AppendixA. We expect that conductance above the gap should decrease when we include
the finite gap onset length, i.e. in the case of slow gap onset we expect smaller probability
of AR above the gap than in the case of a step function gap, similar to the transmission
coefficient in ramp-barrier problem of Appendix A.
We already said that the BTK makes an error of the order ∆/EF by setting all the
momenta in the problem equal to Fermi momentum. E.g. error induced in a momentum is:
δk = k+ − kF =√k2
F − 2m/h2 (E2 −∆2)− kF ≈ kF1
2
√E2 −∆2/EF ) (4.1)
and for the characteristic energy scale ∆ we get δk/kF ≈ ∆/EF .
It is a same order of magnitude as the error we get by neglecting the length scale ξ. We
have:
δk =1
ξ=
∆i
hvF
=2π∆
kFEF
⇒ δk
kF
=∆
EF
(4.2)
30
Figure 4.2: A comparison of the BTK conductance (full line) to the similarcalculation with gap onset length ξ, and µ = 1eV , ∆ = 10meV , Z = 0 (left)and Z = 0.367 (right). Note that y-axis doesn’t start at zero.
Note that all corrections to the momentum of the order ∆/EF automatically result in
the corrections to the conductance of the same order - which can be seen on the simplest
example of a single particle of charge e and velocity v = hk/m. Current carried by that
particle is I = ehk/m, so clearly correction in the momentum cause corrections in the current
and consequently conductance.
Calculational approach to this problem is described in Section5.1. Here we present the result
of that approach assuming the non-self consistent gap, using Ginzburg-Landau solution
∆(r) = ∆0 ∗ tanh(r/√
2ξ), where ∆0 is the value of an order parameter in bulk, and ξ is
the temperature-dependent correlation length ξ(T ) = h∗vF/π∆(T ). Only zero-temperature
result is shown, integrated over all angles, in Fig.4.2. In Z = 0 case there is a small
suppression of the conductance above the gap, as expected. It is important to note that this
suppression occurs only if we keep exact momenta k± and q±, unlike the BTK. If we make
approximation that these are equal to Fermi momenta the calculation falls exactly on the
BTK-line. In Z = 0.367 case, besides the suppression of conductance above the gap, there
is an enhancement below, as well as slight shift in the position of the maximum. Reason for
this is more subtle and will be discussed with later.
31
4.2 Non-exact Retro-reflection
The effect of non-exact retro reflection (NERR) of AR particles has been discussed in the
context of sound absorption experiments by Gorelik and Kadigrobov [16] and the thermo-
electric phenomena by Dzhikaev [15]. Kadigrobov [17] made estimates of contribution of
this effect to IV characteristic of NS junctions phenomenologically, and Tafuri et al. [18]
discussed its effect on a conductance of SN junction with layered material. In a completely
different context this effect has been interesting to people studying quantum billiards and
quantum chaos [19].
Let us for the moment consider two systems in contact, with same characteristic EF and
isotropic band mass m, the only difference between them being that one is SC and the other
is N metal. If we wanted to extend a zero voltage bias single trajectory BTK calculation to a
3D tunneling problem, we’d have to integrate over the half-space (solid angle 2π) and weigh
each trajectory by cos θ, where θ is the angle measured from a perpendicular direction. At
zero temperature this approach works. At finite T , the contribution to the tunneling char-
acteristics comes not only from the Fermi surface, but also from the excited particles. It is
excited particles that introduce this correction to BTK.
To understand the nature of it, let us first study a plausible and oversimplified case, and
use it to estimate the magnitude of this correction, and later we’ll get more stringent condi-
tions. Let us observe the particle incoming at an angle θ with momentum ke > kF (Fig. 4.3).
We factor out the parallel component of a momentum, which has to be conserved k‖. An
incoming electron has the momentum k+ > kF , but AR hole has the momentum k− < kF
and its perpendicular component is shorter by the amount 2δk = k+− k−. It moves along a
different path compared to that of an incident electron, it is not exactly retroreflected. For
particles close to the Fermi surface this error is small. Assuming that particles retroreflect
exactly, effectively sets their momenta k+ = k− = kF , which, as shown in (4.1), makes an
error of the order δk/k = ∆/EF .
The problem is clearly that not all particles can undergo AR. Let us observe for simplicity
an excited particle at T = 0, Fig.4.4. In these two examples, excited particles outside of the
32
Figure 4.3: Andreev reflection for a particle above Fermi surface.
space bounded by lines AB and CD cannot Andreev reflect, since there is no available hole for
a final state. Particles k1 and k2 cannot Andreev reflect, even though they are transmitted
in a NN junction. Therefore this effect decreases the normalized conductance below the
gap. The limiting condition for the momentum is ky, kx > kF . For h2(k2 − k2F ) < 2m∆
only specular reflection is allowed, whereas for larger momentum (corresponding to the
energies above the gap) transmission is possible as well. Critical angle is apparently given
by sin θ0 = kF/k+.
Let us see what error one makes with procedure described in Sec.2.2 without limiting
angle θ0. By counting the number of states in a layer of thickness kBT we see that a fraction
of the affected states is of the order(
kBTEF
)1/2
. Since these states are situated at very large
angles, their contribution to the overall conductance is weighed by cos θ ≈ (δk/kF )1/2, we get
corrections to the conductance of the order(
kBTEF
). This is exactly the order of magnitude we
are interested in. In some cases it may be much larger. One example is transport dominated
by the large angle scattering events - in that case most of the N-N trajectories have the same
weighing factor as the SC-N trajectories affected by the described correction; cos θ factor
cancels out in the conductance ratio - the overall correction is of the order(
kBTEF
)1/2
. The
other case is that of a dirty N metal layer - the incoming particle scatters several times
before hitting the interface, and all trajectories have the same weight - cos θ factor is lost,
33
Figure 4.4: Particles on the outside of the space limited with lines AB andCD cannot AR (momenta k1 and k2). Particle k3 is allowed to AR. Left handside is a case kFSC > kFN , right side kFSC < kFN .
and correction is again of the order(
kBTEF
)1/2
.
As Andreev reflection is more important effect for particles going from N to SC than
the other way around, one would expect that this correction is unimportant if kFN > kFSC ,
so that large angles are cut off by a critical tunneling angle θc (determined by the parallel
momentum conservation, see 4.3). This is not so, same state-counting argument shows that
corrections are of the same order, and construction of these states is shown in Fig.4.4. Par-
ticle with momentum k1 is allowed to retroreflect, whereas particle k2 is not, even though
both do contribute to a normal state conduction. This clearly suppresses the normalized
SN conductance. Thus the effect is always strong around the critical angle defined by the
conservation of parallel momentum (see equation (4.6) in the following section).
The effect of NERR on conductance is shown in Fig. 4.5. We assume the randomized mo-
menta of the incoming particles, and parameters are chosen so that the effect is pronounced
(see figure). Compared to the finite temperature BTK calculation, we see suppression of the
conductance below the gap (dominated by AR), and little difference above the gap (where
AR plays small or no role), just as expected form the previous discussion.
Let us now turn to the more accurate treatment, taking into account both an electron and
34
Figure 4.5: The effect of limited tunneling due to the non-exact retro-reflectionin a system with µ = 1eV , ∆ = 10meV , T = Tc/2 = 33K in a dirty limit (lowercurve) compared to the finite temperature BTK calculation (upper curve).
a hole with k 6= kF . Let us study the difference between the angle of reflection of a hole and
the incident angle of an electron. Since parallel momentum has to be conserved, we have:
k+ sin θ+ = k− sin θ− ⇒ sin θ− = sin θ+
√EF +
√E2 −∆2
EF −√E2 −∆2
(4.3)
where θ+ and θ− are the angles of incidence of an electron and a hole measured from a
perpendicular direction. Since θ− ≤ π/2, we see that condition for the critical angle is
actually:
sin θ0(E) =k−(E)
k+(E)(4.4)
where we explicitly stated that the critical angle depends on the energy of a particle. This
situation is shown schematically in Fig.4.6: a particle with momentum k1 is not allowed to
Andreev reflect, even though it is within provisional limits specified in Fig.4.4. A simple
estimate of the magnitude of this correction at the zero bias is still valid, since for all
reasonable temperatures (T EF ) the condition (4.4) is restrictive only at very large angles,
where curve given by (4.4) is almost identical to the straight lines given in Fig.4.4. At this
point it is evident that a zero-temperature calculation also has the conductance supressed by
NERR at the finite voltage bias. A characteristic correction to the conductance by NERR,
35
Figure 4.6: Limit on retro-reflection as given by (4.4) - kmax =√
2kF .
by the same argument as before, is of the order ∆/EF . For a finite voltage, corresponding
to a finite energy offset of an electron and a hole from the original chemical potential, the
magnitudes of the momenta of an electron and a hole are different, and therefore NERR
must be taken into account. Note that θ0 is critical angle for AR only - if a particle has
energy above the gap, it can be transmitted regardless of θ0.
4.3 Angle Dependence of Effective Barrier Strength
It is obvious that if the barrier were of a finite width, particles incoming at different angles
would ’see’ different effective width (weighed by factor cos−1 θ), resulting in the larger reflec-
tion coefficient (or barrier strength). That effect is not of interest here, since it introduces
additional fitting parameter (width of the barrier), and we wish to study one-parameter
models only.
This is purely a geometric effect and has been studied before by several groups. Most
notably Mortensen et al. [20] applied it to a study of NS junctions and found analytic
expression for (4.7) valid at small energies. Sipr and Gyoffry [21] used numerical method to
36
find the effect for particles with arbitrary energy. Prada and Sols [22] showed that the result
of Mortensen et al can be seen as a limiting value of a similar effect with a finite barrier
thickness.
If two sides of the junction have different Fermi momenta and/or effective masses, angle
dependence of the barrier strength enters the calculation in a non-trivial way. It comes
from the fact that properties of Fermi surfaces do not enter the expression for Z simply as
rv = vNF /v
SCF (2.8) - the relevant expression is actually angle dependent, as will be shown
below.
In Fig. 4.7 we show a typical case of two metals with the isotropic effective masses and
different Fermi momenta kFN 6= kFSC . Effective mass anisotropy may also be included,
as we’ll see later. We’ll assume that kNF < kSC
F , and let z-axis be perpendicular to the
barrier. Let us for simplicity study the particle with E = 0. Since the system is isotropic
in a direction parallel to the barrier, momentum in that direction has to be conserved, thus
kNx = kSC
x and kNy = kSC
y . Conservation of energy then forces the magnitude of kz. In analogy
with the perpendicular incidence problem, it is a perpendicular component vz = hkz/m that
enters the expression for Z (2.8). But we now see that angle of the incident and transmitted
particles are not equal, and therefore vNz /v
SCz = vN
F cos θN/vSCF cos θSC 6= vN
F /vSCF !
Starting from the requirement of equal parallel momenta and expressing everything in terms
of incoming angle only, we get:
k2Nx + k2
Ny = k2SCx + k2
SCy ⇒ (4.5)
k2SCz = k2
SCF − k2NF sin2 θ ⇒ kSCz = kSCF
√1− r2
k sin2 θ
where rk = kFN/kFSC , and by definition of θ : kzFN = kFN cos θ. We can also see that
transmitted particles obey Snell’s law:
sin θSC = rk sin θN (4.6)
and that there is a limiting angle to the tunneling process, determined by a conservation of
the parallel momentum sin θc = 1/rk.
Taking into account the expressions for kz we can go back to the equations (2.6, 2.7). We
make the BTK approximation that k+ = k− = kF (thus neglecting the terms of the order
37
Figure 4.7: A contact of two metals with different Fermi wavevectors. Tunnel-ing to (and from) regions above the line AB and below CD is forbidden. Notethat k‖ is conserved.
∆/EF ), and solve for the various components of current (2.10) and conductance (2.11). We
find that all the result from Sec.2.2 are still valid if we make substitution Z → Zeff (θ) and
γ = u20 + (u2
0 − v20)Z
2eff (θ), where:
Zeff (θ) =
(Γ(θ)
(Z0
cosθ
)2
+(Γ(θ)rv − 1)
4Γ(θ)rv
)1/2
Γ(θ) = cosθ/(1− r2ksin
2θ) (4.7)
where rv = vN/vSC and Z0 is unrenormalized barrier strength, as shown by Mortensen et al.
[20]. Note that (4.7) contains both rk and rv. In the limit θ = 0 or rk = 0 we recover the
BTK results.
The effect is shown in Fig.4.8. The barrier strength is set to Z0 = 0, and the ratio of
masses to mSC/mN = 5. Original BTK implies that (2.8) for the ratio of Fermi energies
ESCF /EN
F = 5 we have a perfect junction, since rv = 1. This is not so, and the effect described
here produces finite Zeff. We also see that formula (4.7) takes care of the limiting angle θc, by
producing Zeff →∞ for values θ > θc. For a certain value θZ < θc effective barrier strength
38
Figure 4.8: Angle dependence of Zeff for Z0 = 0, m1/m2 = 5 and values ofEF1/EF2, from the bottom curve: 2, 1, 1/2, 1/5, 1/8, 1/10.
is Z = 0. At that angle perpendicular components of Fermi velocity are equal:
vN⊥/vSC⊥ = 1 ⇒ tan2 θZ =r2v − 1
1− r2k
(4.8)
Clearly, not all combinations of rk and rv allow the occurrence of a zero-barrier angle. Intu-
itively this minimum corresponds to the increased density of target states corresponding to
the tangential direction on the Fermi surface right before the critical angle is reached.
We will now extend the calculation of Mortensen et al. [20] to include the effects of
anisotropy of a Fermi surface. It should be noted that anisotropic Fermi surface even in
the simplest extension of BTK (i.e.not taking into account the effect of bending of the tra-
jectories (4.6)) produces conductance graphs different from the original, one-dimensional
problem. Since particles incoming at two angles have different Fermi velocity mismatches,
their corresponding Zeff are not equal. They produce different BTK contributions to overall
conductance. However, summing them will not result in BTK-graph, since sum of BTK
graphs for different Z will not produce another BTK graph.
We model a Fermi surface by an ellipsoid, with three principal axis (x, y, z) and the
39
corresponding effective massesmx,my,mz. And let’s say thatmz is large, andmx = my ≈ m.
We’ll parametrize this situation by the angle dependent effective mass m1(θ) = m+δm cos θ.
The other side of the junction is an ordinary isotropic metal with the effective mass m2 = m.
We’ll assume that these functions are known, as well as the Fermi energies on each side
EF1, EF2. We need not worry about which metal is SC and which is N, since equations are
automatically symmetric, so we’ll just call them 1 and 2. We have to take into account
the mismatch of Fermi wave vectors kF1/kF2 and Fermi velocities vF1/vF2 in an anisotropic
system. The problem is that we cannot use the relation (4.6), since rk = rk(θ), as well.
Instead we have:
m1(θ1)EF1 sin2 θ1 = m2(θ2)EF2 sin2 θ2 (4.9)
we can find θ2 solving this equation numerically, and with that value find:
rv(θ1) =v1(θ1)
v2(θ2)=
√EF1
EF2
√m2(θ2)
m1(θ1)
rk(θ1) =k1(θ1)
k2(θ2)=
√EF1
EF2
√m1(θ1)
m2(θ2)(4.10)
Using these values we can find Zeff(θ1) for each incoming angle using (2.8) and (4.7). Note
that even in an anisotropic system:
rv(θ1)rk(θ1) =EF1
EF2
(4.11)
With respect to the large angle scattering events, depending on the ratio of Fermi mo-
menta, there are two possibilities for the geometry of this junction, given in Fig.4.7. A
situation with isotropic kF1 smaller than k2‖ is not interesting, since only particles that are
allowed to tunnel are those with large mass and incident angle close to perpendicular. In
the opposite case these events are allowed, but as we shall now see, strongly suppressed.
To avoid cluttering of the data, the results of this calculation are shown in two figures
- Fig.4.9 and Fig.4.10, for various values of EF1/EF2. These two figures correspond to two
different regimes, similar to k1 < k2 and k1 > k2 in the isotropic case. We see that there
is an expected effect of limiting angle sin θc = 1/rk, and that Zeff grows at large angles.
Thus, despite the fact that large angles are expected to be an easy tunneling direction due
to a good matching of the effective masses and the Fermi velocities for EF1/EF2 = 1, this
40
Figure 4.9: Zeff as a function of incident angle, for a system with m1/m2 =(1 + 4 cos θ) and ratio EF1/EF2 (from the left): 20, 10, 5, 3, 2.5, 2.
does not happen, since conservation of the parallel momentum dictates that this is valid in a
negligible portion of phase space. Even the small variation from π/2 in incident momentum
vector, causes a large difference in perpendicular component of the velocity (since two Fermi
surfaces are tangential to each other), and therefore large Zeff. In comparison with Fig.4.8 we
see that minimum in effective barrier strength occurs not for the combination of parameters
that limits the tunneling angle, but rather for a case where whole Fermi surface is allowed to
tunnel. This is no surprise - the critical angle θc is determined by rk only, whereas the zero
barrier strength is determined by both rk and rv (4.8), thus all combinations are allowed.
The overall effect of this correction is that Zeff (θ) gets larger than Z as defined by original
BTK as we go away from the perpendicular incidence. Consequently, total conductance
(integrated over half-space incident angles) is smaller than it would be calculated by applying
BTK with constant Z at all angles. This is particularly important since (by phase-space
argument) it is tunneling at the incident angles close to π/4 that dominates the transport
in three-dimensional contact junction. The effects can be seen in Fig. 4.11, where correction
is included in the dotted line plot, and pure BTK is given by the full line: tunneling is
suppressed both below and above the gap. The point here is that calculated conductance
cannot be fitted by any value of Z, this curve does not belong to the family of curves
41
Figure 4.10: Zeff as a function of incident angle, for a system with m1/m2 =(1 + 4 cos θ) and ratio EF1/EF2 (from the left): 2, 1, 1/2, 1/5, 1/10, 1/20.
produced by BTK.
As already stressed, equation (4.7) and numerical result for the anisotropic case based on
it are valid only in the limit k+ = k− = kF , which we emphatically want to avoid. Including
this correction is already improvement on existing calculations, but it’s not yet up to the
accuracy we are aiming for.
The problem of finding a refraction angle of the transmitted particle without making
k = kF assumption is easily solved in analogy with (4.9), and for the anisotropic system we
have:
m1(θ1)
(EF1 +
√E2 −∆2
1
)sin2 θ1 = m2(θ2)
(EF2 +
√E2 −∆2
2
)sin2 θ2 (4.12)
which is easy to solve numerically. This equation is interesting, because it shows that in the
limit of two isotropic systems in contact, with slowly varying gap we have:
sin2 θ1
sin2 θ2
=EF +
√E2 −∆2
1
EF +√E2 −∆2
2
=
(k+
1
k+2
)2
⇒
sin θ1
sin θ2
=k+
1
k+2
(4.13)
which is of course Snell’s law. What is interesting is that it shows that even for two perfectly
42
Figure 4.11: Effect of the proper inclusion of the angle dependent Z, for asystem with Z0 = 0.1, rk = 2/3. Dots: calculation with correction taken intoaccount; full line - BTK calculated with corresponding Zeff = 0.367.
matching samples, a particle incoming at an finite angle θ1 slowly bends as it goes from N
to SC. Obviously, the order of this effect is δk⊥/kF⊥ = ∆/EF and it is therefore neglected
in the BTK treatment.
43
4.4 Corrections Not Taken into Account
A few comments are due about the corrections we will not take into account here.
• The effect of a finite lifetime of a particle. This is most often used additional parameter
for the BTK fits. It is application of Dynes’ prescription [26] of substitution of energy
E in teh conductance formulas with E + iΓ, where Γ is inverse quasiparticle lifetime.
Inelastic effects at the interface [27] come as another guise of this correction.
• A finite thickness of the barrier. This is an effect that can be very interesting, since
barrier of a finite width is selective in energy and tunneling angle [22]. However, it
does require an additional fitting parameter, and thus doesn’t fall under the scope of
the corrections we are dealing with here.
• A finite length scale of effective mass onset. Besides the additional parameter, it is
very unlikely to occur in the majoroty of physical systems. For an ordinary BTK our
calculations ([28]) showed that this effect only renormalized Z. This is not surprising,
since slow growth of the mass is equivalent to a change of Fermi velocities. Piece by
piece constant increase of velocity just adds small barriers according to (2.8), but it’s
not so clear how would it affect the full self-consistent calculation.
• Boundary conditions for particles in a band. BTK deals with free electrons, and wave
functions with the wave vector kF , yet it uses an effective mass (band mass), which is
explicitly concept related to a particle in band. As such, it does not describe a wave
function itself, but rather an envelope multiplying rapidly varying Bloch function. This
form of solution is not even well defined at discontinuity, and certainly isn’t continuous.
It has to satisfy only generalized boundary conditions of the form [30, 31] (for time-
reversal invariant system): ψL
∂zψL
a b
c d
=
ψR
∂zψR
(4.14)
where a, b, c and d are real and satisfy unitarity condition ad − cb = 1. They can be
calculated microscopically in a few cases of semiconductor junctions. Our attempts to
see the effect of this change in a simple BTK, showed that any choice of parameters
that satisfies the unitarity condition only renormalizes Z. As if instead three degrees
44
of freedom we had only one. This is likely so because BTK makes ansatz that all
particles are plane waves. This need not be true for a more accurate calculation
with self-consistent gap, where wave functions actually fall off over the length scale
ξ. Question of the boundary conditions and effective masses is also neglected in all
self-consistent calculations, and stays as open and potentially important problem.
• Self-consistent treatment of a condensate. Upon Andreev reflection, pair of electrons
is transfered to a condensate and carried away. Condensate current implies gradient
of a phase, as shown by DeGennes [7]:
∆ = |∆| exp(i2qr) (4.15)
where q is a condensate momentum that has to be determined self-consistently. This
form of the gap in BdG (2.1) in turn produces ’Doppler shift’ - change of energy
of particle with momentum k depending on a direction of motion with respect to
condensate wavevector q:
E = ±
√(h2k2
2m− EF
)2
+ ∆2 +h2
mqk (4.16)
Since in BTK we label the particles by their energy, this produces different momenta
for the particles moving ’left’ and ’right’, and therefore their reflection coefficients.
Obviously, self consistence plays crucial role. However, this task is enormously difficult,
since one has to compute both functional form of the amplitude of a gap and of the
phase. The problem is not yet solved in general, though the calculation with fixed
step-function gap is attempted by Sols and Sanchez-Canizares [29].
This effect becomes prominent in a situation when a bulk SC is connected to a N
side via thin, long (of the order coherence length) SC constriction, and current is
comparable to the critical current of SC. This case is at the moment not interesting
for us, and it remains an important open problem.
• Note that in order to keep the correction of Sec.4.3 in one-parameter regime, it is
necessary to know independently values of EN,SCF and mN,SC , since they enter the
expressions independently through both rk and rv, not only the rv as in the original
BTK (2.8). These quantities can be found by independent measurements, and are
assumed to be known. There is a problem with the nature of the effective mass that
45
enters these expressions - since we are operating with currents, it should be the ’current
mass’ in sense of Landau Fermi liquid theory that enters these expressions. That can
in principle be very different from the effective mass as measured by the specific heat
experiments, e.g. Current mass can be deduced from the experiments that measure
coherence length, likeHc2 in SC materials. Since it is often not independently measured
and known, we have to rely on the band-theory calculations or other experiments, that
measure ’fully dressed’ mass. In that sense, this approximation is a true one-parameter
only if the effective mass is not strongly renormalized by the retarded part of electron-
electron interaction, as explained by Deutscher and Nozieres [23].
46
Chapter 5
Calculation of the Conductance
This section discusses the method of calculation of a conductance in NS junction using
approach similar to the BTK. In practice one has to calculate self-consistent gap first, and
use it to calculate conductance. The order of presentation here is reversed. The reason is
that the method for conductance calculation is natural extension of BTK, and it is easy
to follow. The same method will then be used in a more advanced way to calculate gap
self-consistently. Therefore, in this section we will assume that ∆(r) is known, and in the
Sec.6.2 we will develop a method to calculate it. In essence, both sections are version of
calculation on grid, used in various areas of physics - in context of SC systems it was used
to solve the BdG equations (e.g.Hayashi et al [24]) or the time-dependent Ginzburg-Landau
equations [25].
5.1 Particle with Perpendicular Incidence Angle
If we are given functional form of the gap ∆(r), we can calculate the conductance using
generalized BTK scheme. In the spirit of BTK, we assume that parameters of two sides are
known EFN , EFSC ,mN ,mSC , that there is a delta function barrier at the interface, and that
incoming particles cause no change in the system.
For the moment, let’s study only the particle with perpendicular incident angle. Let
us observe the area of size L around the contact on the SC side. We choose L such that
L ∼= mξ(T ), where m is small number (less then 10). It is obvious that one has to choose
47
Figure 5.1: Schematics of approximation of a real potential by a piecewiseconstant model potential.
length of at least L = ξ(T ) in order to observe the effect of the ’full’ gap ∆0. However, in
order to capture the phase change of the wavefunction upon Andreev reflection properly, one
has to take into account part of the wave function that has exponential decay on the SC side
- for the particles with energy E = ∆ the electron-to-hole conversion occurs at distance ξ(T )
from the boundary, and decay takes another ξ(T ) from the conversion point, thus factor m
has to be larger than 2; it turns out that m = 5, 6 captures all the interesting features and
isn’t wasteful on calculational time.
We then divide the region into n parts of equal length such that ξ(T ) L/n > 1/kf .
Let us call the width of each segment l = L/n. The coordinate of the segment boundaries
are z1 for the contact between N and SC, z2, z3 · · · zn. It is not necessary that all segments
are equal, but it’s very convenient for the implementation in the computer code. Assuming
slow variations of the gap on the length scale l, we make an approximation that gap is piece-
by-piece constant in each segment. Thus for segment i: ∆(r ∈ [zi, zi+1)) = ∆(zi +zi+1)/2) =
∆i = const. See Fig.5.1 for the general idea.
The test of the accuracy of this method on a simple quantum-mechanical system with
known exact solution is given in Appendix A.
With this approximation we can solve separately the BdG equations in each segment
(we get the solution for the homogeneous SC), and match the boundary conditions between
48
the contiguous segments. Following the scattering approach to the problem, we assume a
particle entering from the N-side (left), and there are only outgoing particles on the far right
side (inside SC). However, unlike the original BTK, in all the other segments we have all
four types of the quasiparticles, for i-th segment their amplitudes are (see Fig.5.2):
• - a right-going electron-like quasiparticle (eR): Ai
• - a right-going hole-like quasiparticle (hR): Bi
• - a left-going electron-like quasiparticle (eL): Ci
• - a left-going hole-like quasiparticle (hL): Di.
Thus wave function in segment i is:
Ψi = AiψeRi +Biψ
hRi + Ciψ
eLi +Diψ
hLi (5.1)
where ψ are given by the BdG solutions:
ψeRi =
ui
vi
eiq+i zi ; ψhR
i =
vi
ui
e−iq−i xi (5.2)
ψeLi =
ui
vi
e−iq+i zi ; ψhL
i =
vi
ui
eiq−i zi
For the boundary between i-th and i+1-th segment we have (for i, i+1 6= 1, n) as usual:
Ψi(zi+1) = Ψi+1(zi+1) (5.3)
h2/2mi∂zΨi(zi+1)− h2/2mi+1∂zΨi+1(zi+1) = H ∗ δ1,iΨi(zi+1) (5.4)
where H is unrenormalized delta-function potential, as before; in this case it is present only
at the contact, though the algorithm is applicable to the case of many barriers, as well. For
49
Figure 5.2: One segment with corresponding particle amplitudes.
our case we these conditions read (for i 6= 1):
Ai
ui
vi
eiq+i zi + Bi
vi
ui
e−iq−i zi + Ci
ui
vi
e−iq+i zi + Di
vi
ui
eiq−i zi = (5.5)
Ai+1
ui+1
vi+1
eiq+i+1zi + Bi+1
vi+1
ui+1
e−iq−i+1zi +
Ci+1
ui+1
vi+1
e−iq+i+1zi + Di+1
vi+1
ui+1
eiq−i+1zi
for the continuity condition of the wave function. This is same as (2.6), but now we have
all four types of particles on each side of the boundary. For the continuity of the derivative,
equivalent to 2.7:
Aiiq+i
ui
vi
eiq+i zi −Biiq
−i
vi
ui
e−iq−i zi − Ciiq+i
ui
vi
e−iq+i zi +Diiq
−i
vi
ui
e−iq−i zi =
Ai+1iq+i+1
ui+1
vi+1
eiq+i+1zi −Bi+1iq
−i+1
vi+1
ui+1
e−iq−i+1zi −
Ci+1iq+i+1
ui+1
vi+1
e−iq+i+1zi +Di+1iq
−i+1
vi+1
ui+1
eiq−i+1zi (5.6)
If i = n, the above equations are still valid, but since we have only outgoing particles on
50
the right side, we have to set Cn+1 = Dn+1 = 0 (particle incoming from the left, produces
outgoing particles on the right side).
For the first boundary, we have an incoming particle form the left with amplitude A1 = 1,
and no incoming hole, thus B1 = 0. Also, we have to take into account existence of the
δ-function barrier. Since segment 1 is just the normal metal, we have u1 = 1, v1 = 0.
Altogether, for the wavefunction continuity: 1
0
eiq+1 z1 + C1
1
0
e−iq+1 z1 +D1
0
1
eiq−1 z1 = (5.7)
A2
u2
v2
eiq+2 z1 +B2
v2
u2
e−iq−2 z1 + C2
u2
v2
e−iq+2 z1 +D2
v2
u2
eiq−2 z1
For the boundary condition for derivatives we have (taking into account δ-function bar-
rier):
mSC
mN
iq+1
1
0
eiq+i zi − C1iq
+1
1
0
e−iq+1 z1 +D1iq
−1
0
1
e−iq−1 z1− (5.8)
A2iq+2
u2
v2
eiq+2 z1
+B2iq−2
v2
u2
e−iq−2 z1 +
C2iq+2
u2
v2
e−iq+2 z1 −D2iq
−2
v2
u2
eiq−2 z1 =
2mSC
h2 H
1
0
eiq+1 z1+ C1
1
0
e−iq+1 z1 +D1
0
1
eiq−1 z1
Note that H is unrenormalized barrier strength. This closes the system of 4 ∗ (n + 1)
scalar equations with 4∗(n+1) unknowns (C1, D1, An+1, Bn+1 and Ai, Bi, Ci, Di for i = 2, n).
Casting the system into canonical form (unknowns on the LHS, free-terms on the RHS), we
find the solution by using elementary linear algebra, solving for matrix equation:
M ~A = ~B (5.9)
Where we get M by reading off the coefficients in front of the unknowns C1, D1, A2, B2, C2 . . .,
~A is the solutions vector ~A = (C1, D1, A2, B2, C2 · · ·An+1, Bn+1)T . ~B is given by the incoming
51
particle wavefunction ~B = (−1, 0,−iq1, 0, 0, 0...)T . Similar matrix equation is written out
explicitly in Appendix A.
In order to calculate conductance, we actually need only the terms on the far left and far
right side, thus C1, D1, An+1 and Bn+1. For the particle incoming from the N-side they have
the obvious physical meaning:
• - C1 - an amplitude for the specular reflection
• - D1 - an amplitude for the Andreev reflection
• - An+1 - an amplitude for the transmission without branch-crossing
• - Bn+1 - an amplitude for the transmission with branch-crossing.
Since the total probability is conserved, the following condition is satisfied:
|C1|2 + |D1|2 ∗k−1k+
1
+ (|An+1|2 ∗k+
n+1
k+1
− |Bn+1|2 ∗k−n+1
k+1
)mN
mSC
(u2n+1 − v2
n+1) = 1 (5.10)
similar to the corresponding condition in the original BTK. Additional condition is satisfied
on the boundaries between the segments, also corresponding to the conservation of current.
Ji(zi) = Ji+1(zi) ⇒ Im (Ψi(zi)∇Ψ∗i (zi)) = Im
(Ψi+1(zi)∇Ψ∗
i+1(zi))⇒
(k+i |Ai|2 − k−i |Bi|2 + k+
i |Ci|2 − k−i |Bi|2)(u2i − v2
i ) =
(k+i+1 |Ai+1|2 − k−i+1 |Bi+1|2 + k+
i+1 |Ci+1|2 − k−i+1 |Bi+1|2)(u2i+1 − v2
i+1) (5.11)
Though not of direct use for calculating the observable quantities, Eq.(5.11) is an excellent
tool for checking for the systematic errors in calculation, and is used throughout the present
work.
Finally, the conductance for the single quasiclassical trajectory is given by:
σN−SC = 1 + |D1|2 ∗k−1k+
1
− |C1|2 . (5.12)
To get a conductance at a finite temperature, we employ a small trick and the equation
(2.16). We first calculate profile of ∆(r;T ) for a given T . Then for that profile we calculate
σ(E) from (2.16) (i.e.conductance that would result from a given profile at T = 0, and
which in itself is not a measurable quantity), and using (2.16) we get a self-consistent finite-
temperature conductance, which is measured in the experiments .
52
Already at this point we can get some interesting results. Let us put step function for
a gap profile ∆(r) = ∆ ∗ θ(z − z1), and say that potential barrier is Z = 0. Results of our
calculation should then coincide with the analytic BTK solution. That indeed is the case,
only if we make BTK approximation and set k+ = k− = kF ! E.g. for the components of the
current our graphs fall right on the top of those in Fig.2.5. However, keeping the momenta
exact, makes qualitative change. Results of this calculation are shown in Fig.5.3. Note that
coefficients a and d are not zero, compared to results shown in Fig.2.5. Retaining the exact
momenta enables a particle to be specularly reflected and transmitted with branch crossing
even without interface barrier.
Reason for this is the non-exact matching of say incoming k+ from the N side, and cor-
responding k+ on the SC side. Difference of these wavevectors results in a different particle
velocities. Effect of non-matching velocities is similar to (2.8), in a sense that system be-
haves as if there were a barrier. Particularly interesting is an observation that probability for
the transmission with branch crossing d grows with energy, very different from the behavior
of BTK system with barrier (Fig.2.6), where this coefficients falls off rapidly as energy is
increased. Reason for this is that as energy is increased the difference between wave vectors
k+ and −k− gets smaller, and transition to a hole branch gets easier. The effect is very
small, though, and we can see in Fig.5.3 that even for an extreme case ∆/EF = 0.2, branch
crossing and specularly reflection terms carry only 2% of the total current.
Using this method we can also see how is current distributed among the four types of
particles in the space, as shown in Fig.5.4. Electron is incoming from the right, and since
it has E < ∆ exponentially falls off to the right. Same happens with transmitted hole.
Electron and hole going to the right (specularly and Andreev reflected) have components
only on the right side. At some point there is no more current carried by the quasiparticles,
all current is carried by the condensate.
It is not hard to determine the fall-off length. E.g. for an incoming electron with zero
energy, we have:
k+ =
√2m/h2
√E2
F + i∆ ≈√
2mEF/h2 (1 + i∆/2EF ) (5.13)
and it is the imaginary part that produces the suppression of a wave function through
53
Figure 5.3: Components of the conductance for a system with step-functiongap and exact momenta retained throughout the calculation, with Z = 0,µ = 1eV , ∆ = 0.2eV (upper row): a-transmission without branch crossing,b - transmission with branch crossing, (lower row) c - Andreev reflection, d-specular reflection. Note a different scale in parts c and d. Compare withFig.2.5 to see an effect of exact momenta. Vertical axes - current, normalizedto the incoming particle; horizontal axes - energy, in units 0.1meV
54
Figure 5.4: Distribution of the current in space for each component eR, eL(upper row), hR, hL (lower row), normalized to the incoming eR current.Z = 0.7, µ = 1eV , ∆ = 0.1eV . An electron is incoming from the right,position of the barrier is at the mark 50. Length ξ is 10 divisions on x axis.
55
exp(ik+r) term, with factor exp(−∆kF/2EF ). The suppression factor for a current is square
of this term, and we get for a distance at which current falls off to 1/e of its original value:
r1/e(E = 0) = EF/∆kF = h2kF/2m∆ = π/2 ∗ ξ (5.14)
Thus current of a particle at E = 0 penetrated into the SC to a distance of the order ξ. For
particle with energy that is a fraction α of the gap - E = α∆:
r1/e(E = α∆) = EF/∆kF = h2kF/2m∆ = π/2 ∗ 1/(1− α2) ∗ ξ (5.15)
which can be much larger than correlation length ξ.
5.2 Finite Incidence Angle
It looks as if it were easy to apply the procedure given above to the arbitrary angle. Since the
incoming particle ’sees’ longer effective onset length, one way to do it is to simply rescale all
the lengths by the factor 1/cosθ, where θ is angle of incidence, measured from the direction
perpendicular to the interface, and weigh each trajectory by cosθ (since only perpendicular
component of the current contributes to the conductance). The weighing factor for a con-
tribution from angle θ in three-dimensional sample is 2π sin θ ∗ cos θ, where 2π sin θ is the
phase space factor, and cosθ is a fraction that contributes to the conductance. We see that
this factor has maximum when θ = π/4, thus in isotropic three dimensional sample particles
incoming at the intermediate angles dominate the transport.
We have to be careful with this approach, since we are not solving the equations along
the direction of motion. Procedure has to conform to the symmetry of the problem, so we
shall separate the parallel and the perpendicular components, and apply algorithm from the
previous section to a perpendicular component only. Since we are solving BdG equations
(2.1) separately in each segment, we get solutions of the form (2.2), as in previous section.
The difference is that now we ought to take care of the phase accumulated by a parallel
56
component. Solutions are of the form:
ψeR =
u0
v0
eiq+ cos θ∗zeiq+ sin θ∗ρ;ψeL =
u0
v0
e−iq+ cos θ∗ze−iq+ sin θ∗ρ (5.16)
ψhR =
v0
u0
e−iq− cos θ∗ze−iq− sin θ∗ρ;ψhL =
v0
u0
eiq− cos θ∗zeiq− sin θ∗ρ
where ρ is coordinate in x, y plane, parallel to the interface and perpendicular to the direction
of motion, and from the geometry of the problem ρ = z tan θ. Then we can rewrite this
equation (using cos2 θ + sin2 θ = 1) as:
ψeR =
u0
v0
eiq+z/ cos θ;ψeL =
u0
v0
e−iq+z/ cos θ (5.17)
ψhR =
v0
u0
e−iq−z/ cos θ;ψhL =
v0
u0
eiq−z/ cos θ
Thus the result is identical to a ’naive’ one, and the overall effect is that length scale is
rescaled by cos θ−1.
However, we have already seen in Sec.4.2 that incident angle of electron and hole are not
identical for finite energy and θ > 0. Thus, strictly speaking, the wave functions are:
ψeR =
u0
v0
eiq+z/ cos θ+
;ψeL =
u0
v0
e−iq+z/ cos θ+
(5.18)
ψhR =
v0
u0
e−iq−z/ cos θ− ;ψhL =
v0
u0
eiq−z/ cos θ−
where θ+ and θ− refer to an angle of incidence of electron and hole, and they are related
by equation (4.3). This equation takes care of NERR effects. For every segment, starting
from the known energy E and the incidence angle θ+ of an incoming electron, we calculate
the angle θ− for a hole. If θ+ > θ0 given by (4.4), angle θ− becomes complex. Then we
define coefficients in (5.18) so that the entire term is exponentially suppressed when θ− is
complex (this has to be done by hand, since making cos θ− with complex θ sometimes makes
exploding solution either for ψhL or for ψhR). This still allows particle to be transmitted, if
it has enough energy, but cannot AR.
57
Figure 5.5: Schematics of the change of incident angle for a sequence of seg-ments, due to the increase of gap at the barrier, as calculated in (4.12)
.
Next question is how shall we incorporate results derived in Sec.4.3 without dropping out
terms of the order ∆/EF , as we had to do to derive explicit formula (4.7). The beauty of
this approach is that we don’t have to calculate Zeff at all! What are we really doing here is
solving the system of the equations (5.5, 5.6...) with exact momenta retained in all terms.
In that sense, we do not need to reduce the problem to a single mass m, or momentum kF ,
all terms can be kept just like they are, without any renormalization of the barrier strength.
Only Z that enters the problem is Z0 - given by unrenormalized δ-potential, without contri-
butions from Fermi velocity mismatch etc. The problem of finding angle θi for each segment
is solved in (4.12).
Thus the procedure is following: for every given energy and the incident angle for an in-
coming electron θ+1 , we calculate the propagation angle in subsequent segment using (4.12).
Now having a set θ+i for every i, we can use (4.3) to calculate angle for the hole θ−i in each
segment. We suppress hole wave function in segment i if θi > π/2. Now we have set of
wave functions (5.18), which we plug into the procedure for perpendicular incidence given
in Sec.5.1. We solve the system of equations as described, with unrenormalized Z as barrier
strength. For every energy we run the loop over all angles θ, with weight factor 2π sin θ cos θ
and we automatically get conductance with effects of finite angle incidence, NERR and exact
58
momenta accurate in the order ∆/EF (thus, making error of the order (∆/EF )2)...provided
that we had accurate ∆(z) to start with.
By doing this, we have applied all the corrections mentioned in Sec.4, except self-
consistent gap calculation ∆(z). That is a subject of the following section.
59
Chapter 6
Self-consistent Gap Calculation
Important effect that one has to include in the conductance calculations is that of the fi-
nite length scale. While any functional form of ∆(r) can be plugged into the calculation
scheme for the conductance in Sec.(5.1), to get the correct answer we have to use one that is
obtained self-consistently with the same parameters that we use for the conductance calcula-
tion - Fermi energies (ESCF , EN
F ) and effective masses (mSC ,mN) on two sides of the junction,
bulk gap value ∆0 and temperature T and Z. E.g., electrons that we shoot in to test for
conductance have to see same barrier as those in the SC that determine shape of the gap.
All calculations of this kind so far have been done either non-self consistently or in quasi-
classical limit. The self-consistent calculation presented here does not make the quasiclassical
approximation, and as such is valid even in the limit when ∆/EF is not small. Also, it does
not rely on Green function approach, and therefore does not suffer of the problem of ’ex-
ploding solutions’, common to quasiclassical calculations - this solution is given entirely in
terms of wave functions. The fact that only basic formulas (2.1) are used gives it appealing
simplicity. The wavefunctions of the system are calculated numerically, and ∆(r) obtained
from the definition (2.1). The approximation that we do make is that ∆(r) varies slowly
over the range l = L/n (except at the barrier itself), and can be taken to be constant in a
segment of the width l (n is a number of segments, L total length of the region around the
interface that we study). The accuracy of this approximation will be discussed later.
Whatever our approach, the final aim is to calculate functional form ∆(r). Appendix C
60
summarizes the definition and various equations one can use for this calculation. We can
get ∆(r) either by knowing the off-diagonal component of the quasiclassical SC propagator,
or by knowing the wave-functions of the BdG or Andreev eigenproblem.
6.1 Quasi-classical Self-consistent Gap Calculations
To understand the advantages of our approach, let us first look into the standard, quasi-
classical calculation. The first attempt along these lines was made by McMillan [32], who
considered the SN contact without the barrier, and did one-loop approximation, effectively
ending iterative self-consistent process after first iteration. McMillan used Andreev approxi-
mation, but didn’t use the Eilenberger quasiclassical Green function formalism. Eilenberger
[33] and Larkin and Ovchinnikov [34] formulated the equations of motion for the quasiclas-
sical propagator. These equations are supplemented by the various boundary conditions in
works of Buchholtz and Rainer [35] for a surface wall, Zaitsev [36] for a contact between
two metals, Millis et al. [37] for a magnetically active interface, and later in their work by
Ashauer et al. [38] for a non-conventional SC, and Fenton [41] for the heavy fermions. The
application of the formalism to the study of 3He was done by Serene and Rainer[40]. Zhang
et al. [42] calculated ∆(r) for two semi-infinite slabs in 3He, and Kieselmann [39] for the case
of finite N layer touching the bulk SC. Nagai and Hara [43] found the proper normalization
for the contact of two finite slabs, which is applied to calculate ∆(r) in bilayer by Ashida
et al [44] and Hara et al [45], and tri-layer by Nagato [46]. Anisotropic SC are studied by
Bruder [47], and zero-bias states (and their splitting) are found self-consistently by many
groups, e.g. Matsumoto and Shiba [48], Fogelstrom et al [49], Barash et al [50] etc.
The starting point of all these calculations is linearization of the energy spectrum around
the Fermi surface. By making the following ansatz in BdG equations:
un(r, t) = un(r) ∗ exp (−i(E ∗ t− kF nr) (6.1)
vn(r, t) = vn(r) ∗ exp (−i(E ∗ t− kF nr)
we factor out the x, y dependence and fast oscillating part of the wave function in the
direction of motion of particle (or other, dictated by symmetry of the problem), and by
61
neglecting terms in BdG of the order h2/2m ∗ (k − kF )2/EF =√E2 −∆2/EF ≈ ∆/EF we
get the linearized BdG, also called Andreev equations:
Enun(r) =
(−ihvF
∂
∂r
)un(r) + ∆(r)vn(r) (6.2)
Envn(r) = −(−ihvF
∂
∂r
)vn(r) + ∆(r)un(r)
As usual, problem can be discussed in terms of the wave-functions only, or in terms of
the Green functions. If we apply the same approximation to the Green functions in Gorkov’s
equations, we’d get their quasiclassical equivalent - the Eilenberger equations. The basic
formulas concerning these are given in Appendix B. Since Eilenberger equations provide
a condensed way to write sum over the states, they are the main tool in the quasiclassical
study of NS contacts. As shown in AppendixC, we can use either approach to calculate ∆(r).
Compared to the original BdG system, equations(6.2) have a great advantage that they
are the first order differential equations, and thus very easy to solve numerically. Of course,
they have to be supplemented by the boundary conditions. For a moment we’ll consider two
semiinfinite slabs with the same parameters (Ef ,m), the only difference between them being
that one is SC and another N. In that case, un and vn at ±∞ are given by their bulk SC and
bulk N values. The problem that remains is how to match them at the boundary. By making
Andreev approximation, we integrated out the short length scale degrees of freedom (of the
order 1/kF ), so the continuity equations valid for the BdG wave functions do not apply
here. We can find proper boundary conditions by studying the reflection and transmission
coefficients for the current carried by a particle of given energy. The boundary is described
by the behavior of an incoming particle at Fermi surface:
ψ1 =
e−ik1zz + reik1zz ; z > 0
te−ik2z ; z < 0;ψ2 =
eik2zz + re−ik2zz ; z < 0
teik1z ; z > 0(6.3)
For the case that we consider r =√R, t =
√1−R, and R is the reflection coefficient
at the interface, parametrized by the BTK parameter Z as R = Z2/(1 + Z2). We then use
these equations and the continuity of the exact wave function (un, vn) to find the boundary
conditions for a slowly varying part (un, vn), controlled by the Andreev equation.
62
Zaitsev [36] has applied this alghoritm to study the properties of various components of
the Eilenberger propagator. He observed the part of the propagator constructed by two left-
going (g−−) and two right-going (g++) particles (see AppendixB and the following section)
and derived the boundary conditions satisfied by odd and even components of the propagator
with respect to the contact. One can therefore solve the Eilenberger equations numerically
starting from, say, known bulk value of the propagator, with the boundary conditions given
in AppendixB. This is approach used by, e.g. Kieselmann [39] or Bruder [47].
Another approach is pursued by the Japanese groups. They study the asymptotic behav-
ior of the wave-function solution of (6.2), and construct an evolution operator that transforms
the solution along the coordinate axis. From these solutions they construct the Eilenberger
propagator, which automatically satisfies the boundary conditions [45].
Either way, one has to start, with calculations far on the superconducting side, where all
the variables have known, bulk superconducting values, then calculate the derivative from
(6.2) and use that derivative to calculate values at the next step (this is in essence Runge-
Kutta method for numerical solution of differential equation). At the contact, the value at
the SC side will be known, and from the boundary conditions we can calculate the value at
the N side, and continue with the calculation. From thus obtained wave-function/Green func-
tion, we can calculate a new ∆(r) and repeat the calculation until convergence is achieved.
At this point it is obvious why the method needed modification [43] for the finite SN
slabs: if width of the SC slab dSC is of the order ξ or smaller, the gap never achieves the
bulk value, and we don’t know from the outset how to normalize the calculation (i.e. the
starting value is not known). Rather, normalization has to be determined in the iterative
process itself.
The overall accuracy of this approach is limited by the approximation made in the first
step - neglecting the term (k − kF )2 implies that the energy is calculated with the accuracy
of ∆/EF . Also, quasiclassical particles are allowed to live only on their trajectories, and
effects of NERR are neglected, as well as the effects related to the finite incidence angle
63
we discussed in Sec.5.2. The improved method we will now present takes care of all these
drawbacks, in much the same way we did in sections 5.1 and 5.2.
6.2 Improvement on Quasiclassical Approach
One obvious problem with using quasiclassical gap, is that aim of our conductance calculation
in a first place is to include the corrections of the order ∆/EF . As stressed before, quasiclas-
sical calculation explicitly neglects the terms of this magnitude. In order to be consistent,
we have to keep the terms of this size throughout the calculation. It is also methodologi-
cally interesting problem, since some effects simply cannot be taken into account through
quasiclassical approximation - e.g. drift states due to NERR at the (110) surface of SN
contact of d-wave SC, and thus cannot be taken into account self-consistently in density of
states calculation (drift states may be directly observed in an experiment similar to [51],
though they were not found in that particular work). It was this method that we used for
self-consistent calculations throughout this work. Particular appeal for this choice in study
of the conductance is that exactly the same algorithm is used for both calculations.
Instead of the above described quasiclassical approach, we will make use of the algorithm
described in Section 5.1. We divide the region around the boundary in segments, and as-
sume piecewise constant properties (gap ∆ in particular) in each segment. That enables us
to solve the Bogoliubov de Gennes equation (and not the Andreev equation) exactly in each
segment, and match the boundary conditions between them. The process is equivalent to
that described in the previous section, and will not be repeated. Note that we are match-
ing the boundary conditions of the wave functions, and not envelopes (except in a sense of
comment in Sec.4.4), so we are entitled to use usual boundary conditions of the continuity
of wave function and it’s derivative. We start off with initial guess of ∆(r) which may or
may not be a step function. Our aim is to determine convergent solution ∆(r) in an iterative
process using equation (2.1).
At this point we will not specify which side is is SC and which is N. The entire calculation
is insensitive to the swap, as all the expressions are put in a symmetric form. A N side is
64
Figure 6.1: Boundary conditions for a SN contact: an electron incoming fromthe left (A) and a hole outgoing to the right (B). Full line - electron, dottedline - hole. Arrows point in the direction of propagation. N metal is on theleft side of the interface in both figures.
defined in a same way as SC side, with ∆ = 0 and (consequently) Tc = 0. In that sense,
when we speak of an electron or a hole as an abbreviation for ’electron-like quasiparticle’ or
’hole-like quasiparticle’.
Let us observe an incoming electron from the left (eR) (Fig.6.1, A ). It will propagate
to the boundary, and there either get transmitted or reflected in one of four ways. Note
that there is a finite probability for a transmission to a certain distance even if E < ∆ (see
Fig.5.4). Possible sequence of specular and Andreev reflections is given in Fig.6.2. We see
that in this process we start with pure electron with a wave function in particle-hole space
(1, 0)T , and we end up with a mixture of electron and hole wave-function on every ’branch’
of this process. This is a process that describes transfer N side particles into a SC. Note
that this is exactly the same calculation as the one described in a Sec.5.1 - we shoot electron
from a RHS and calculate it’s wave-function everywhere. The difference is that now we are
not interested in transport properties (i.e. coefficients C1, D1, An+1 and Bn+1), but rather
in the amplitudes of the resulting wavefunctions throughout the system. These amplitudes
were calculated in Sec.5.1, but were not used - they were just intermediate states connecting
65
particles we were interested in (i.e.outgoing particles at the edge of the system).
We also need to include a process that describes transfer of particles from SC to N. We
choose boundary condition of outgoing hole (hR) on the SC side (Fig.6.1, B). Both cases can
be described by a same diagram in Fig.6.2 (left panel). It takes very little modification to
our algorithm from Sec.5.1 to describe wave functions resulting from this boundary condition
(e.g.we can make prescription u ↔ v and k+ ↔ −k− and use the same algorithm). This
process describes transfer of a hole (in this case outgoing) from SC to N metal.
We also need the processes that describe transfer of a hole from N to SC, and an electron
from SC to N. For that we choose outgoing hole on the right (hL) and incoming electron
on the left (eL). These two cases produce diagrams corresponding to Fig.6.2 with all arrows
reversed. They are also calculated easily with prescriptions similar to the algorithm for (hR).
There are also other possible processes, but they are not independent from those described.
Each of these processes results in a wave function of a type (5.1) in each segment. All
we have to do now is to use the self-consistency condition of BdG to calculate the gap:
∆(r) = V Σnfn(r, t)g∗n(r, t) ∗ (1− 2n(En)) (6.4)
Since ∆ exists only on SC side (where V is non-zero), we also define correlation function,
which describes the density of pairs on both SC and N side:
F (r) =∑
n
fng∗n(1− 2n(En)) (6.5)
Sum n runs over all available states. In BdG we have four states for each energy, and those
are the states we described with four boundary conditions (eR, hR, eL, hL). Contribution
to the gap from each of them is added separately. A question left is how to deal with two
intersecting branches of the same wave-function that contribute to the correlation function.
We can either add amplitudes and then make product uv∗ or the other way around. Since
this is one wave function, we really should do the former. However, ’interference’ terms
resulting from such product have the fast oscillating factors of the type exp(i(k+ + k−)) or
exp(2ik±), compared to exp(±i(k+ − k−)) or 1 that we have on a same branch. These fast
66
oscillations get averaged out to zero, and we will not include them (this is also standard
procedure in the quasiclassical theory).
Let us write down explicitly the wave function (f, g)T in segment i:
Ψ =
fi
gi
=
Aiuieik+
i r +Bivie−ik−i r + Ciuie
−ik+i r +Divie
ik−i r
Aivieik+
i r +Biuie−ik−i r + Civie
−ik+i r +Diuie
ik−i r
(6.6)
Summing all the non-fast oscillating terms together we have:
∆(r) = V∑
n,θ,p(1− 2n(En)) (6.7)(ui ∗ Ai ∗ eik+
i r + vi ∗Di ∗ e−ik−i r)(vi ∗ Ai ∗ eik+i r + ui ∗Di ∗ e−ik−i r)∗ +
(vi ∗Bi ∗ eik−i r + ui ∗ Ci ∗ e−ik+i r)(ui ∗Bi ∗ eik−i r + vi ∗ Ci ∗ e−ik+
i r)∗|n,θ,p
where p is counting particles for each state p =eL, eR, hL, hR; the sum now goes over
all positive energy states n and incident angles θ. States with three indices (n, θ, p) are
non-degenerate. Subscript i denotes that functions of r are calculated in the segment at
distance r; r ∈ [i ∗ l, (i+ 1) ∗ l). The notation is same as that of Sec.5.1. Note that u, v,
and k± are all implicit functions of ∆(r) and E. To get actual ∆(r), one has to sum the
contributions from all energies and angles. Exactly the same equation applies to the right
side, with appropriate r and i plugged in. Prefactor V is interaction constant, which we
dispose of by normalizing a gap to the known bulk value far on the SC side.
In drawing Fig.6.1 and Fig.6.2 we pretended that particle specularly reflects only at the
interface. However, as we know from 5.3 if we keep the exact momenta this is not true.
In practice this is not a problem, since algorithm allows mixing of the components of wave
functions at every step.
The results of this calculation are well-known from the quasiclassical approach. Clean
limit contact has a gap that decays on the length scale ξ. At finite temperatures ξ(T ) in-
creases, as consequence of the decrease of ∆(T ).
The presence of barrier disrupts the transport of pairs across the contact, and conse-
quently the fall-off length is shorter then ξ. In the limit Z → ∞ gap stays constant all
the way to the contact. This case is equivalent to the outer surface of SC (’N metal’ is
vacuum), and the result can be explained by the well-known Anderson argument. This goes
67
Figure 6.2: Processes (A) and (B) from the Fig.6.1 drawn to include AR alongthe trajectory (left). Contributions to the gap from two trajectories at everypoint in space (right).
as follows: in s-wave SC, non time reversal breaking impurities (including surfaces) have an
effect of mixing different values of momentum k. This means that k is not a good quantum
number anymore, however, that does not influence the SC properties, since SC Hamiltonian
can be rewritten in terms of new time-reversed states (n, n) instead of the usual (k,−k). In
particular, the gap will not be supressed at such impurities. This is also valid for Z → ∞
case. For finite Z, closer we are to this limit, shorter the gap-onset length.
Although no results by other authors are available to check the application of our method
in the regime ∆/EF ≈ 1, with the choice of parameters appropriate for Nb (EF = 4eV,∆ =
1meV ) the results are in agreement with those of quasiclassical approach (see Fig.6.5).
Following discussion is related to the Nb at T = 0 in contact with isotropic N metal with
same characteristics as Nb.
Fig.6.3 shows the contributions to the pair correlation function (defined by equation (??)
from two different energies. A left figure shows the energy just above the gap. Oscillations
are related to the coherence between electron and a hole, wave length is 2π/(k+ − k−). We
see that it is smaller on the N side - since in SC an electron and a hole just above the gap
have (almost) the same wave vector (see Fig.2.1). Figure on the right side is for energy of
the order 3∆ - electrons and holes in SC are almost decoupled, and interference terms are
68
Figure 6.3: The unnormalized contribution to the pair correlation function(6.5) from the particles of one energy and along one incident angle for Nb,Z=0, T=0 (E ≈ ∆ (left), E ≈ 3∆ (right)). Units on x-axis are 1/10ξ, andcontact is at the mark 100, N is to the left, SC to the right of it.
of the same wave length as in N.
In Fig.6.4 (left) we see the contributions from one angle - θ = 0 integrated over all en-
ergies. The ripples are consequence of electron-hole coherence, and they disappear after we
sum contributions from other angles (right). They are not artifact of the calculation. They
appear because Andreev reflection (the source of electron-hole coherence) occurs in a limited
energy range, and contribution to the pair correlation function from corresponding k+−k− is
dominant. Note that in Fig.6.3, scale along the ’F ’ axis (vertical) is ten times larger for the
particles of smaller energy (two graphs have same normalization, and are thus comparable -
even though they are not normalized with respect to the bulk value of F ).
In Fig.6.5 we have the pair correlation function after three iterations, and the gap cal-
culated from these iterations. The gap value changes somewhat in subsequent iteration, but
the curves are too close to be shown in this figure. A finite temperature calculation is given
in 6.6. To do this calculation we use the transcription of integral with Fermi factor to a sum
over Matsubara frequencies, given in Appendix C. Besides the smaller gap, we see that the
effective correlation length ξ is longer (gap grows to the full value over longer distance). In
Fig.6.7 the same calculation is repeated for barrier with Z = 4. Evidently, there is a jump
in correlation function, and gap offset value (initial jump of gap magnitude) is 0.9∆ (instead
of 0.5∆ for a clean contact).
69
Figure 6.4: The unnormalized contribution to the pair correlation functionfrom particles at an incident angle θ = 0 (left) and integrated over all angles(i.e. after complete first iteration) for Nb, Z=0 (E ≈ ∆ (left), E ≈ 3∆ (right).Units on x-axis are 1/10ξ, and contact is at the mark 100.
Figure 6.5: The calculated gap in each iteration (top to bottom) (right) andthe unnormalized pair correlation function after three iteration loops (left) forNb, Z=0 . Units on x-axis are 1/10ξ, and contact is at the mark 100.
70
Figure 6.6: Self-consistent gap and normalized pair correlation function forT = 0.95Tc, all parameters are the same as in other figures.
Figure 6.7: Self-consistent gap and normalized pair correlation function forbarrier parameter Z = 4.0, T = 0, all parameters the same as in other figures.
71
Figure 6.8: Self consistent gap after 4 iterations for EF = 1eV and ∆ = 0.1eV(left) and ∆ = 0.2eV (right) at T=0, Z=0.
Finally, we show the results in the case when ∆/EF is not small in Fig.6.8. One interesting
feature that we would like to stress is offset value of the gap, which is not 0.5∆ as for other
clean systems, but larger. We saw that large value of gap offset corresponds to the presence
of the barrier (Fig.6.7). The ’barrier’ in this case is a mismatch of wave vectors on N and
SC side due to the large gap, which we already saw to produce an effect similar to finite Z
in Fig.5.3.
.
Let us address the accuracy of the method. As we said above, the quasiclassical method
neglects energy terms of the order ∆/EF . An error that we make using segment model is
of the order (∆/Ef )/n on each segment. Note that for the given boundary conditions (i.e.
solution in the contiguous segments) solution Ψi in the i-th segment is exact - wave function
itself bends to accommodate imposed boundary conditions. For this reason, error in one
segment cannot propagate to other segments, only choice of potential ∆i causes error in
segment i. We see that only if there is a systematic error in choice of potential ∆i, we will
have overall accuracy as big as quasiclassical one. If the choice of potential is ’perfect’ (in a
sense that boundary conditions of a wave function are identical to the exact solution on that
segment for given E), solution is exact in the limit n→∞, and the error propagation is sim-
ilar to the one-dimensional random walk (which is, of course, localized). In a case that there
is a small systematic error in choice of ∆i, this random walk process acquires a drift, and
there is finite error even in the n→∞ limit, although still smaller than the quasiclassical one.
72
Chapter 7
Results and Interpretation
We will now present the results of a fully self-consistent calculation taking into account
the corrections from Sec.4, on a model of a contact junction between highly anisotropic
and isotropic metal. Choice of anisotropy is stipulated by the results of [14]. According
to Deutscher and Nozieres [23] not all the renormalization of electron mass is important
in tunneling, it is also clear that in CeCoIn5 at least part of the anisotropy comes from
lattice structure effects - we choose the numbers so that in the limit of clean contact they
approximately reproduce ZB conductance measured by [14]. We choose model anisotropy as
in Sec.4.3:m1/m2 = 1 + 4 cos θ. Results for the zero-temperature conductance are given in
Fig.7.1.
Conductance plots in Fig.7.1 are compared with the BTK fit that has same value of
high-voltage conductance. We see that plots are not identical to BTK, but they still have
undoubtly BTK features - such as coherence peak and finite subgap conductance. There
is not much difference between the gap onset length scales for these systems - see Fig.7.3
for comparison of the self-consistent gap for systems with ratio of Fermi energies 0.2 and 3.
Thus, most of the differences comes from what in BTK limit (all momenta set to kF ) would
be renormalization of Zeff and NERR.
Let us make a couple of remarks about the results before going to discussion of details. It
is interesting to compare plots of Fig.7.1 and Fig.7.2. We have plots for the ratio of Fermi
energies 2 and 3 given for the same Fermi energy of the N side (1eV) and three different
73
Figure 7.1: Evolution of the conductance curve formSC/mN = (1+4 cos θ) andEFSC/EFN 1/5, 1/2 (upper row), 2, 3 (lower row). EF = 1eV , ∆ = 10meV ,Z0 = 0. Full line is BTK curve, fitted to the high energy values, dotted lineis this calculation. Vertical axis is a conductance, normalized to a perfectcontact, horizontal - energy, in units 1/100∆.
74
Figure 7.2: A conductance curve for mSC/mN = (1 + 4 cos θ) and EFSC/EFN
- 2 (left)and 3 (right) . Z0 = 0, EF = 1eV , ∆ = 100meV (upper row)and ∆ = 200meV (lower row). Full line is BTK curve, fitted to the highenergy values, dotted line is this calculation. Vertical axis is a conductance,normalized to the perfect contact, horizontal - energy, in units 1/100∆.
Figure 7.3: A comparison of the self-consistent calculation of the gap for asystem with mSC/mN = (1 + 4 cos θ) and EFSC/EFN - 0.2 (dots) and 3 (fullline), after four iterations. Vertical axis is gap in eV , horizontal is distance inunits 1/10ξ - contact at 50.
75
values of the gap on SC side - 10meV, 100meV and 200meV. There is a surprisingly little
difference between the plots, and the plots with gap of 10meV and 100meV are almost
identical. Only gap of 20% of Fermi energy bring significant change, mostly due to the
non-matching of various wave-vectors and the effects of NERR. One interesting feature is
that large gap plots have a slight upturn in the conductance as E → 0. This is due to the
mismatch of the momenta, which is smallest at ZB and also due to the NERR, which is
important at finite voltages. As energy increases, the mismatch grows larger, and in a sense
of Fig.5.3 ’an effective barrier’ gets larger. Note that since we do not have a real barrier in
this case, it is not a surprise that there is not much change in the conductance above the gap,
where NERR is not important process - comparing to Fig.5.3 we see that the overal effect
of the mismatch of the momentum vectors is very small, and that current above the gap is
also carried by a branch-crossing process. Also, as the gap increases, the coherence length
gets smaller, and so the effect of the finite length-scale in a system becomes less important.
It is the ratio of conductance at E < ∆ and E ∆ that is to some extent non-BTK like,
and that can be explained by a finite length-scale effects, which we will now discuss.
7.1 Effects of Finite Gap Onset Length
As expected in analogy with the quantum-mechanical ramp potential, and as discussed in the
connection with Fig.4.2, the finite gap onset length combined with the momentum mismatch
leads to the suppressed excess conductance above the gap. This effect is more prominent
with the longer gap onset length, which is of the order L ≈ ξ. On the other hand, L ≈ ξ is
inversely proportional to ∆. A momentum-mismatch on two sides, which also reduces the
conductance, is proportional to ∆ (for small ∆, at least). Thus only one of these two effects
can be large.
A self-consistent calculation limits the size of ξ. This restricts a behavior very different
from the BTK to the quasiclassical trajectories at very large incident angles (with effective
L(θ) = L/cos(θ) ξ). However those particles carry a small perpendicular component of
momentum, and have a little influence on the overall tunneling characteristic (integrated
over all angles).
76
Figure 7.4: Evolution of the subgap structure with incident angle, Z=1.3,Ef = 1eV , ∆ = 1meV : full line - BTK, dots - this calculation, normalized sothat conductance at high voltage without barrier is σ0 = 1. Consequence ofthis normalization is that subgap conductance σSN(E) = 2 means that particleat that energy does not feel the presence of the barrier.
We have seen both in Fig.4.2 and in Fig.7.1, that there is a slight shift of a maximum
conductance from the gap edge to the values of energy E < ∆, accompanied with the
enhanced subgap conductance (compared to the BTK), as if gap were ’filling up’. To see
why this happens, let us isolate the effect of the trajectories at very large incidence angles.
Fig.7.4 shows the sequence of the trajectories incoming at a large angle. In this calculation,
to make the effect more prominent, we did not use the self-consistently calculated gap (it
will be clear later why - it tends to suppress the effect we are to demonstrate). Instead, we
use Ginzbug-Landau form. We see that maximum is shifted more as the angle, and thus
the effective length L/cosθ increases. The conventional interpretation of that effect is that
quasiparticles probe only the length-scale ξ inside SC, and thus cannot reach the distance
where the full gap is achieved (see Fig.5.4). But what is the mechanism of that effect in this
calculation?
77
Figure 7.5: The schematics of the model of slowly varying gap. N - normal side,SC - superconducting side (with gap ∆). Region R is either superconducting(with gap ∆ < ∆SC), or normal (∆ = 0).
Our interpretation is following: the maximum of conductance appears when a wave
function in the region between interface and reflection point has a node at the position of
the barrier. Let us see how that happens.
Let us consider the situation given in Fig.7.5: the region R is between the SC on the right
and the N metal on the left. The gap in SC is ∆SC . Between R and N there is a potential
barrier. We consider the situation when R itself is a superconductor with a constant gap
∆ < ∆SC or a normal metal (with zero gap).
Let us first consider the case when R is a normal metal, and observe the wave func-
tion made up of an electron and AR hole of the same amplitude A = 1/√
2, and find the
probability density of such state:
ΨN = ψeR + ψhL = 1√2
1
0
eik+r +
0
1
eik−r+∆φ
(7.1)
|ΨN |2 = 12(1 + 1) = 1 = const. (7.2)
where ∆φ is the change of phase upon Andreev reflection, cos ∆φ = E/∆SC . Since elec-
trons and holes do not mix in normal state, there is no interference effects, and probability
78
density is constant.
We now look at the similar situation with R being SC. A state corresponding to ΨN is:
ΨSC = ψeR + ψhL =1√2
u
v
eik+r +
v
u
eik−r+∆φ
(7.3)
with probability density given by:
|ΨSC |2 = 12
2|u|2 + 2|v|2 + (uv∗ + vu∗)ei(k+−k−)r−∆φ + (uv∗ + vu∗)e−i(k+−k−)r+∆φ
=
1 + uv∗ cos((k+ − k−)r −∆φ) + v∗u cos(−(k+ − k−)r + ∆φ) = (7.4)
1 + 2 Re (uv∗) cos ((k+ − k−)r −∆φ)
And with the constant gap in R and energy E positive, using the explicit formula for u
and v we get:
|ΨSC |2 = 1 +∆
Ecos((k+ − k−)r −∆φ
)(7.5)
Thus in a superconducting system, wave function is a mixture of an electron and a hole,
and has a modulations of probability density on a scale 2π/(k+ − k−). If the barrier is at
a position of the minimum, tunneling is enhanced. Position of the minimum is given by
(setting ∆φ = 0)
(k+ − k−) ∗ Lmin = π → L ≈ hπvF
4√
(E2 −∆2)(7.6)
where Lmin is measured along the trajectory, from the Andreev reflection point. In our sim-
ple model, for every energy E there is an angle θ, such that distance d/ cos θ = Lmin (where
d is a size of region R), and the other way around - for every effective length L = d/ cos θ we
can find an energy that corresponds to a wave function with minimum at the position of the
barrier, resulting in a conductance peak. In real life the situation is more complicated, since
different energies have different reflection points distances (i.e. distance d in this model).
the higher energy terms result in an oscillations on a shorter length scale.
However, note that because of the pre-factor ∆/E in equation (7.6) a short distance
Lmin corresponds to a very shallow minimum in the probability density. To get small overall
|ΨSC |2 one needs small E, and therefore large incidence angle. To get effective coupling
reduced by a factor 5, since δ-function potential couples to the probability density, we need
79
E = 5/4∆. This results in Lmin = ξ ∗ π2/3 ≈ 3ξ, or incident angle such that cos θ = 1/3,
θ ≈ 70o. Thus, this is clearly not an extreme angle effect. If we observe a single trajectory,
we will find that conductance maximum shifts toward lower energy as we increase the in-
cidence angle. Note that arguments from Sec.3 do not apply here, since we are explicitly
taking into account difference in momenta of an electron and a hole.
We can demonstrate that our interpretation is correct by performing the same calculation
as in Fig.7.4 with q+ = q− = kf , so that phase difference doesn’t accumulate along the path.
As shown in Fig. 7.7, with this approximation a maximum does not shift from ∆.
Thus ’filling up’ of the subgap conductance is due to the shift of conductance maxima at
large angles toward E < ∆. Note that this ’filling of the gap’ is not related to the transfer
of a spectral weight of particles from higher to lower energy. It is consequence of the change
of the reflection coefficient for a particle of given energy due to the geometry of the problem.
Also, note that there are oscillations of wave length
λ =2π
(k+ − k−)≈ hπvF√
(E2 −∆2)(7.7)
exist for all energies. For E = 2∆ wave length of the oscillations is exactly λ = hvFπ∆ =
π2 ∗ ξ. These oscillations are of the same origin as those we have seen in Sec.6.2 - coherence
between electron-like and a hole-like wave functions.
Another possibility is that the conductance peak may be a signature of the bound state.
This state at energy E should be localized inside the SC, between the barrier and the point
where gap reaches value E. This is equivalent to De Gennes-Saint-James [4] states that
occur in the thin N overlayer on the surface of SC. This has been suggested by Nagai et al.
[43], but that is just a different interpretation of the same phenomenon. Condition for the
existence of the bound state is that wave-functions add coherently - with the same phase.
This is achieved when integer number of wave lengths fits in the binding potential region,
which is exactly the condition given above (7.7) - with RHS multiplied by an integer. Thus
two ways to resolve this effect are equivalent. It should be stressed that these bound states
are automatically included in the self-consistent calculation of the gap function, and do not
80
Figure 7.6: The schematics of the condition (7.6): (A) - side view (distance vs.energy), (B) - view from the above. A thick vertical line is a surface barrier,a thin line is the position where Andreev reflection occurs
.
require special handling.
The process is shown in Fig.7.6. Part (A) shows sideview (distance vs. energy), and part
(B) view from above (x vs. y coordinate). When condition (7.6) is satisfied, we have the
upper case in (B): particle goes in and out of the barrier-gap potential well. The reflection
line is defined as a position at which wave-vector of electron becomes imaginary. If (7.6)
does not apply, there is a finite probability that (i) the incident electron will get reflected
and (ii) the outgoing hole will be reflected back, transfered to an electron again, and make
another attempt to go through the barrier as the electron. The latter process results in a
smaller conductance than the former. This figure demonstrates what is basically De Gennes-
Saint-James [4] bound state, with limitation of zero-barrier at surface of SC (i.e. only ’one
reflection’ states are allowed), and somewhat different energy spectrum (since k+ and k− are
space-dependent).
To conclude, is evident that most interesting effects due to the finite gap onset length
occur when transport is dominated by the large angle tunneling events. An obvious choice
is isotropic material in contact with a nearly two-dimensional metal, such that there is a
large mismatch of Fermi velocities at 0 incident angle, and a good match close to π/2. These
are exactly the conditions when the other two effects we study become prominent, and we’ll
81
Figure 7.7: Conductance at very large incident angle θ > 88o, Z = 1.3, Ef =1eV , ∆ = 1meV . Full lines are BTK formula. Dots are calculation without(left) and with (right) k = kf approximation. The normalization is the sameas above.
have to study their interplay.
7.2 Effects of Mismatch and Anisotropy on Fermi Surface
We saw in Sec.4.3 that the effect of the non-matching Fermi energies and the non-matching
effective masses suppresses the tunneling at the large angles, and in particular it suppresses
the large angle tunneling in a system that is natural choice for the prominence of the large
angle tunneling events - one with our model of the effective mass. In other words effects of a
finite gap onset length scale and non-matching Fermi surfaces to a large extent cancel each
other. Though in some cases this effect leaves an easy tunneling channel open at a large angle
(Fig.fig:Eratio2) that channel is either not wide enough for the effects of phase accumulation
to be prominent, or it is not at the angle where cos−1 θ makes effective length sufficient for it.
Note that the conductance in Fig.7.1 has an interesting feature as function of EFS/EFN .
It almost doesn’t change between the values 0.2 and 0.5, and then it falls off for the values
2 and 3. Value 2 is a limiting number, where we still have a minimum for Zeff = 0 in Fig.4.9
and Fig.4.10, however that minimum for ratio 2 occurs at a large angle, and thus has little
consequence for the transport. Besides that, at the finite voltage it tends to be suppressed
by the effects of NERR. One expects that smaller values of ratio of Fermi energies still have
82
an easy tunneling channel open at smaller angles, resulting in a much higher conductance.
Even though that channel is also open in k = kF limit for EFS/EFN = 2, it does’t seem
important in these figures. We conclude that the difference between ratios 0.5 and 2 is due
to the features of Zeff that survive even when not taking the BTK-like limit k = kF .
7.3 Effects of Non-exact Retro-reflection
There is another effect dominant at the large angles - non-exact retro-reflection (NERR).
Effect discussed in previous section changes only the effective barrier strength, which affects
equally N-N and N-SC junction. As shown in Sec.3 small change in this quantity changes
the normalized conductance by less than factor of 1/2 for selected trajectories. On the con-
trary, Andreev refection is exclusively SC effect, and anything that affects it must result in
a change of normalized conductance of given trajectory by a factor of 1/2, or not at all. The
main effect has already been shown in Sec.4.2, and we will here only briefly comment on its
interplay with other factors.
As we already said in Sec.4.2, we are dealing once more with the effect that in general
suppresses the conductance. In particular, it suppresses the conductance at large incident
angles. That means that at finite temperature trajectories that result in the most interesting
features associated with finite gap onset length will be suppressed. Thus here NERR works
in the same direction as the effect of FS mismatch and both against a finite onset length.
What is more interesting is the effect close to the critical angle (4.6). We saw in Fig.4.8
that for a particle incoming with an angle just below θx, Zeff → 0. These particles have an
easy tunneling channel, and as such a strong influence (and if θc ≈ π/4 the strongest) on
tunneling characteristic in both NN and NS junctions. And that is exactly the channel that
will have AR suppressed by non-retroreflection.
To conclude: even if Fermi velocities are not equal, we can have a direction in which ef-
fective barrier is zero - an easy tunneling channel (contrary to original BTK), but transport
along that direction is limited by NERR. In this case, FS mismatch and NERR work against
83
each other.
7.4 Effects of Self-consistence
As the main point of this work is taking all the effects into account in a self-consistent man-
ner, we will now discuss how does the self-consistent calculation limit the effects discussed
above, and how is the calculation itself changed to accommodate them.
Self-consistence determines the precise functional form of a gap, and therefore limits the
length scale available for the finite gap onset length events. Not only that length is limited,
but a functional form is very peculiar, Fig.6.5. There is a sudden jump, steep growth, and
then slow settling toward the bulk value. Below the offset value of a gap (which is ∆/2 for
a clean boundary, and more than that for a finite barrier), there can be no bound states
or conductance peaks discussed in Sec.(6.5), since there is no space between the interface
barrier and reflection point for the wave function oscillations to take place. Thus these are
severely suppressed everywhere but in the energy range just below the bulk value of the gap.
That is a region where a conductance peak related at E = ∆ occurs in BTK. Width of that
peak is smaller as a barrier strength is increased, but exacty the same effect makes onset
length shorter. This brings us to another counterintuitive property of this system - that
BTK should work better for imperfect junctions than for the perfect one. A rationale is that
the large effective barrier strength by self-consistency produces the short gap onset length,
thus suppressing one source of the discrepancy with BTK. This is easily seen even without
the self-consistent calculation: a good contact of two metals with equal vf produces L ≈ ξ,
whereas at a contact with the vacuum (at least for a s-wave case) gap has basically the form
of a step function, thus L→ 0, which is exactly the BTK ansatz. All real-life junctions are
somewhere in between.
Self-consistency plays an important limiting factor in the system described in Sec[7.2).
We required a large mismatch in Fermi velocities at the angle θ = 0 in order to enhance the
effects of large scattering events. However, a large effective barrier created that way produces
84
very short effective gap onset length, L ξ. Thus even the large angle tunneling events
cannot accumulate enough phase difference to produce a significant shift of the maximum,
which was a purpose of this choice of system. In general, self-consistence limits the effects
of the very feature it creates - finite length scale in NS junctions.
85
Chapter 8
Conclusions
Even if the overall effect of the studied corrections is not very interesting (being relatively
small and not producing significant departures from the BTK), the reason for it is inter-
esting - it comes about because the various corrections work opposite of each other, and
self-consistency gives the negative feed-back to any attempt of a large discrepancy with
BTK. This to some extent explains the robustness of the BTK model. It is worth pointing
out again that this claim explicitly applies only to the corrections that do not introduce an
additional fitting parameter - situation is quite different if we introduce a finite-width barrier
or a finite quasiparticle lifetime. None of the effects described, nor their combination, seems
to suppress the conductance peaks close to E = ∆ - all peaks in Fig.7.1 have their peak
reaching exactly 2.
To be fair, it should be stressed that detailed changes in the shape of gap, even though
interesting in itself, have very little influence on the resulting conductance curve. It is the
main features - as onset value of the gap (i.e.jump at the barrier), bulk value, and length scale
that govern the conductance, and it matters very little what is the exact functional shape.
In retrospect, had one been able to determine these features for the general combination of
parameters, whole exercise presented here would be futile. However, we do not have such
’rule of thumb’, and the full self-consistent calculation presented here is not only a matter
of principle and methodology, but a necessity.
Though the conductance plots we get are to some extent different from BTK, they still
86
show unmistakable features of the BTK calculation. The fact that various renormalizations
may change Z appreciably, does not matter, since the experimentalist is still fitting the data
in the same way - using effective Z as a fitting parameter, regardless of its origin.
Our program to find better fitting functions for BTK approach is fulfilled. With given
Fermi surface parameters we can now construct the new fitting function which is certainly
better than the BTK, although not spectacularly different. We are not introducing any new
physical effects, but simply considering physics already in the starting formulation of the
BTK, to the higher degree of accuracy.
In connection with the experiment discussed [14], it is evident that the corrections de-
scribed here cannot account for its results. In particular, none of the corrections we studied
can account for the suppression of the ZB conductance without emergence of the conduc-
tance peaks at the gap edge. It is likely that other effects described in Sec.4.4 may play an
important role. Also, corrections studied here are to a large extent purely kinematic, and the
heavy-fermion compounds are strongly interacting system with correlated dynamics. Before
undertaking more complex calculation, it is good to get simpler possible causes out of the
way.
87
Appendix A
Quantum Mechanical Ramp Barrier
The purpose of this section is twofold: to give a motivation for a study of the finite gap
onset length scale effects in tunneling experiments, and to demonstrate the accuracy of the
approximation scheme used for the conductance calculation. We will calculate the reflection
coefficient in a simple one-dimensional quantum-mechanical problem of a particle incident on
a ramp potential, for which we know the exact solution, and compare it with the numerical
prediction.
A.1 Exact Solution of the Tunneling Problem
Let us consider the Schrodinger equation
− h2
2m∗∂2
∂x2ψ(x) + V (x)ψ(x) = E ∗ ψ(x)
with potential V (x) given by:
V (x) =
0 x < 0
V0 ∗ x/L 0 ≤ x ≤ L
V0 L < x
(A.1)
and shown in Fig. A.1. The exact solution of the Schroedinger equation in this potential in
88
Figure A.1: Ramp potential in standard quantum-mechanical problem. Weset V0 = 0.01eV .
scattering formulation is:
ψ(x) =
eik1x + a ∗ e−ik1x x < 0
b ∗ Ai(x) + c ∗Bi(x) 0 ≤ x ≤ L
d ∗ eik2x L < x
(A.2)
where Ai and Bi are Airy functions, and coefficients a, b, c, d can be determined from the
boundary conditions; momentum on left and right-hand side is k21 = (2m∗/h2) ∗ E and
k22 = (2m∗/h2) ∗ (E − U). For m∗ we use the free electron mass, and we’ll set V0 = 0.01eV .
The problem features characteristic length and energy scales V0 and L, and natural units
of energy and length are l0 = (h2V0/2m∗L)−1/3 and e0 = (V0/L)2/3 ∗ (2m∗/h2)1/3. Defining
the dimensionless quantities λ = L/l0, ε = E/e0 and
α = −i ∗ k2 ∗Bi(λ− ε)− 1/l0 ∗Bi′(λ− ε)
i ∗ k2 ∗ Ai(λ− ε)− 1/l0 ∗ Ai′(λ− ε)(A.3)
to find transmission coefficient we need only amplitude
d =2ik1e
−i∗k2∗L ∗ (α ∗ Ai(λ− ε) +Bi(λ− ε))
(α ∗ (i ∗ k1 ∗ Ai(ε) + 1/l0 ∗ Ai′(ε)) + i ∗ k1 ∗Bi(−ε) + 1/l0 ∗Bi′(−ε))(A.4)
where Ai′ and Bi′ are the derivatives of Airy functions. We can now find the transmission
coefficient as T (E) = k2/k1 ∗ |d|2 and the reflection coefficients as R(E) = 1− T (E). We’ll
concentrate on the reflection in this example, since that is the process that corresponds to
the Andreev reflection in clean contact which dominates the trnasport in N-SC junctions.
The result of this calculation is shown in Fig. A.2. For the same size of the barrier height
89
Figure A.2: The reflection coefficient of a ramp potential for U = 0.01eV , andvalues of L = 0, 10, 20, 40, 80, 160, 320, 640A (descending curves).
(V0 = 0.01eV ), and energies E > V0 reflection coefficient gets smaller as we increase the
length scale over which the potential sets in (i.e. as we decrease the slope of the ramp). In
the limit L→∞, R = 0 even for E → V0 +0. Therefore in the Andreev problem, we expect
that inclusion of the finite gap onset lenght should decrease excess conductance above the
gap.
A.2 Numerical Results and Comparison of the Solutions
We now implement the algorithm given in Chapter 2. We divide region 2 in n segments of
the length x0 = L/n with the constant potential in each segment (Fig. A.3):
V (x) =
0 x < 0
V0 ∗m ∗ x0/L (m− 1)x0 ≤ x ≤ m ∗ x0, m = 1, n− 1
V0 L < x
(A.5)
and solutions are
90
Figure A.3: A numerical approximation to the real potential form Fig. A.1(steps), and the ramp potential (straight line), for n = 10 steps.
ψ(x) =
eik0x + a ∗ e−ik0x x < 0
bm ∗ eikmx + cm ∗ e−ikmx (m− 1) ∗ x0 ≤ x ≤ m ∗ x0, m = 1, n− 1
d ∗ eik(m+1)x L < x
(A.6)
with momentum in m-th segment given by k2m = (2m∗/h2) ∗ (E − U ∗m/n).
Amplitudes a, bm, cm and d have obvious physical meaning:
• a - an amplitude for the reflection off the barrier
• d - an amplitude for the transmision through the barrier
• bm - an amplitude for the left moving solution in m-th segment
• cm - an amplitude for the right-moving solution in m-th segment
To find these amplitudes we impose the usual boundary conditions:
for x < L
1 + a = b1 + c1
ik0 − ik0a = ik1b1 − ik1c1
for m = 1, n− 1
bmeikmx0m + cme
−ikmx0m = bm+1eikm+1x0m + cm+1e
−ikm+1x0m
ikmbmeikmx0m − ikmcme
−ikmx0m = ikm+1bm+1eikm+1x0m − ikm+1cm+1e
−ikm+1x0m
for L < x
bn−1eikn−1L + cn−1e
−ikn−1L = deiknL
ikn−1cn−1eikn−1L − ikn−1dn−1e
−ikn−1L = ikndeiknL
(A.7)
91
Figure A.4: Fitting the conductance on the energy scale of a gap. Full line -the exact solution of the ramp potential problem, dots - the numerical solution.U=0.01eV, L=10A (upper curve) and L=320A (lower curve)
This is ordinary system of 2(n+ 1) equations and 2(n+ 1) unknowns:
0BBBBBBBBBBBBBBBBBBBB@
1 −1 −1 0 · · ·
−ik0 −ik1 ik1 0 · · ·
· · · · · ·
· · · eikmx0m e−ikmx0m −eikm+1x0m −e
−ikm+1x0m · · ·
· · · ikmeikmx0m −ikme−ikmx0m −ikm+1eikm+1x0m
ikm+1e−ikm+1x0m · · ·
· · · · · ·
· · · 0 eikn−1L
e−ikn−1L −eiknL
· · · 0 ikn−1eikn−1L −ikn−1e
−ikn−1L −ikneiknL
1CCCCCCCCCCCCCCCCCCCCA
0BBBBBBBBBBBBBBBBBBBBBBBB@
a
b1
.
.
.
bm
cm
.
.
.
cn
d
1CCCCCCCCCCCCCCCCCCCCCCCCA
=
0BBBBBBBBBBBBBBBBBBBBBBBB@
−1
−ik0
.
.
.
0
0
.
.
.
0
0
1CCCCCCCCCCCCCCCCCCCCCCCCA
We solve for transmision amplitude d, which we use to calculate conductance as we did in
the previous section.
Results of the calculation are given in Fig. A.4 and Fig. A.5. The fit is perfect. Note that
numerical solution captures even the small oscilations above the gap, with the amplitude two
times smaller than the primary effect - these are characteristics of this particular functional
form of the barrier we chose.
It’s easy to check the convergence of the process by ploting several conductance curves for
various size of l. It’s clear that the process converges rather quickly. While it is in principle
possible to devise numerical limit to the size of the segment for desired accuracy, we shall
utilize the convergence check to determine the maximum segment size. All the results shown
henceforth are well inside the convergence limits.
92
Figure A.5: Fitting the conductance on a very small scale - energy axis isoffset so that gap energy is at zero. Note that R-axis shows details smallerthan Fig. A.4. Full line - the exact solution, dots - the numerical solution.U=0.01eV, L=320A
93
Appendix B
Basic Quasiclassical Equations
A quasiclassical propagator is a matrix with the single particle propagators g on the diagonal,
and the pair correlation function f at the off-daigonal position:
g(k, z; εn) =
g(k, z; εn) f(k, z; εn)
f(k, z; εn) g(k, z; εn)
(B.1)
It satisfies the Eilenberger equation, obtained by applying the quasiclassical approximation
on Gorkov propagator and Gorkov equation - in effect integrating out the fast oscillating
degree of freedom (length scale 1/kF ):[iεnτ3 − ∆(k, z), g(k, z; εn)
]+ ivF (kz)
d
dzg(k, z; εn) = 0 (B.2)
We define
dN = g(kN , 0−; εn)− g(ˆkN , 0−; εn) (B.3)
sN = g(kN , 0−; εn) + g(ˆkN , 0−; εn)
with
k = k− 2zkz (B.4)
with the corresponding equations forN ↔ S (where s and d are defined with 0+ in argument).
The boundary condition for a speculary reflecting wall at x = −a:
g(kN ,−a; εn) = g(ˆkN ,−a; εn) (B.5)
94
And for the contact interface between SC and N metal we have:
dN = dS (B.6)
−iπ1−R
1 +R
[sS
(1− idS/2π
), sN
]= dS (sS)2
and similarly for N ↔ S.
The normalization is chosen so that the bulk value of the gap is acheved in the self-
consistency equation:
g(k, z; εn)2 = −π21 (B.7)
Symmetry relations simplify the solution:
g(k, z; εn) = −g+(−k, z; εn) = −g+(ˆk, z; εn) (B.8)
In particular, for the system with particle-hole symmetry:
g(k, z; εn) = −g(k, z; εn) (B.9)
The self-consistency condition reads:
∆(z) =2T∑
n
∫dΩk/(4π)g(k, z; εn)1,2
ln (T/Tc(z)) +∑
n 1/(n− 1/2)(B.10)
Thus by solving the Eilenberger equation for each component of the matrix separately,
using the symmetry relations, we get two coupled linear differential equations. The initial
values of g and f are known, being just the bulk SC values. Starting from these values at
point z0, we calculate the derivatives ∂zg and ∂zf , which we use to calculate new values
g1(z0 + ∆z) = g0(z0) + ∂zg0∆z + (∂g0/∂f0)∂zf0∆z).
In bulk SC:
g(k, z; iεn) =−π√
ε2n +∣∣∣∆(k)
∣∣∣2 iεn −∆(k)
∆+(k) −iεn
(B.11)
95
Appendix C
Definition and Calculation of Gap
If we assume a point-like interaction, and zero-spin pairs, the gap is given by:
∆(r) = V 〈ψ↓(r)ψ↑(r)〉 (C.1)
We express ψ in terms of Bogoliubov operators γ and γ+:
∆(r) = V
⟨ ∑Ek,El>0
(uk↓(r)γk + v∗k↓(r)γ+k )(ul↑(r)γl + v∗l↑(r)γ
+l )
⟩(C.2)
Using 〈γkγ+l 〉 = δk,lf(Ek), where f is Fermi occupation factor, we get:
∆(r) = V∑Ek>0
(uk↑(r)v∗k↓(r) (1− f(Ek)) + uk↓(r)v
∗k↑(r)f(Ek) (C.3)
We express the occupation factors in terms of sum over Matsubara frequencies:
f(Ek) =1
1 + eβEk=
1
β
∑ωn
1
iωn − Ek
(C.4)
where Matsubara frequencies are given by ωn = π(2 ∗ n + 1)/β and β = 1/kBT . Finally, in
the second term we change the summation variable Ek → −Ek to get summation over all
energies (positive and negative)
∆(r) =1
βV∑ωn
∑k
uk↑(r)v∗k↓(r)
iωn − Ek
(C.5)
In practice, both sums will have a high-energy cutoff ωc. In terms of Gorkov’s Green’s
functions, this is just an off-diagonal element:
∆(r) =1
βV∑ωn
G(r, r; iωn)1,2 (C.6)
96
and similar equation is valid for Eilenberger’s function:
∆(r) =πN(0)V
2β
∑ωn
∫dθ sin θ(g(z; iωn)++ + g(z; iωn)−−)1,2 (C.7)
where g++ and g−− correspond to product states of eR and hL (++) and eL and hR (−−)
in terms of language of AppendixB. To express everything in the terms of the measurable
quantities, we substitute:
1
N(0)V= log
T
Tc
+
ωc/2πT∑n=0
1
n+ 1/2(C.8)
which eliminates N(0)V and introduces measurable quantity Tc.
97
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