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28
29 \begin{document}
30
31 \title{Simulating interfacial thermal conductance at metal-solvent
32 interfaces: the role of chemical capping agents}
33
34 \author{Shenyu Kuang and J. Daniel
35 Gezelter\footnote{Corresponding author. \ Electronic mail: gezelter@nd.edu} \\
36 Department of Chemistry and Biochemistry,\\
37 University of Notre Dame\\
38 Notre Dame, Indiana 46556}
39
40 \date{\today}
41
42 \maketitle
43
44 \begin{doublespace}
45
46 \begin{abstract}
47
48 With the Non-Isotropic Velocity Scaling algorithm (NIVS) we have
49 developed, an unphysical thermal flux can be effectively set up even
50 for non-homogeneous systems like interfaces in non-equilibrium
51 molecular dynamics simulations. In this work, this algorithm is
52 applied for simulating thermal conductance at metal / organic solvent
53 interfaces with various coverages of butanethiol capping
54 agents. Different solvents and force field models were tested. Our
55 results suggest that the United-Atom models are able to provide an
56 estimate of the interfacial thermal conductivity comparable to
57 experiments in our simulations with satisfactory computational
58 efficiency. From our results, the acoustic impedance mismatch between
59 metal and liquid phase is effectively reduced by the capping
60 agents, and thus leads to interfacial thermal conductance
61 enhancement. Furthermore, this effect is closely related to the
62 capping agent coverage on the metal surfaces and the type of solvent
63 molecules, and is affected by the models used in the simulations.
64
65 \end{abstract}
66
67 \newpage
68
69 %\narrowtext
70
71 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
72 % BODY OF TEXT
73 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
74
75 \section{Introduction}
76 Interfacial thermal conductance is extensively studied both
77 experimentally and computationally\cite{cahill:793}, due to its
78 importance in nanoscale science and technology. Reliability of
79 nanoscale devices depends on their thermal transport
80 properties. Unlike bulk homogeneous materials, nanoscale materials
81 features significant presence of interfaces, and these interfaces
82 could dominate the heat transfer behavior of these
83 materials. Furthermore, these materials are generally heterogeneous,
84 which challenges traditional research methods for homogeneous
85 systems.
86
87 Heat conductance of molecular and nano-scale interfaces will be
88 affected by the chemical details of the surface. Experimentally,
89 various interfaces have been investigated for their thermal
90 conductance properties. Wang {\it et al.} studied heat transport
91 through long-chain hydrocarbon monolayers on gold substrate at
92 individual molecular level\cite{Wang10082007}; Schmidt {\it et al.}
93 studied the role of CTAB on thermal transport between gold nanorods
94 and solvent\cite{doi:10.1021/jp8051888}; Juv\'e {\it et al.} studied
95 the cooling dynamics, which is controlled by thermal interface
96 resistence of glass-embedded metal
97 nanoparticles\cite{PhysRevB.80.195406}. Although interfaces are
98 commonly barriers for heat transport, Alper {\it et al.} suggested
99 that specific ligands (capping agents) could completely eliminate this
100 barrier ($G\rightarrow\infty$)\cite{doi:10.1021/la904855s}.
101
102 Theoretical and computational models have also been used to study the
103 interfacial thermal transport in order to gain an understanding of
104 this phenomena at the molecular level. Recently, Hase and coworkers
105 employed Non-Equilibrium Molecular Dynamics (NEMD) simulations to
106 study thermal transport from hot Au(111) substrate to a self-assembled
107 monolayer of alkylthiol with relatively long chain (8-20 carbon
108 atoms)\cite{hase:2010,hase:2011}. However, ensemble averaged
109 measurements for heat conductance of interfaces between the capping
110 monolayer on Au and a solvent phase has yet to be studied.
111 The comparatively low thermal flux through interfaces is
112 difficult to measure with Equilibrium MD or forward NEMD simulation
113 methods. Therefore, the Reverse NEMD (RNEMD)
114 methods\cite{MullerPlathe:1997xw} would have the advantage of having
115 this difficult to measure flux known when studying the thermal
116 transport across interfaces, given that the simulation methods being
117 able to effectively apply an unphysical flux in non-homogeneous
118 systems. Garde and coworkers\cite{garde:nl2005,garde:PhysRevLett2009}
119 applied this approach to various liquid interfaces and studied how
120 thermal conductance (or resistance) is dependent on chemistry details
121 of interfaces, e.g. hydrophobic and hydrophilic aqueous interfaces.
122
123 Recently, we have developed the Non-Isotropic Velocity Scaling (NIVS)
124 algorithm for RNEMD simulations\cite{kuang:164101}. This algorithm
125 retains the desirable features of RNEMD (conservation of linear
126 momentum and total energy, compatibility with periodic boundary
127 conditions) while establishing true thermal distributions in each of
128 the two slabs. Furthermore, it allows effective thermal exchange
129 between particles of different identities, and thus makes the study of
130 interfacial conductance much simpler.
131
132 The work presented here deals with the Au(111) surface covered to
133 varying degrees by butanethiol, a capping agent with short carbon
134 chain, and solvated with organic solvents of different molecular
135 properties. Different models were used for both the capping agent and
136 the solvent force field parameters. Using the NIVS algorithm, the
137 thermal transport across these interfaces was studied and the
138 underlying mechanism for the phenomena was investigated.
139
140 [MAY ADD WHY STUDY AU-THIOL SURFACE; CITE SHAOYI JIANG]
141
142 \section{Methodology}
143 \subsection{Imposd-Flux Methods in MD Simulations}
144 Steady state MD simulations has the advantage that not many
145 trajectories are needed to study the relationship between thermal flux
146 and thermal gradients. For systems including low conductance
147 interfaces one must have a method capable of generating or measuring
148 relatively small fluxes, compared to those required for bulk
149 conductivity. This requirement makes the calculation even more
150 difficult for those slowly-converging equilibrium
151 methods\cite{Viscardy:2007lq}. Forward methods may impose gradient,
152 but in interfacial conditions it is not clear what behavior to impose
153 at the interfacial boundaries. Imposed-flux reverse non-equilibrium
154 methods\cite{MullerPlathe:1997xw} have the flux set {\it a priori} and
155 the thermal response becomes easier to measure than the flux. Although
156 M\"{u}ller-Plathe's original momentum swapping approach can be used
157 for exchanging energy between particles of different identity, the
158 kinetic energy transfer efficiency is affected by the mass difference
159 between the particles, which limits its application on heterogeneous
160 interfacial systems.
161
162 The non-isotropic velocity scaling (NIVS)\cite{kuang:164101} approach to
163 non-equilibrium MD simulations is able to impose a wide range of
164 kinetic energy fluxes without obvious perturbation to the velocity
165 distributions of the simulated systems. Furthermore, this approach has
166 the advantage in heterogeneous interfaces in that kinetic energy flux
167 can be applied between regions of particles of arbitary identity, and
168 the flux will not be restricted by difference in particle mass.
169
170 The NIVS algorithm scales the velocity vectors in two separate regions
171 of a simulation system with respective diagonal scaling matricies. To
172 determine these scaling factors in the matricies, a set of equations
173 including linear momentum conservation and kinetic energy conservation
174 constraints and target energy flux satisfaction is solved. With the
175 scaling operation applied to the system in a set frequency, bulk
176 temperature gradients can be easily established, and these can be used
177 for computing thermal conductivities. The NIVS algorithm conserves
178 momenta and energy and does not depend on an external thermostat.
179
180 \subsection{Defining Interfacial Thermal Conductivity $G$}
181 Given a system with thermal gradients and the corresponding thermal
182 flux, for interfaces with a relatively low interfacial conductance,
183 the bulk regions on either side of an interface rapidly come to a
184 state in which the two phases have relatively homogeneous (but
185 distinct) temperatures. The interfacial thermal conductivity $G$ can
186 therefore be approximated as:
187 \begin{equation}
188 G = \frac{E_{total}}{2 t L_x L_y \left( \langle T_\mathrm{hot}\rangle -
189 \langle T_\mathrm{cold}\rangle \right)}
190 \label{lowG}
191 \end{equation}
192 where ${E_{total}}$ is the imposed non-physical kinetic energy
193 transfer and ${\langle T_\mathrm{hot}\rangle}$ and ${\langle
194 T_\mathrm{cold}\rangle}$ are the average observed temperature of the
195 two separated phases.
196
197 When the interfacial conductance is {\it not} small, there are two
198 ways to define $G$.
199
200 One way is to assume the temperature is discrete on the two sides of
201 the interface. $G$ can be calculated using the applied thermal flux
202 $J$ and the maximum temperature difference measured along the thermal
203 gradient max($\Delta T$), which occurs at the Gibbs deviding surface
204 (Figure \ref{demoPic}):
205 \begin{equation}
206 G=\frac{J}{\Delta T}
207 \label{discreteG}
208 \end{equation}
209
210 \begin{figure}
211 \includegraphics[width=\linewidth]{method}
212 \caption{Interfacial conductance can be calculated by applying an
213 (unphysical) kinetic energy flux between two slabs, one located
214 within the metal and another on the edge of the periodic box. The
215 system responds by forming a thermal response or a gradient. In
216 bulk liquids, this gradient typically has a single slope, but in
217 interfacial systems, there are distinct thermal conductivity
218 domains. The interfacial conductance, $G$ is found by measuring the
219 temperature gap at the Gibbs dividing surface, or by using second
220 derivatives of the thermal profile.}
221 \label{demoPic}
222 \end{figure}
223
224 The other approach is to assume a continuous temperature profile along
225 the thermal gradient axis (e.g. $z$) and define $G$ at the point where
226 the magnitude of thermal conductivity $\lambda$ change reach its
227 maximum, given that $\lambda$ is well-defined throughout the space:
228 \begin{equation}
229 G^\prime = \Big|\frac{\partial\lambda}{\partial z}\Big|
230 = \Big|\frac{\partial}{\partial z}\left(-J_z\Big/
231 \left(\frac{\partial T}{\partial z}\right)\right)\Big|
232 = |J_z|\Big|\frac{\partial^2 T}{\partial z^2}\Big|
233 \Big/\left(\frac{\partial T}{\partial z}\right)^2
234 \label{derivativeG}
235 \end{equation}
236
237 With the temperature profile obtained from simulations, one is able to
238 approximate the first and second derivatives of $T$ with finite
239 difference methods and thus calculate $G^\prime$.
240
241 In what follows, both definitions have been used for calculation and
242 are compared in the results.
243
244 To compare the above definitions ($G$ and $G^\prime$), we have modeled
245 a metal slab with its (111) surfaces perpendicular to the $z$-axis of
246 our simulation cells. Both with and without capping agents on the
247 surfaces, the metal slab is solvated with simple organic solvents, as
248 illustrated in Figure \ref{gradT}.
249
250 With the simulation cell described above, we are able to equilibrate
251 the system and impose an unphysical thermal flux between the liquid
252 and the metal phase using the NIVS algorithm. By periodically applying
253 the unphysical flux, we are able to obtain a temperature profile and
254 its spatial derivatives. These quantities enable the evaluation of the
255 interfacial thermal conductance of a surface. Figure \ref{gradT} is an
256 example of how an applied thermal flux can be used to obtain the 1st
257 and 2nd derivatives of the temperature profile.
258
259 \begin{figure}
260 \includegraphics[width=\linewidth]{gradT}
261 \caption{A sample of Au-butanethiol/hexane interfacial system and the
262 temperature profile after a kinetic energy flux is imposed to
263 it. The 1st and 2nd derivatives of the temperature profile can be
264 obtained with finite difference approximation (lower panel).}
265 \label{gradT}
266 \end{figure}
267
268 \section{Computational Details}
269 \subsection{Simulation Protocol}
270 The NIVS algorithm has been implemented in our MD simulation code,
271 OpenMD\cite{Meineke:2005gd,openmd}, and was used for our
272 simulations. Different metal slab thickness (layer numbers of Au) was
273 simulated. Metal slabs were first equilibrated under atmospheric
274 pressure (1 atm) and a desired temperature (e.g. 200K). After
275 equilibration, butanethiol capping agents were placed at three-fold
276 hollow sites on the Au(111) surfaces. These sites could be either a
277 {\it fcc} or {\it hcp} site. However, Hase {\it et al.} found that
278 they are equivalent in a heat transfer process\cite{hase:2010}, so
279 they are not distinguished in our study. The maximum butanethiol
280 capacity on Au surface is $1/3$ of the total number of surface Au
281 atoms, and the packing forms a $(\sqrt{3}\times\sqrt{3})R30^\circ$
282 structure\cite{doi:10.1021/ja00008a001,doi:10.1021/cr9801317}. A
283 series of different coverages was derived by evenly eliminating
284 butanethiols on the surfaces, and was investigated in order to study
285 the relation between coverage and interfacial conductance.
286
287 The capping agent molecules were allowed to migrate during the
288 simulations. They distributed themselves uniformly and sampled a
289 number of three-fold sites throughout out study. Therefore, the
290 initial configuration would not noticeably affect the sampling of a
291 variety of configurations of the same coverage, and the final
292 conductance measurement would be an average effect of these
293 configurations explored in the simulations. [MAY NEED SNAPSHOTS]
294
295 After the modified Au-butanethiol surface systems were equilibrated
296 under canonical ensemble, organic solvent molecules were packed in the
297 previously empty part of the simulation cells\cite{packmol}. Two
298 solvents were investigated, one which has little vibrational overlap
299 with the alkanethiol and a planar shape (toluene), and one which has
300 similar vibrational frequencies and chain-like shape ({\it n}-hexane).
301
302 The space filled by solvent molecules, i.e. the gap between
303 periodically repeated Au-butanethiol surfaces should be carefully
304 chosen. A very long length scale for the thermal gradient axis ($z$)
305 may cause excessively hot or cold temperatures in the middle of the
306 solvent region and lead to undesired phenomena such as solvent boiling
307 or freezing when a thermal flux is applied. Conversely, too few
308 solvent molecules would change the normal behavior of the liquid
309 phase. Therefore, our $N_{solvent}$ values were chosen to ensure that
310 these extreme cases did not happen to our simulations. And the
311 corresponding spacing is usually $35 \sim 75$\AA.
312
313 The initial configurations generated are further equilibrated with the
314 $x$ and $y$ dimensions fixed, only allowing length scale change in $z$
315 dimension. This is to ensure that the equilibration of liquid phase
316 does not affect the metal crystal structure in $x$ and $y$ dimensions.
317 To investigate this effect, comparisons were made with simulations
318 that allow changes of $L_x$ and $L_y$ during NPT equilibration, and
319 the results are shown in later sections. After ensuring the liquid
320 phase reaches equilibrium at atmospheric pressure (1 atm), further
321 equilibration are followed under NVT and then NVE ensembles.
322
323 After the systems reach equilibrium, NIVS is implemented to impose a
324 periodic unphysical thermal flux between the metal and the liquid
325 phase. Most of our simulations are under an average temperature of
326 $\sim$200K. Therefore, this flux usually comes from the metal to the
327 liquid so that the liquid has a higher temperature and would not
328 freeze due to excessively low temperature. After this induced
329 temperature gradient is stablized, the temperature profile of the
330 simulation cell is recorded. To do this, the simulation cell is
331 devided evenly into $N$ slabs along the $z$-axis and $N$ is maximized
332 for highest possible spatial resolution but not too many to have some
333 slabs empty most of the time. The average temperatures of each slab
334 are recorded for 1$\sim$2 ns. When the slab width $d$ of each slab is
335 the same, the derivatives of $T$ with respect to slab number $n$ can
336 be directly used for $G^\prime$ calculations:
337 \begin{equation}
338 G^\prime = |J_z|\Big|\frac{\partial^2 T}{\partial z^2}\Big|
339 \Big/\left(\frac{\partial T}{\partial z}\right)^2
340 = |J_z|\Big|\frac{1}{d^2}\frac{\partial^2 T}{\partial n^2}\Big|
341 \Big/\left(\frac{1}{d}\frac{\partial T}{\partial n}\right)^2
342 = |J_z|\Big|\frac{\partial^2 T}{\partial n^2}\Big|
343 \Big/\left(\frac{\partial T}{\partial n}\right)^2
344 \label{derivativeG2}
345 \end{equation}
346
347 All of the above simulation procedures use a time step of 1 fs. And
348 each equilibration / stabilization step usually takes 100 ps, or
349 longer, if necessary.
350
351 \subsection{Force Field Parameters}
352 Our simulations include various components. Figure \ref{demoMol}
353 demonstrates the sites defined for both United-Atom and All-Atom
354 models of the organic solvent and capping agent molecules in our
355 simulations. Force field parameter descriptions are needed for
356 interactions both between the same type of particles and between
357 particles of different species.
358
359 \begin{figure}
360 \includegraphics[width=\linewidth]{structures}
361 \caption{Structures of the capping agent and solvents utilized in
362 these simulations. The chemically-distinct sites (a-e) are expanded
363 in terms of constituent atoms for both United Atom (UA) and All Atom
364 (AA) force fields. Most parameters are from
365 Refs. \protect\cite{TraPPE-UA.alkanes,TraPPE-UA.alkylbenzenes} (UA) and
366 \protect\cite{OPLSAA} (AA). Cross-interactions with the Au atoms are given
367 in Table \ref{MnM}.}
368 \label{demoMol}
369 \end{figure}
370
371 The Au-Au interactions in metal lattice slab is described by the
372 quantum Sutton-Chen (QSC) formulation\cite{PhysRevB.59.3527}. The QSC
373 potentials include zero-point quantum corrections and are
374 reparametrized for accurate surface energies compared to the
375 Sutton-Chen potentials\cite{Chen90}.
376
377 For both solvent molecules, straight chain {\it n}-hexane and aromatic
378 toluene, United-Atom (UA) and All-Atom (AA) models are used
379 respectively. The TraPPE-UA
380 parameters\cite{TraPPE-UA.alkanes,TraPPE-UA.alkylbenzenes} are used
381 for our UA solvent molecules. In these models, sites are located at
382 the carbon centers for alkyl groups. Bonding interactions, including
383 bond stretches and bends and torsions, were used for intra-molecular
384 sites not separated by more than 3 bonds. Otherwise, for non-bonded
385 interactions, Lennard-Jones potentials are used. [CHECK CITATION]
386
387 By eliminating explicit hydrogen atoms, these models are simple and
388 computationally efficient, while maintains good accuracy. However, the
389 TraPPE-UA for alkanes is known to predict a lower boiling point than
390 experimental values. Considering that after an unphysical thermal flux
391 is applied to a system, the temperature of ``hot'' area in the liquid
392 phase would be significantly higher than the average of the system, to
393 prevent over heating and boiling of the liquid phase, the average
394 temperature in our simulations should be much lower than the liquid
395 boiling point.
396
397 For UA-toluene model, the non-bonded potentials between
398 inter-molecular sites have a similar Lennard-Jones formulation. For
399 intra-molecular interactions, considering the stiffness of the benzene
400 ring, rigid body constraints are applied for further computational
401 efficiency. All bonds in the benzene ring and between the ring and the
402 methyl group remain rigid during the progress of simulations.
403
404 Besides the TraPPE-UA models, AA models for both organic solvents are
405 included in our studies as well. For hexane, the OPLS-AA\cite{OPLSAA}
406 force field is used. Additional explicit hydrogen sites were
407 included. Besides bonding and non-bonded site-site interactions,
408 partial charges and the electrostatic interactions were added to each
409 CT and HC site. For toluene, the United Force Field developed by
410 Rapp\'{e} {\it et al.}\cite{doi:10.1021/ja00051a040} is
411 adopted. Without the rigid body constraints, bonding interactions were
412 included. For the aromatic ring, improper torsions (inversions) were
413 added as an extra potential for maintaining the planar shape.
414 [CHECK CITATION]
415
416 The capping agent in our simulations, the butanethiol molecules can
417 either use UA or AA model. The TraPPE-UA force fields includes
418 parameters for thiol molecules\cite{TraPPE-UA.thiols} and are used for
419 UA butanethiol model in our simulations. The OPLS-AA also provides
420 parameters for alkyl thiols. However, alkyl thiols adsorbed on Au(111)
421 surfaces do not have the hydrogen atom bonded to sulfur. To adapt this
422 change and derive suitable parameters for butanethiol adsorbed on
423 Au(111) surfaces, we adopt the S parameters from Luedtke and
424 Landman\cite{landman:1998}[CHECK CITATION]
425 and modify parameters for its neighbor C
426 atom for charge balance in the molecule. Note that the model choice
427 (UA or AA) of capping agent can be different from the
428 solvent. Regardless of model choice, the force field parameters for
429 interactions between capping agent and solvent can be derived using
430 Lorentz-Berthelot Mixing Rule:
431 \begin{eqnarray}
432 \sigma_{ij} & = & \frac{1}{2} \left(\sigma_{ii} + \sigma_{jj}\right) \\
433 \epsilon_{ij} & = & \sqrt{\epsilon_{ii}\epsilon_{jj}}
434 \end{eqnarray}
435
436 To describe the interactions between metal Au and non-metal capping
437 agent and solvent particles, we refer to an adsorption study of alkyl
438 thiols on gold surfaces by Vlugt {\it et
439 al.}\cite{vlugt:cpc2007154} They fitted an effective Lennard-Jones
440 form of potential parameters for the interaction between Au and
441 pseudo-atoms CH$_x$ and S based on a well-established and widely-used
442 effective potential of Hautman and Klein\cite{hautman:4994} for the
443 Au(111) surface. As our simulations require the gold lattice slab to
444 be non-rigid so that it could accommodate kinetic energy for thermal
445 transport study purpose, the pair-wise form of potentials is
446 preferred.
447
448 Besides, the potentials developed from {\it ab initio} calculations by
449 Leng {\it et al.}\cite{doi:10.1021/jp034405s} are adopted for the
450 interactions between Au and aromatic C/H atoms in toluene. A set of
451 pseudo Lennard-Jones parameters were provided for Au in their force
452 fields. By using the Mixing Rule, this can be used to derive pair-wise
453 potentials for non-bonded interactions between Au and non-metal sites.
454
455 However, the Lennard-Jones parameters between Au and other types of
456 particles, such as All-Atom normal alkanes in our simulations are not
457 yet well-established. For these interactions, we attempt to derive
458 their parameters using the Mixing Rule. To do this, Au pseudo
459 Lennard-Jones parameters for ``Metal-non-Metal'' (MnM) interactions
460 were first extracted from the Au-CH$_x$ parameters by applying the
461 Mixing Rule reversely. Table \ref{MnM} summarizes these ``MnM''
462 parameters in our simulations.
463
464 \begin{table*}
465 \begin{minipage}{\linewidth}
466 \begin{center}
467 \caption{Non-bonded interaction parameters (including cross
468 interactions with Au atoms) for both force fields used in this
469 work.}
470 \begin{tabular}{lllllll}
471 \hline\hline
472 & Site & $\sigma_{ii}$ & $\epsilon_{ii}$ & $q_i$ &
473 $\sigma_{Au-i}$ & $\epsilon_{Au-i}$ \\
474 & & (\AA) & (kcal/mol) & ($e$) & (\AA) & (kcal/mol) \\
475 \hline
476 United Atom (UA)
477 &CH3 & 3.75 & 0.1947 & - & 3.54 & 0.2146 \\
478 &CH2 & 3.95 & 0.0914 & - & 3.54 & 0.1749 \\
479 &CHar & 3.695 & 0.1003 & - & 3.4625 & 0.1680 \\
480 &CRar & 3.88 & 0.04173 & - & 3.555 & 0.1604 \\
481 \hline
482 All Atom (AA)
483 &CT3 & 3.50 & 0.066 & -0.18 & 3.365 & 0.1373 \\
484 &CT2 & 3.50 & 0.066 & -0.12 & 3.365 & 0.1373 \\
485 &CTT & 3.50 & 0.066 & -0.065 & 3.365 & 0.1373 \\
486 &HC & 2.50 & 0.030 & 0.06 & 2.865 & 0.09256 \\
487 &CA & 3.55 & 0.070 & -0.115 & 3.173 & 0.0640 \\
488 &HA & 2.42 & 0.030 & 0.115 & 2.746 & 0.0414 \\
489 \hline
490 Both UA and AA
491 & S & 4.45 & 0.25 & - & 2.40 & 8.465 \\
492 \hline\hline
493 \end{tabular}
494 \label{MnM}
495 \end{center}
496 \end{minipage}
497 \end{table*}
498
499 \subsection{Vibrational Spectrum}
500 To investigate the mechanism of interfacial thermal conductance, the
501 vibrational spectrum is utilized as a complementary tool. Vibrational
502 spectra were taken for individual components in different
503 simulations. To obtain these spectra, simulations were run after
504 equilibration, in the NVE ensemble. Snapshots of configurations were
505 collected at a frequency that is higher than that of the fastest
506 vibrations occuring in the simulations. With these configurations, the
507 velocity auto-correlation functions can be computed:
508 \begin{equation}
509 C_A (t) = \langle\vec{v}_A (t)\cdot\vec{v}_A (0)\rangle
510 \label{vCorr}
511 \end{equation}
512 Followed by Fourier transforms, the power spectrum can be constructed:
513 \begin{equation}
514 \hat{f}(\omega) = \int_{-\infty}^{\infty} C_A (t) e^{-2\pi it\omega}\,dt
515 \label{fourier}
516 \end{equation}
517
518 \section{Results and Discussions}
519 In what follows, how the parameters and protocol of simulations would
520 affect the measurement of $G$'s is first discussed. With a reliable
521 protocol and set of parameters, the influence of capping agent
522 coverage on thermal conductance is investigated. Besides, different
523 force field models for both solvents and selected deuterated models
524 were tested and compared. Finally, a summary of the role of capping
525 agent in the interfacial thermal transport process is given.
526
527 \subsection{How Simulation Parameters Affects $G$}
528 We have varied our protocol or other parameters of the simulations in
529 order to investigate how these factors would affect the measurement of
530 $G$'s. It turned out that while some of these parameters would not
531 affect the results substantially, some other changes to the
532 simulations would have a significant impact on the measurement
533 results.
534
535 In some of our simulations, we allowed $L_x$ and $L_y$ to change
536 during equilibrating the liquid phase. Due to the stiffness of the
537 crystalline Au structure, $L_x$ and $L_y$ would not change noticeably
538 after equilibration. Although $L_z$ could fluctuate $\sim$1\% after a
539 system is fully equilibrated in the NPT ensemble, this fluctuation, as
540 well as those of $L_x$ and $L_y$ (which is significantly smaller),
541 would not be magnified on the calculated $G$'s, as shown in Table
542 \ref{AuThiolHexaneUA}. This insensivity to $L_i$ fluctuations allows
543 reliable measurement of $G$'s without the necessity of extremely
544 cautious equilibration process.
545
546 As stated in our computational details, the spacing filled with
547 solvent molecules can be chosen within a range. This allows some
548 change of solvent molecule numbers for the same Au-butanethiol
549 surfaces. We did this study on our Au-butanethiol/hexane
550 simulations. Nevertheless, the results obtained from systems of
551 different $N_{hexane}$ did not indicate that the measurement of $G$ is
552 susceptible to this parameter. For computational efficiency concern,
553 smaller system size would be preferable, given that the liquid phase
554 structure is not affected.
555
556 Our NIVS algorithm allows change of unphysical thermal flux both in
557 direction and in quantity. This feature extends our investigation of
558 interfacial thermal conductance. However, the magnitude of this
559 thermal flux is not arbitary if one aims to obtain a stable and
560 reliable thermal gradient. A temperature profile would be
561 substantially affected by noise when $|J_z|$ has a much too low
562 magnitude; while an excessively large $|J_z|$ that overwhelms the
563 conductance capacity of the interface would prevent a thermal gradient
564 to reach a stablized steady state. NIVS has the advantage of allowing
565 $J$ to vary in a wide range such that the optimal flux range for $G$
566 measurement can generally be simulated by the algorithm. Within the
567 optimal range, we were able to study how $G$ would change according to
568 the thermal flux across the interface. For our simulations, we denote
569 $J_z$ to be positive when the physical thermal flux is from the liquid
570 to metal, and negative vice versa. The $G$'s measured under different
571 $J_z$ is listed in Table \ref{AuThiolHexaneUA} and
572 \ref{AuThiolToluene}. These results do not suggest that $G$ is
573 dependent on $J_z$ within this flux range. The linear response of flux
574 to thermal gradient simplifies our investigations in that we can rely
575 on $G$ measurement with only a couple $J_z$'s and do not need to test
576 a large series of fluxes.
577
578 \begin{table*}
579 \begin{minipage}{\linewidth}
580 \begin{center}
581 \caption{Computed interfacial thermal conductivity ($G$ and
582 $G^\prime$) values for the 100\% covered Au-butanethiol/hexane
583 interfaces with UA model and different hexane molecule numbers
584 at different temperatures using a range of energy
585 fluxes. Error estimates indicated in parenthesis.}
586
587 \begin{tabular}{ccccccc}
588 \hline\hline
589 $\langle T\rangle$ & $N_{hexane}$ & Fixed & $\rho_{hexane}$ &
590 $J_z$ & $G$ & $G^\prime$ \\
591 (K) & & $L_x$ \& $L_y$? & (g/cm$^3$) & (GW/m$^2$) &
592 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
593 \hline
594 200 & 266 & No & 0.672 & -0.96 & 102(3) & 80.0(0.8) \\
595 & 200 & Yes & 0.694 & 1.92 & 129(11) & 87.3(0.3) \\
596 & & Yes & 0.672 & 1.93 & 131(16) & 78(13) \\
597 & & No & 0.688 & 0.96 & 125(16) & 90.2(15) \\
598 & & & & 1.91 & 139(10) & 101(10) \\
599 & & & & 2.83 & 141(6) & 89.9(9.8) \\
600 & 166 & Yes & 0.679 & 0.97 & 115(19) & 69(18) \\
601 & & & & 1.94 & 125(9) & 87.1(0.2) \\
602 & & No & 0.681 & 0.97 & 141(30) & 78(22) \\
603 & & & & 1.92 & 138(4) & 98.9(9.5) \\
604 \hline
605 250 & 200 & No & 0.560 & 0.96 & 75(10) & 61.8(7.3) \\
606 & & & & -0.95 & 49.4(0.3) & 45.7(2.1) \\
607 & 166 & Yes & 0.570 & 0.98 & 79.0(3.5) & 62.9(3.0) \\
608 & & No & 0.569 & 0.97 & 80.3(0.6) & 67(11) \\
609 & & & & 1.44 & 76.2(5.0) & 64.8(3.8) \\
610 & & & & -0.95 & 56.4(2.5) & 54.4(1.1) \\
611 & & & & -1.85 & 47.8(1.1) & 53.5(1.5) \\
612 \hline\hline
613 \end{tabular}
614 \label{AuThiolHexaneUA}
615 \end{center}
616 \end{minipage}
617 \end{table*}
618
619 Furthermore, we also attempted to increase system average temperatures
620 to above 200K. These simulations are first equilibrated in the NPT
621 ensemble under normal pressure. As stated above, the TraPPE-UA model
622 for hexane tends to predict a lower boiling point. In our simulations,
623 hexane had diffculty to remain in liquid phase when NPT equilibration
624 temperature is higher than 250K. Additionally, the equilibrated liquid
625 hexane density under 250K becomes lower than experimental value. This
626 expanded liquid phase leads to lower contact between hexane and
627 butanethiol as well.[MAY NEED SLAB DENSITY FIGURE]
628 And this reduced contact would
629 probably be accountable for a lower interfacial thermal conductance,
630 as shown in Table \ref{AuThiolHexaneUA}.
631
632 A similar study for TraPPE-UA toluene agrees with the above result as
633 well. Having a higher boiling point, toluene tends to remain liquid in
634 our simulations even equilibrated under 300K in NPT
635 ensembles. Furthermore, the expansion of the toluene liquid phase is
636 not as significant as that of the hexane. This prevents severe
637 decrease of liquid-capping agent contact and the results (Table
638 \ref{AuThiolToluene}) show only a slightly decreased interface
639 conductance. Therefore, solvent-capping agent contact should play an
640 important role in the thermal transport process across the interface
641 in that higher degree of contact could yield increased conductance.
642
643 \begin{table*}
644 \begin{minipage}{\linewidth}
645 \begin{center}
646 \caption{Computed interfacial thermal conductivity ($G$ and
647 $G^\prime$) values for a 90\% coverage Au-butanethiol/toluene
648 interface at different temperatures using a range of energy
649 fluxes. Error estimates indicated in parenthesis.}
650
651 \begin{tabular}{ccccc}
652 \hline\hline
653 $\langle T\rangle$ & $\rho_{toluene}$ & $J_z$ & $G$ & $G^\prime$ \\
654 (K) & (g/cm$^3$) & (GW/m$^2$) & \multicolumn{2}{c}{(MW/m$^2$/K)} \\
655 \hline
656 200 & 0.933 & 2.15 & 204(12) & 113(12) \\
657 & & -1.86 & 180(3) & 135(21) \\
658 & & -3.93 & 176(5) & 113(12) \\
659 \hline
660 300 & 0.855 & -1.91 & 143(5) & 125(2) \\
661 & & -4.19 & 135(9) & 113(12) \\
662 \hline\hline
663 \end{tabular}
664 \label{AuThiolToluene}
665 \end{center}
666 \end{minipage}
667 \end{table*}
668
669 Besides lower interfacial thermal conductance, surfaces in relatively
670 high temperatures are susceptible to reconstructions, when
671 butanethiols have a full coverage on the Au(111) surface. These
672 reconstructions include surface Au atoms migrated outward to the S
673 atom layer, and butanethiol molecules embedded into the original
674 surface Au layer. The driving force for this behavior is the strong
675 Au-S interactions in our simulations. And these reconstructions lead
676 to higher ratio of Au-S attraction and thus is energetically
677 favorable. Furthermore, this phenomenon agrees with experimental
678 results\cite{doi:10.1021/j100035a033,doi:10.1021/la026493y}. Vlugt
679 {\it et al.} had kept their Au(111) slab rigid so that their
680 simulations can reach 300K without surface reconstructions. Without
681 this practice, simulating 100\% thiol covered interfaces under higher
682 temperatures could hardly avoid surface reconstructions. However, our
683 measurement is based on assuming homogeneity on $x$ and $y$ dimensions
684 so that measurement of $T$ at particular $z$ would be an effective
685 average of the particles of the same type. Since surface
686 reconstructions could eliminate the original $x$ and $y$ dimensional
687 homogeneity, measurement of $G$ is more difficult to conduct under
688 higher temperatures. Therefore, most of our measurements are
689 undertaken at $\langle T\rangle\sim$200K.
690
691 However, when the surface is not completely covered by butanethiols,
692 the simulated system is more resistent to the reconstruction
693 above. Our Au-butanethiol/toluene system had the Au(111) surfaces 90\%
694 covered by butanethiols, but did not see this above phenomena even at
695 $\langle T\rangle\sim$300K. The empty three-fold sites not occupied by
696 capping agents could help prevent surface reconstruction in that they
697 provide other means of capping agent relaxation. It is observed that
698 butanethiols can migrate to their neighbor empty sites during a
699 simulation. Therefore, we were able to obtain $G$'s for these
700 interfaces even at a relatively high temperature without being
701 affected by surface reconstructions.
702
703 \subsection{Influence of Capping Agent Coverage on $G$}
704 To investigate the influence of butanethiol coverage on interfacial
705 thermal conductance, a series of different coverage Au-butanethiol
706 surfaces is prepared and solvated with various organic
707 molecules. These systems are then equilibrated and their interfacial
708 thermal conductivity are measured with our NIVS algorithm. Figure
709 \ref{coverage} demonstrates the trend of conductance change with
710 respect to different coverages of butanethiol. To study the isotope
711 effect in interfacial thermal conductance, deuterated UA-hexane is
712 included as well.
713
714 \begin{figure}
715 \includegraphics[width=\linewidth]{coverage}
716 \caption{Comparison of interfacial thermal conductivity ($G$) values
717 for the Au-butanethiol/solvent interface with various UA models and
718 different capping agent coverages at $\langle T\rangle\sim$200K
719 using certain energy flux respectively.}
720 \label{coverage}
721 \end{figure}
722
723 It turned out that with partial covered butanethiol on the Au(111)
724 surface, the derivative definition for $G^\prime$
725 (Eq. \ref{derivativeG}) was difficult to apply, due to the difficulty
726 in locating the maximum of change of $\lambda$. Instead, the discrete
727 definition (Eq. \ref{discreteG}) is easier to apply, as the Gibbs
728 deviding surface can still be well-defined. Therefore, $G$ (not
729 $G^\prime$) was used for this section.
730
731 From Figure \ref{coverage}, one can see the significance of the
732 presence of capping agents. Even when a fraction of the Au(111)
733 surface sites are covered with butanethiols, the conductivity would
734 see an enhancement by at least a factor of 3. This indicates the
735 important role cappping agent is playing for thermal transport
736 phenomena on metal / organic solvent surfaces.
737
738 Interestingly, as one could observe from our results, the maximum
739 conductance enhancement (largest $G$) happens while the surfaces are
740 about 75\% covered with butanethiols. This again indicates that
741 solvent-capping agent contact has an important role of the thermal
742 transport process. Slightly lower butanethiol coverage allows small
743 gaps between butanethiols to form. And these gaps could be filled with
744 solvent molecules, which acts like ``heat conductors'' on the
745 surface. The higher degree of interaction between these solvent
746 molecules and capping agents increases the enhancement effect and thus
747 produces a higher $G$ than densely packed butanethiol arrays. However,
748 once this maximum conductance enhancement is reached, $G$ decreases
749 when butanethiol coverage continues to decrease. Each capping agent
750 molecule reaches its maximum capacity for thermal
751 conductance. Therefore, even higher solvent-capping agent contact
752 would not offset this effect. Eventually, when butanethiol coverage
753 continues to decrease, solvent-capping agent contact actually
754 decreases with the disappearing of butanethiol molecules. In this
755 case, $G$ decrease could not be offset but instead accelerated. [NEED
756 SNAPSHOT SHOWING THE PHENOMENA / SLAB DENSITY ANALYSIS]
757
758 A comparison of the results obtained from differenet organic solvents
759 can also provide useful information of the interfacial thermal
760 transport process. The deuterated hexane (UA) results do not appear to
761 be much different from those of normal hexane (UA), given that
762 butanethiol (UA) is non-deuterated for both solvents. These UA model
763 studies, even though eliminating C-H vibration samplings, still have
764 C-C vibrational frequencies different from each other. However, these
765 differences in the infrared range do not seem to produce an observable
766 difference for the results of $G$ (Figure \ref{uahxnua}).
767
768 \begin{figure}
769 \includegraphics[width=\linewidth]{uahxnua}
770 \caption{Vibrational spectra obtained for normal (upper) and
771 deuterated (lower) hexane in Au-butanethiol/hexane
772 systems. Butanethiol spectra are shown as reference. Both hexane and
773 butanethiol were using United-Atom models.}
774 \label{uahxnua}
775 \end{figure}
776
777 Furthermore, results for rigid body toluene solvent, as well as other
778 UA-hexane solvents, are reasonable within the general experimental
779 ranges\cite{Wilson:2002uq,cahill:793,PhysRevB.80.195406}. This
780 suggests that explicit hydrogen might not be a required factor for
781 modeling thermal transport phenomena of systems such as
782 Au-thiol/organic solvent.
783
784 However, results for Au-butanethiol/toluene do not show an identical
785 trend with those for Au-butanethiol/hexane in that $G$ remains at
786 approximately the same magnitue when butanethiol coverage differs from
787 25\% to 75\%. This might be rooted in the molecule shape difference
788 for planar toluene and chain-like {\it n}-hexane. Due to this
789 difference, toluene molecules have more difficulty in occupying
790 relatively small gaps among capping agents when their coverage is not
791 too low. Therefore, the solvent-capping agent contact may keep
792 increasing until the capping agent coverage reaches a relatively low
793 level. This becomes an offset for decreasing butanethiol molecules on
794 its effect to the process of interfacial thermal transport. Thus, one
795 can see a plateau of $G$ vs. butanethiol coverage in our results.
796
797 \subsection{Influence of Chosen Molecule Model on $G$}
798 In addition to UA solvent/capping agent models, AA models are included
799 in our simulations as well. Besides simulations of the same (UA or AA)
800 model for solvent and capping agent, different models can be applied
801 to different components. Furthermore, regardless of models chosen,
802 either the solvent or the capping agent can be deuterated, similar to
803 the previous section. Table \ref{modelTest} summarizes the results of
804 these studies.
805
806 \begin{table*}
807 \begin{minipage}{\linewidth}
808 \begin{center}
809
810 \caption{Computed interfacial thermal conductivity ($G$ and
811 $G^\prime$) values for interfaces using various models for
812 solvent and capping agent (or without capping agent) at
813 $\langle T\rangle\sim$200K. (D stands for deuterated solvent
814 or capping agent molecules; ``Avg.'' denotes results that are
815 averages of simulations under different $J_z$'s. Error
816 estimates indicated in parenthesis.)}
817
818 \begin{tabular}{llccc}
819 \hline\hline
820 Butanethiol model & Solvent & $J_z$ & $G$ & $G^\prime$ \\
821 (or bare surface) & model & (GW/m$^2$) &
822 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
823 \hline
824 UA & UA hexane & Avg. & 131(9) & 87(10) \\
825 & UA hexane(D) & 1.95 & 153(5) & 136(13) \\
826 & AA hexane & Avg. & 131(6) & 122(10) \\
827 & UA toluene & 1.96 & 187(16) & 151(11) \\
828 & AA toluene & 1.89 & 200(36) & 149(53) \\
829 \hline
830 AA & UA hexane & 1.94 & 116(9) & 129(8) \\
831 & AA hexane & Avg. & 442(14) & 356(31) \\
832 & AA hexane(D) & 1.93 & 222(12) & 234(54) \\
833 & UA toluene & 1.98 & 125(25) & 97(60) \\
834 & AA toluene & 3.79 & 487(56) & 290(42) \\
835 \hline
836 AA(D) & UA hexane & 1.94 & 158(25) & 172(4) \\
837 & AA hexane & 1.92 & 243(29) & 191(11) \\
838 & AA toluene & 1.93 & 364(36) & 322(67) \\
839 \hline
840 bare & UA hexane & Avg. & 46.5(3.2) & 49.4(4.5) \\
841 & UA hexane(D) & 0.98 & 43.9(4.6) & 43.0(2.0) \\
842 & AA hexane & 0.96 & 31.0(1.4) & 29.4(1.3) \\
843 & UA toluene & 1.99 & 70.1(1.3) & 65.8(0.5) \\
844 \hline\hline
845 \end{tabular}
846 \label{modelTest}
847 \end{center}
848 \end{minipage}
849 \end{table*}
850
851 To facilitate direct comparison, the same system with differnt models
852 for different components uses the same length scale for their
853 simulation cells. Without the presence of capping agent, using
854 different models for hexane yields similar results for both $G$ and
855 $G^\prime$, and these two definitions agree with eath other very
856 well. This indicates very weak interaction between the metal and the
857 solvent, and is a typical case for acoustic impedance mismatch between
858 these two phases.
859
860 As for Au(111) surfaces completely covered by butanethiols, the choice
861 of models for capping agent and solvent could impact the measurement
862 of $G$ and $G^\prime$ quite significantly. For Au-butanethiol/hexane
863 interfaces, using AA model for both butanethiol and hexane yields
864 substantially higher conductivity values than using UA model for at
865 least one component of the solvent and capping agent, which exceeds
866 the general range of experimental measurement results. This is
867 probably due to the classically treated C-H vibrations in the AA
868 model, which should not be appreciably populated at normal
869 temperatures. In comparison, once either the hexanes or the
870 butanethiols are deuterated, one can see a significantly lower $G$ and
871 $G^\prime$. In either of these cases, the C-H(D) vibrational overlap
872 between the solvent and the capping agent is removed (Figure
873 \ref{aahxntln}). Conclusively, the improperly treated C-H vibration in
874 the AA model produced over-predicted results accordingly. Compared to
875 the AA model, the UA model yields more reasonable results with higher
876 computational efficiency.
877
878 \begin{figure}
879 \includegraphics[width=\linewidth]{aahxntln}
880 \caption{Spectra obtained for All-Atom model Au-butanethil/solvent
881 systems. When butanethiol is deuterated (lower left), its
882 vibrational overlap with hexane would decrease significantly,
883 compared with normal butanethiol (upper left). However, this
884 dramatic change does not apply to toluene as much (right).}
885 \label{aahxntln}
886 \end{figure}
887
888 However, for Au-butanethiol/toluene interfaces, having the AA
889 butanethiol deuterated did not yield a significant change in the
890 measurement results. Compared to the C-H vibrational overlap between
891 hexane and butanethiol, both of which have alkyl chains, that overlap
892 between toluene and butanethiol is not so significant and thus does
893 not have as much contribution to the heat exchange
894 process. Conversely, extra degrees of freedom such as the C-H
895 vibrations could yield higher heat exchange rate between these two
896 phases and result in a much higher conductivity.
897
898 Although the QSC model for Au is known to predict an overly low value
899 for bulk metal gold conductivity\cite{kuang:164101}, our computational
900 results for $G$ and $G^\prime$ do not seem to be affected by this
901 drawback of the model for metal. Instead, our results suggest that the
902 modeling of interfacial thermal transport behavior relies mainly on
903 the accuracy of the interaction descriptions between components
904 occupying the interfaces.
905
906 \subsection{Role of Capping Agent in Interfacial Thermal Conductance}
907 The vibrational spectra for gold slabs in different environments are
908 shown as in Figure \ref{specAu}. Regardless of the presence of
909 solvent, the gold surfaces covered by butanethiol molecules, compared
910 to bare gold surfaces, exhibit an additional peak observed at the
911 frequency of $\sim$170cm$^{-1}$, which is attributed to the S-Au
912 bonding vibration. This vibration enables efficient thermal transport
913 from surface Au layer to the capping agents. Therefore, in our
914 simulations, the Au/S interfaces do not appear major heat barriers
915 compared to the butanethiol / solvent interfaces.
916
917 Simultaneously, the vibrational overlap between butanethiol and
918 organic solvents suggests higher thermal exchange efficiency between
919 these two components. Even exessively high heat transport was observed
920 when All-Atom models were used and C-H vibrations were treated
921 classically. Compared to metal and organic liquid phase, the heat
922 transfer efficiency between butanethiol and organic solvents is closer
923 to that within bulk liquid phase.
924
925 Furthermore, our observation validated previous
926 results\cite{hase:2010} that the intramolecular heat transport of
927 alkylthiols is highly effecient. As a combinational effects of these
928 phenomena, butanethiol acts as a channel to expedite thermal transport
929 process. The acoustic impedance mismatch between the metal and the
930 liquid phase can be effectively reduced with the presence of suitable
931 capping agents.
932
933 \begin{figure}
934 \includegraphics[width=\linewidth]{vibration}
935 \caption{Vibrational spectra obtained for gold in different
936 environments.}
937 \label{specAu}
938 \end{figure}
939
940 [MAY ADD COMPARISON OF AU SLAB WIDTHS]
941
942 \section{Conclusions}
943 The NIVS algorithm we developed has been applied to simulations of
944 Au-butanethiol surfaces with organic solvents. This algorithm allows
945 effective unphysical thermal flux transferred between the metal and
946 the liquid phase. With the flux applied, we were able to measure the
947 corresponding thermal gradient and to obtain interfacial thermal
948 conductivities. Under steady states, single trajectory simulation
949 would be enough for accurate measurement. This would be advantageous
950 compared to transient state simulations, which need multiple
951 trajectories to produce reliable average results.
952
953 Our simulations have seen significant conductance enhancement with the
954 presence of capping agent, compared to the bare gold / liquid
955 interfaces. The acoustic impedance mismatch between the metal and the
956 liquid phase is effectively eliminated by proper capping
957 agent. Furthermore, the coverage precentage of the capping agent plays
958 an important role in the interfacial thermal transport
959 process. Moderately lower coverages allow higher contact between
960 capping agent and solvent, and thus could further enhance the heat
961 transfer process.
962
963 Our measurement results, particularly of the UA models, agree with
964 available experimental data. This indicates that our force field
965 parameters have a nice description of the interactions between the
966 particles at the interfaces. AA models tend to overestimate the
967 interfacial thermal conductance in that the classically treated C-H
968 vibration would be overly sampled. Compared to the AA models, the UA
969 models have higher computational efficiency with satisfactory
970 accuracy, and thus are preferable in interfacial thermal transport
971 modelings. Of the two definitions for $G$, the discrete form
972 (Eq. \ref{discreteG}) was easier to use and gives out relatively
973 consistent results, while the derivative form (Eq. \ref{derivativeG})
974 is not as versatile. Although $G^\prime$ gives out comparable results
975 and follows similar trend with $G$ when measuring close to fully
976 covered or bare surfaces, the spatial resolution of $T$ profile is
977 limited for accurate computation of derivatives data.
978
979 Vlugt {\it et al.} has investigated the surface thiol structures for
980 nanocrystal gold and pointed out that they differs from those of the
981 Au(111) surface\cite{vlugt:cpc2007154}. This difference might lead to
982 change of interfacial thermal transport behavior as well. To
983 investigate this problem, an effective means to introduce thermal flux
984 and measure the corresponding thermal gradient is desirable for
985 simulating structures with spherical symmetry.
986
987 \section{Acknowledgments}
988 Support for this project was provided by the National Science
989 Foundation under grant CHE-0848243. Computational time was provided by
990 the Center for Research Computing (CRC) at the University of Notre
991 Dame. \newpage
992
993 \bibliography{interfacial}
994
995 \end{doublespace}
996 \end{document}
997