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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) methods would have the
114 advantage of having this difficult to measure flux known when studying
115 the thermal transport across interfaces, given that the simulation
116 methods being able to effectively apply an unphysical flux in
117 non-homogeneous systems.
118
119 Recently, we have developed the Non-Isotropic Velocity Scaling (NIVS)
120 algorithm for RNEMD simulations\cite{kuang:164101}. This algorithm
121 retains the desirable features of RNEMD (conservation of linear
122 momentum and total energy, compatibility with periodic boundary
123 conditions) while establishing true thermal distributions in each of
124 the two slabs. Furthermore, it allows effective thermal exchange
125 between particles of different identities, and thus makes the study of
126 interfacial conductance much simpler.
127
128 The work presented here deals with the Au(111) surface covered to
129 varying degrees by butanethiol, a capping agent with short carbon
130 chain, and solvated with organic solvents of different molecular
131 properties. Different models were used for both the capping agent and
132 the solvent force field parameters. Using the NIVS algorithm, the
133 thermal transport across these interfaces was studied and the
134 underlying mechanism for this phenomena was investigated.
135
136 [MAY ADD WHY STUDY AU-THIOL SURFACE; CITE SHAOYI JIANG]
137
138 \section{Methodology}
139 \subsection{Imposd-Flux Methods in MD Simulations}
140 For systems with low interfacial conductivity one must have a method
141 capable of generating relatively small fluxes, compared to those
142 required for bulk conductivity. This requirement makes the calculation
143 even more difficult for those slowly-converging equilibrium
144 methods\cite{Viscardy:2007lq}.
145 Forward methods impose gradient, but in interfacail conditions it is
146 not clear what behavior to impose at the boundary...
147 Imposed-flux reverse non-equilibrium
148 methods\cite{MullerPlathe:1997xw} have the flux set {\it a priori} and
149 the thermal response becomes easier to
150 measure than the flux. Although M\"{u}ller-Plathe's original momentum
151 swapping approach can be used for exchanging energy between particles
152 of different identity, the kinetic energy transfer efficiency is
153 affected by the mass difference between the particles, which limits
154 its application on heterogeneous interfacial systems.
155
156 The non-isotropic velocity scaling (NIVS)\cite{kuang:164101} approach to
157 non-equilibrium MD simulations is able to impose a wide range of
158 kinetic energy fluxes without obvious perturbation to the velocity
159 distributions of the simulated systems. Furthermore, this approach has
160 the advantage in heterogeneous interfaces in that kinetic energy flux
161 can be applied between regions of particles of arbitary identity, and
162 the flux will not be restricted by difference in particle mass.
163
164 The NIVS algorithm scales the velocity vectors in two separate regions
165 of a simulation system with respective diagonal scaling matricies. To
166 determine these scaling factors in the matricies, a set of equations
167 including linear momentum conservation and kinetic energy conservation
168 constraints and target energy flux satisfaction is solved. With the
169 scaling operation applied to the system in a set frequency, bulk
170 temperature gradients can be easily established, and these can be used
171 for computing thermal conductivities. The NIVS algorithm conserves
172 momenta and energy and does not depend on an external thermostat.
173
174 \subsection{Defining Interfacial Thermal Conductivity $G$}
175 For interfaces with a relatively low interfacial conductance, the bulk
176 regions on either side of an interface rapidly come to a state in
177 which the two phases have relatively homogeneous (but distinct)
178 temperatures. The interfacial thermal conductivity $G$ can therefore
179 be approximated as:
180 \begin{equation}
181 G = \frac{E_{total}}{2 t L_x L_y \left( \langle T_\mathrm{hot}\rangle -
182 \langle T_\mathrm{cold}\rangle \right)}
183 \label{lowG}
184 \end{equation}
185 where ${E_{total}}$ is the imposed non-physical kinetic energy
186 transfer and ${\langle T_\mathrm{hot}\rangle}$ and ${\langle
187 T_\mathrm{cold}\rangle}$ are the average observed temperature of the
188 two separated phases.
189
190 When the interfacial conductance is {\it not} small, there are two
191 ways to define $G$.
192
193 One way is to assume the temperature is discrete on the two sides of
194 the interface. $G$ can be calculated using the applied thermal flux
195 $J$ and the maximum temperature difference measured along the thermal
196 gradient max($\Delta T$), which occurs at the Gibbs deviding surface,
197 as:
198 \begin{equation}
199 G=\frac{J}{\Delta T}
200 \label{discreteG}
201 \end{equation}
202
203 The other approach is to assume a continuous temperature profile along
204 the thermal gradient axis (e.g. $z$) and define $G$ at the point where
205 the magnitude of thermal conductivity $\lambda$ change reach its
206 maximum, given that $\lambda$ is well-defined throughout the space:
207 \begin{equation}
208 G^\prime = \Big|\frac{\partial\lambda}{\partial z}\Big|
209 = \Big|\frac{\partial}{\partial z}\left(-J_z\Big/
210 \left(\frac{\partial T}{\partial z}\right)\right)\Big|
211 = |J_z|\Big|\frac{\partial^2 T}{\partial z^2}\Big|
212 \Big/\left(\frac{\partial T}{\partial z}\right)^2
213 \label{derivativeG}
214 \end{equation}
215
216 With the temperature profile obtained from simulations, one is able to
217 approximate the first and second derivatives of $T$ with finite
218 difference methods and thus calculate $G^\prime$.
219
220 In what follows, both definitions have been used for calculation and
221 are compared in the results.
222
223 To compare the above definitions ($G$ and $G^\prime$), we have modeled
224 a metal slab with its (111) surfaces perpendicular to the $z$-axis of
225 our simulation cells. Both with and withour capping agents on the
226 surfaces, the metal slab is solvated with simple organic solvents, as
227 illustrated in Figure \ref{demoPic}.
228
229 \begin{figure}
230 \includegraphics[width=\linewidth]{method}
231 \caption{Interfacial conductance can be calculated by applying an
232 (unphysical) kinetic energy flux between two slabs, one located
233 within the metal and another on the edge of the periodic box. The
234 system responds by forming a thermal response or a gradient. In
235 bulk liquids, this gradient typically has a single slope, but in
236 interfacial systems, there are distinct thermal conductivity
237 domains. The interfacial conductance, $G$ is found by measuring the
238 temperature gap at the Gibbs dividing surface, or by using second
239 derivatives of the thermal profile.}
240 \label{demoPic}
241 \end{figure}
242
243 With the simulation cell described above, we are able to equilibrate
244 the system and impose an unphysical thermal flux between the liquid
245 and the metal phase using the NIVS algorithm. By periodically applying
246 the unphysical flux, we are able to obtain a temperature profile and
247 its spatial derivatives. These quantities enable the evaluation of the
248 interfacial thermal conductance of a surface. Figure \ref{gradT} is an
249 example how those applied thermal fluxes can be used to obtain the 1st
250 and 2nd derivatives of the temperature profile.
251
252 \begin{figure}
253 \includegraphics[width=\linewidth]{gradT}
254 \caption{The 1st and 2nd derivatives of temperature profile can be
255 obtained with finite difference approximation.}
256 \label{gradT}
257 \end{figure}
258
259 \section{Computational Details}
260 \subsection{Simulation Protocol}
261 The NIVS algorithm has been implemented in our MD simulation code,
262 OpenMD\cite{Meineke:2005gd,openmd}, and was used for our
263 simulations. Different slab thickness (layer numbers of Au) were
264 simulated. Metal slabs were first equilibrated under atmospheric
265 pressure (1 atm) and a desired temperature (e.g. 200K). After
266 equilibration, butanethiol capping agents were placed at three-fold
267 sites on the Au(111) surfaces. The maximum butanethiol capacity on Au
268 surface is $1/3$ of the total number of surface Au
269 atoms\cite{vlugt:cpc2007154}. A series of different coverages was
270 investigated in order to study the relation between coverage and
271 interfacial conductance.
272
273 The capping agent molecules were allowed to migrate during the
274 simulations. They distributed themselves uniformly and sampled a
275 number of three-fold sites throughout out study. Therefore, the
276 initial configuration would not noticeably affect the sampling of a
277 variety of configurations of the same coverage, and the final
278 conductance measurement would be an average effect of these
279 configurations explored in the simulations. [MAY NEED FIGURES]
280
281 After the modified Au-butanethiol surface systems were equilibrated
282 under canonical ensemble, organic solvent molecules were packed in the
283 previously empty part of the simulation cells\cite{packmol}. Two
284 solvents were investigated, one which has little vibrational overlap
285 with the alkanethiol and a planar shape (toluene), and one which has
286 similar vibrational frequencies and chain-like shape ({\it n}-hexane).
287
288 The space filled by solvent molecules, i.e. the gap between
289 periodically repeated Au-butanethiol surfaces should be carefully
290 chosen. A very long length scale for the thermal gradient axis ($z$)
291 may cause excessively hot or cold temperatures in the middle of the
292 solvent region and lead to undesired phenomena such as solvent boiling
293 or freezing when a thermal flux is applied. Conversely, too few
294 solvent molecules would change the normal behavior of the liquid
295 phase. Therefore, our $N_{solvent}$ values were chosen to ensure that
296 these extreme cases did not happen to our simulations. And the
297 corresponding spacing is usually $35 \sim 60$\AA.
298
299 The initial configurations generated by Packmol are further
300 equilibrated with the $x$ and $y$ dimensions fixed, only allowing
301 length scale change in $z$ dimension. This is to ensure that the
302 equilibration of liquid phase does not affect the metal crystal
303 structure in $x$ and $y$ dimensions. Further equilibration are run
304 under NVT and then NVE ensembles.
305
306 After the systems reach equilibrium, NIVS is implemented to impose a
307 periodic unphysical thermal flux between the metal and the liquid
308 phase. Most of our simulations are under an average temperature of
309 $\sim$200K. Therefore, this flux usually comes from the metal to the
310 liquid so that the liquid has a higher temperature and would not
311 freeze due to excessively low temperature. This induced temperature
312 gradient is stablized and the simulation cell is devided evenly into
313 N slabs along the $z$-axis and the temperatures of each slab are
314 recorded. When the slab width $d$ of each slab is the same, the
315 derivatives of $T$ with respect to slab number $n$ can be directly
316 used for $G^\prime$ calculations:
317 \begin{equation}
318 G^\prime = |J_z|\Big|\frac{\partial^2 T}{\partial z^2}\Big|
319 \Big/\left(\frac{\partial T}{\partial z}\right)^2
320 = |J_z|\Big|\frac{1}{d^2}\frac{\partial^2 T}{\partial n^2}\Big|
321 \Big/\left(\frac{1}{d}\frac{\partial T}{\partial n}\right)^2
322 = |J_z|\Big|\frac{\partial^2 T}{\partial n^2}\Big|
323 \Big/\left(\frac{\partial T}{\partial n}\right)^2
324 \label{derivativeG2}
325 \end{equation}
326
327 \subsection{Force Field Parameters}
328 Our simulations include various components. Therefore, force field
329 parameter descriptions are needed for interactions both between the
330 same type of particles and between particles of different species.
331
332 The Au-Au interactions in metal lattice slab is described by the
333 quantum Sutton-Chen (QSC) formulation\cite{PhysRevB.59.3527}. The QSC
334 potentials include zero-point quantum corrections and are
335 reparametrized for accurate surface energies compared to the
336 Sutton-Chen potentials\cite{Chen90}.
337
338 Figure \ref{demoMol} demonstrates how we name our pseudo-atoms of the
339 organic solvent molecules in our simulations.
340
341 \begin{figure}
342 \includegraphics[width=\linewidth]{structures}
343 \caption{Structures of the capping agent and solvents utilized in
344 these simulations. The chemically-distinct sites (a-e) are expanded
345 in terms of constituent atoms for both United Atom (UA) and All Atom
346 (AA) force fields. Most parameters are from
347 Refs. \protect\cite{TraPPE-UA.alkanes,TraPPE-UA.alkylbenzenes} (UA) and
348 \protect\cite{OPLSAA} (AA). Cross-interactions with the Au atoms are given
349 in Table \ref{MnM}.}
350 \label{demoMol}
351 \end{figure}
352
353 For both solvent molecules, straight chain {\it n}-hexane and aromatic
354 toluene, United-Atom (UA) and All-Atom (AA) models are used
355 respectively. The TraPPE-UA
356 parameters\cite{TraPPE-UA.alkanes,TraPPE-UA.alkylbenzenes} are used
357 for our UA solvent molecules. In these models, pseudo-atoms are
358 located at the carbon centers for alkyl groups. By eliminating
359 explicit hydrogen atoms, these models are simple and computationally
360 efficient, while maintains good accuracy. However, the TraPPE-UA for
361 alkanes is known to predict a lower boiling point than experimental
362 values. Considering that after an unphysical thermal flux is applied
363 to a system, the temperature of ``hot'' area in the liquid phase would be
364 significantly higher than the average, to prevent over heating and
365 boiling of the liquid phase, the average temperature in our
366 simulations should be much lower than the liquid boiling point. [MORE DISCUSSION]
367 For UA-toluene model, rigid body constraints are applied, so that the
368 benzene ring and the methyl-CRar bond are kept rigid. This would save
369 computational time.[MORE DETAILS]
370
371 Besides the TraPPE-UA models, AA models for both organic solvents are
372 included in our studies as well. For hexane, the OPLS-AA\cite{OPLSAA}
373 force field is used. [MORE DETAILS]
374 For toluene, the United Force Field developed by Rapp\'{e} {\it et
375 al.}\cite{doi:10.1021/ja00051a040} is adopted.[MORE DETAILS]
376
377 The capping agent in our simulations, the butanethiol molecules can
378 either use UA or AA model. The TraPPE-UA force fields includes
379 parameters for thiol molecules\cite{TraPPE-UA.thiols} and are used for
380 UA butanethiol model in our simulations. The OPLS-AA also provides
381 parameters for alkyl thiols. However, alkyl thiols adsorbed on Au(111)
382 surfaces do not have the hydrogen atom bonded to sulfur. To adapt this
383 change and derive suitable parameters for butanethiol adsorbed on
384 Au(111) surfaces, we adopt the S parameters from Luedtke and
385 Landman\cite{landman:1998} and modify parameters for its neighbor C
386 atom for charge balance in the molecule. Note that the model choice
387 (UA or AA) of capping agent can be different from the
388 solvent. Regardless of model choice, the force field parameters for
389 interactions between capping agent and solvent can be derived using
390 Lorentz-Berthelot Mixing Rule:
391 \begin{eqnarray}
392 \sigma_{IJ} & = & \frac{1}{2} \left(\sigma_{II} + \sigma_{JJ}\right) \\
393 \epsilon_{IJ} & = & \sqrt{\epsilon_{II}\epsilon_{JJ}}
394 \end{eqnarray}
395
396 To describe the interactions between metal Au and non-metal capping
397 agent and solvent particles, we refer to an adsorption study of alkyl
398 thiols on gold surfaces by Vlugt {\it et
399 al.}\cite{vlugt:cpc2007154} They fitted an effective Lennard-Jones
400 form of potential parameters for the interaction between Au and
401 pseudo-atoms CH$_x$ and S based on a well-established and widely-used
402 effective potential of Hautman and Klein\cite{hautman:4994} for the
403 Au(111) surface. As our simulations require the gold lattice slab to
404 be non-rigid so that it could accommodate kinetic energy for thermal
405 transport study purpose, the pair-wise form of potentials is
406 preferred.
407
408 Besides, the potentials developed from {\it ab initio} calculations by
409 Leng {\it et al.}\cite{doi:10.1021/jp034405s} are adopted for the
410 interactions between Au and aromatic C/H atoms in toluene.[MORE DETAILS]
411
412 However, the Lennard-Jones parameters between Au and other types of
413 particles in our simulations are not yet well-established. For these
414 interactions, we attempt to derive their parameters using the Mixing
415 Rule. To do this, the ``Metal-non-Metal'' (MnM) interaction parameters
416 for Au is first extracted from the Au-CH$_x$ parameters by applying
417 the Mixing Rule reversely. Table \ref{MnM} summarizes these ``MnM''
418 parameters in our simulations.
419
420 \begin{table*}
421 \begin{minipage}{\linewidth}
422 \begin{center}
423 \caption{Non-bonded interaction parameters (including cross
424 interactions with Au atoms) for both force fields used in this
425 work.}
426 \begin{tabular}{lllllll}
427 \hline\hline
428 & Site & $\sigma_{ii}$ & $\epsilon_{ii}$ & $q_i$ &
429 $\sigma_{Au-i}$ & $\epsilon_{Au-i}$ \\
430 & & (\AA) & (kcal/mol) & ($e$) & (\AA) & (kcal/mol) \\
431 \hline
432 United Atom (UA)
433 &CH3 & 3.75 & 0.1947 & - & 3.54 & 0.2146 \\
434 &CH2 & 3.95 & 0.0914 & - & 3.54 & 0.1749 \\
435 &CHar & 3.695 & 0.1003 & - & 3.4625 & 0.1680 \\
436 &CRar & 3.88 & 0.04173 & - & 3.555 & 0.1604 \\
437 \hline
438 All Atom (AA)
439 &CT3 & 3.50 & 0.066 & -0.18 & 3.365 & 0.1373 \\
440 &CT2 & 3.50 & 0.066 & -0.12 & 3.365 & 0.1373 \\
441 &CTT & 3.50 & 0.066 & -0.065 & 3.365 & 0.1373 \\
442 &HC & 2.50 & 0.030 & 0.06 & 2.865 & 0.09256 \\
443 &CA & 3.55 & 0.070 & -0.115 & 3.173 & 0.0640 \\
444 &HA & 2.42 & 0.030 & 0.115 & 2.746 & 0.0414 \\
445 \hline
446 Both UA and AA & S & 4.45 & 0.25 & - & 2.40 & 8.465 \\
447 \hline\hline
448 \end{tabular}
449 \label{MnM}
450 \end{center}
451 \end{minipage}
452 \end{table*}
453
454
455 \section{Results and Discussions}
456 [MAY HAVE A BRIEF SUMMARY]
457 \subsection{How Simulation Parameters Affects $G$}
458 [MAY NOT PUT AT FIRST]
459 We have varied our protocol or other parameters of the simulations in
460 order to investigate how these factors would affect the measurement of
461 $G$'s. It turned out that while some of these parameters would not
462 affect the results substantially, some other changes to the
463 simulations would have a significant impact on the measurement
464 results.
465
466 In some of our simulations, we allowed $L_x$ and $L_y$ to change
467 during equilibrating the liquid phase. Due to the stiffness of the Au
468 slab, $L_x$ and $L_y$ would not change noticeably after
469 equilibration. Although $L_z$ could fluctuate $\sim$1\% after a system
470 is fully equilibrated in the NPT ensemble, this fluctuation, as well
471 as those comparably smaller to $L_x$ and $L_y$, would not be magnified
472 on the calculated $G$'s, as shown in Table \ref{AuThiolHexaneUA}. This
473 insensivity to $L_i$ fluctuations allows reliable measurement of $G$'s
474 without the necessity of extremely cautious equilibration process.
475
476 As stated in our computational details, the spacing filled with
477 solvent molecules can be chosen within a range. This allows some
478 change of solvent molecule numbers for the same Au-butanethiol
479 surfaces. We did this study on our Au-butanethiol/hexane
480 simulations. Nevertheless, the results obtained from systems of
481 different $N_{hexane}$ did not indicate that the measurement of $G$ is
482 susceptible to this parameter. For computational efficiency concern,
483 smaller system size would be preferable, given that the liquid phase
484 structure is not affected.
485
486 Our NIVS algorithm allows change of unphysical thermal flux both in
487 direction and in quantity. This feature extends our investigation of
488 interfacial thermal conductance. However, the magnitude of this
489 thermal flux is not arbitary if one aims to obtain a stable and
490 reliable thermal gradient. A temperature profile would be
491 substantially affected by noise when $|J_z|$ has a much too low
492 magnitude; while an excessively large $|J_z|$ that overwhelms the
493 conductance capacity of the interface would prevent a thermal gradient
494 to reach a stablized steady state. NIVS has the advantage of allowing
495 $J$ to vary in a wide range such that the optimal flux range for $G$
496 measurement can generally be simulated by the algorithm. Within the
497 optimal range, we were able to study how $G$ would change according to
498 the thermal flux across the interface. For our simulations, we denote
499 $J_z$ to be positive when the physical thermal flux is from the liquid
500 to metal, and negative vice versa. The $G$'s measured under different
501 $J_z$ is listed in Table \ref{AuThiolHexaneUA} and [REF]. These
502 results do not suggest that $G$ is dependent on $J_z$ within this flux
503 range. The linear response of flux to thermal gradient simplifies our
504 investigations in that we can rely on $G$ measurement with only a
505 couple $J_z$'s and do not need to test a large series of fluxes.
506
507 %ADD MORE TO TABLE
508 \begin{table*}
509 \begin{minipage}{\linewidth}
510 \begin{center}
511 \caption{Computed interfacial thermal conductivity ($G$ and
512 $G^\prime$) values for the 100\% covered Au-butanethiol/hexane
513 interfaces with UA model and different hexane molecule numbers
514 at different temperatures using a range of energy fluxes.}
515
516 \begin{tabular}{ccccccc}
517 \hline\hline
518 $\langle T\rangle$ & $N_{hexane}$ & Fixed & $\rho_{hexane}$ &
519 $J_z$ & $G$ & $G^\prime$ \\
520 (K) & & $L_x$ \& $L_y$? & (g/cm$^3$) & (GW/m$^2$) &
521 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
522 \hline
523 200 & 266 & No & 0.672 & -0.96 & 102() & 80.0() \\
524 & 200 & Yes & 0.694 & 1.92 & 129() & 87.3() \\
525 & & Yes & 0.672 & 1.93 & 131() & 77.5() \\
526 & & No & 0.688 & 0.96 & 125() & 90.2() \\
527 & & & & 1.91 & 139() & 101() \\
528 & & & & 2.83 & 141() & 89.9() \\
529 & 166 & Yes & 0.679 & 0.97 & 115() & 69.3() \\
530 & & & & 1.94 & 125() & 87.1() \\
531 & & No & 0.681 & 0.97 & 141() & 77.7() \\
532 & & & & 1.92 & 138() & 98.9() \\
533 \hline
534 250 & 200 & No & 0.560 & 0.96 & 74.8() & 61.8() \\
535 & & & & -0.95 & 49.4() & 45.7() \\
536 & 166 & Yes & 0.570 & 0.98 & 79.0() & 62.9() \\
537 & & No & 0.569 & 0.97 & 80.3() & 67.1() \\
538 & & & & 1.44 & 76.2() & 64.8() \\
539 & & & & -0.95 & 56.4() & 54.4() \\
540 & & & & -1.85 & 47.8() & 53.5() \\
541 \hline\hline
542 \end{tabular}
543 \label{AuThiolHexaneUA}
544 \end{center}
545 \end{minipage}
546 \end{table*}
547
548 Furthermore, we also attempted to increase system average temperatures
549 to above 200K. These simulations are first equilibrated in the NPT
550 ensemble under normal pressure. As stated above, the TraPPE-UA model
551 for hexane tends to predict a lower boiling point. In our simulations,
552 hexane had diffculty to remain in liquid phase when NPT equilibration
553 temperature is higher than 250K. Additionally, the equilibrated liquid
554 hexane density under 250K becomes lower than experimental value. This
555 expanded liquid phase leads to lower contact between hexane and
556 butanethiol as well.[MAY NEED FIGURE] And this reduced contact would
557 probably be accountable for a lower interfacial thermal conductance,
558 as shown in Table \ref{AuThiolHexaneUA}.
559
560 A similar study for TraPPE-UA toluene agrees with the above result as
561 well. Having a higher boiling point, toluene tends to remain liquid in
562 our simulations even equilibrated under 300K in NPT
563 ensembles. Furthermore, the expansion of the toluene liquid phase is
564 not as significant as that of the hexane. This prevents severe
565 decrease of liquid-capping agent contact and the results (Table
566 \ref{AuThiolToluene}) show only a slightly decreased interface
567 conductance. Therefore, solvent-capping agent contact should play an
568 important role in the thermal transport process across the interface
569 in that higher degree of contact could yield increased conductance.
570
571 [ADD ERROR ESTIMATE TO TABLE]
572 \begin{table*}
573 \begin{minipage}{\linewidth}
574 \begin{center}
575 \caption{Computed interfacial thermal conductivity ($G$ and
576 $G^\prime$) values for a 90\% coverage Au-butanethiol/toluene
577 interface at different temperatures using a range of energy
578 fluxes.}
579
580 \begin{tabular}{ccccc}
581 \hline\hline
582 $\langle T\rangle$ & $\rho_{toluene}$ & $J_z$ & $G$ & $G^\prime$ \\
583 (K) & (g/cm$^3$) & (GW/m$^2$) & \multicolumn{2}{c}{(MW/m$^2$/K)} \\
584 \hline
585 200 & 0.933 & -1.86 & 180() & 135() \\
586 & & 2.15 & 204() & 113() \\
587 & & -3.93 & 175() & 114() \\
588 \hline
589 300 & 0.855 & -1.91 & 143() & 125() \\
590 & & -4.19 & 134() & 113() \\
591 \hline\hline
592 \end{tabular}
593 \label{AuThiolToluene}
594 \end{center}
595 \end{minipage}
596 \end{table*}
597
598 Besides lower interfacial thermal conductance, surfaces in relatively
599 high temperatures are susceptible to reconstructions, when
600 butanethiols have a full coverage on the Au(111) surface. These
601 reconstructions include surface Au atoms migrated outward to the S
602 atom layer, and butanethiol molecules embedded into the original
603 surface Au layer. The driving force for this behavior is the strong
604 Au-S interactions in our simulations. And these reconstructions lead
605 to higher ratio of Au-S attraction and thus is energetically
606 favorable. Furthermore, this phenomenon agrees with experimental
607 results\cite{doi:10.1021/j100035a033,doi:10.1021/la026493y}. Vlugt
608 {\it et al.} had kept their Au(111) slab rigid so that their
609 simulations can reach 300K without surface reconstructions. Without
610 this practice, simulating 100\% thiol covered interfaces under higher
611 temperatures could hardly avoid surface reconstructions. However, our
612 measurement is based on assuming homogeneity on $x$ and $y$ dimensions
613 so that measurement of $T$ at particular $z$ would be an effective
614 average of the particles of the same type. Since surface
615 reconstructions could eliminate the original $x$ and $y$ dimensional
616 homogeneity, measurement of $G$ is more difficult to conduct under
617 higher temperatures. Therefore, most of our measurements are
618 undertaken at $\langle T\rangle\sim$200K.
619
620 However, when the surface is not completely covered by butanethiols,
621 the simulated system is more resistent to the reconstruction
622 above. Our Au-butanethiol/toluene system did not see this phenomena
623 even at $\langle T\rangle\sim$300K. The Au(111) surfaces have a 90\%
624 coverage of butanethiols and have empty three-fold sites. These empty
625 sites could help prevent surface reconstruction in that they provide
626 other means of capping agent relaxation. It is observed that
627 butanethiols can migrate to their neighbor empty sites during a
628 simulation. Therefore, we were able to obtain $G$'s for these
629 interfaces even at a relatively high temperature without being
630 affected by surface reconstructions.
631
632 \subsection{Influence of Capping Agent Coverage on $G$}
633 To investigate the influence of butanethiol coverage on interfacial
634 thermal conductance, a series of different coverage Au-butanethiol
635 surfaces is prepared and solvated with various organic
636 molecules. These systems are then equilibrated and their interfacial
637 thermal conductivity are measured with our NIVS algorithm. Table
638 \ref{tlnUhxnUhxnD} lists these results for direct comparison between
639 different coverages of butanethiol. To study the isotope effect in
640 interfacial thermal conductance, deuterated UA-hexane is included as
641 well.
642
643 It turned out that with partial covered butanethiol on the Au(111)
644 surface, the derivative definition for $G$ (Eq. \ref{derivativeG}) has
645 difficulty to apply, due to the difficulty in locating the maximum of
646 change of $\lambda$. Instead, the discrete definition
647 (Eq. \ref{discreteG}) is easier to apply, as max($\Delta T$) can still
648 be well-defined. Therefore, $G$'s (not $G^\prime$) are used for this
649 section.
650
651 From Table \ref{tlnUhxnUhxnD}, one can see the significance of the
652 presence of capping agents. Even when a fraction of the Au(111)
653 surface sites are covered with butanethiols, the conductivity would
654 see an enhancement by at least a factor of 3. This indicates the
655 important role cappping agent is playing for thermal transport
656 phenomena on metal/organic solvent surfaces.
657
658 Interestingly, as one could observe from our results, the maximum
659 conductance enhancement (largest $G$) happens while the surfaces are
660 about 75\% covered with butanethiols. This again indicates that
661 solvent-capping agent contact has an important role of the thermal
662 transport process. Slightly lower butanethiol coverage allows small
663 gaps between butanethiols to form. And these gaps could be filled with
664 solvent molecules, which acts like ``heat conductors'' on the
665 surface. The higher degree of interaction between these solvent
666 molecules and capping agents increases the enhancement effect and thus
667 produces a higher $G$ than densely packed butanethiol arrays. However,
668 once this maximum conductance enhancement is reached, $G$ decreases
669 when butanethiol coverage continues to decrease. Each capping agent
670 molecule reaches its maximum capacity for thermal
671 conductance. Therefore, even higher solvent-capping agent contact
672 would not offset this effect. Eventually, when butanethiol coverage
673 continues to decrease, solvent-capping agent contact actually
674 decreases with the disappearing of butanethiol molecules. In this
675 case, $G$ decrease could not be offset but instead accelerated.
676
677 A comparison of the results obtained from differenet organic solvents
678 can also provide useful information of the interfacial thermal
679 transport process. The deuterated hexane (UA) results do not appear to
680 be much different from those of normal hexane (UA), given that
681 butanethiol (UA) is non-deuterated for both solvents. These UA model
682 studies, even though eliminating C-H vibration samplings, still have
683 C-C vibrational frequencies different from each other. However, these
684 differences in the infrared range do not seem to produce an observable
685 difference for the results of $G$. [MAY NEED FIGURE]
686
687 Furthermore, results for rigid body toluene solvent, as well as other
688 UA-hexane solvents, are reasonable within the general experimental
689 ranges[CITATIONS]. This suggests that explicit hydrogen might not be a
690 required factor for modeling thermal transport phenomena of systems
691 such as Au-thiol/organic solvent.
692
693 However, results for Au-butanethiol/toluene do not show an identical
694 trend with those for Au-butanethiol/hexane in that $G$'s remain at
695 approximately the same magnitue when butanethiol coverage differs from
696 25\% to 75\%. This might be rooted in the molecule shape difference
697 for plane-like toluene and chain-like {\it n}-hexane. Due to this
698 difference, toluene molecules have more difficulty in occupying
699 relatively small gaps among capping agents when their coverage is not
700 too low. Therefore, the solvent-capping agent contact may keep
701 increasing until the capping agent coverage reaches a relatively low
702 level. This becomes an offset for decreasing butanethiol molecules on
703 its effect to the process of interfacial thermal transport. Thus, one
704 can see a plateau of $G$ vs. butanethiol coverage in our results.
705
706 [NEED ERROR ESTIMATE]
707 \begin{figure}
708 \includegraphics[width=\linewidth]{coverage}
709 \caption{Comparison of interfacial thermal conductivity ($G$) values
710 for the Au-butanethiol/solvent interface with various UA models and
711 different capping agent coverages at $\langle T\rangle\sim$200K
712 using certain energy flux respectively.}
713 \label{coverage}
714 \end{figure}
715
716 \subsection{Influence of Chosen Molecule Model on $G$}
717 [MAY COMBINE W MECHANISM STUDY]
718
719 In addition to UA solvent/capping agent models, AA models are included
720 in our simulations as well. Besides simulations of the same (UA or AA)
721 model for solvent and capping agent, different models can be applied
722 to different components. Furthermore, regardless of models chosen,
723 either the solvent or the capping agent can be deuterated, similar to
724 the previous section. Table \ref{modelTest} summarizes the results of
725 these studies.
726
727 [MORE DATA; ERROR ESTIMATE]
728 \begin{table*}
729 \begin{minipage}{\linewidth}
730 \begin{center}
731
732 \caption{Computed interfacial thermal conductivity ($G$ and
733 $G^\prime$) values for interfaces using various models for
734 solvent and capping agent (or without capping agent) at
735 $\langle T\rangle\sim$200K. (D stands for deuterated solvent
736 or capping agent molecules; ``Avg.'' denotes results that are
737 averages of several simulations.)}
738
739 \begin{tabular}{ccccc}
740 \hline\hline
741 Butanethiol model & Solvent & $J_z$ & $G$ & $G^\prime$ \\
742 (or bare surface) & model & (GW/m$^2$) &
743 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
744 \hline
745 UA & UA hexane & Avg. & 131() & 86.5() \\
746 & UA hexane(D) & 1.95 & 153() & 136() \\
747 & AA hexane & 1.94 & 135() & 129() \\
748 & & 2.86 & 126() & 115() \\
749 & UA toluene & 1.96 & 187() & 151() \\
750 & AA toluene & 1.89 & 200() & 149() \\
751 \hline
752 AA & UA hexane & 1.94 & 116() & 129() \\
753 & AA hexane & Avg. & 442() & 356() \\
754 & AA hexane(D) & 1.93 & 222() & 234() \\
755 & UA toluene & 1.98 & 125() & 96.5() \\
756 & AA toluene & 3.79 & 487() & 290() \\
757 \hline
758 AA(D) & UA hexane & 1.94 & 158() & 172() \\
759 & AA hexane & 1.92 & 243() & 191() \\
760 & AA toluene & 1.93 & 364() & 322() \\
761 \hline
762 bare & UA hexane & Avg. & 46.5() & 49.4() \\
763 & UA hexane(D) & 0.98 & 43.9() & 43.0() \\
764 & AA hexane & 0.96 & 31.0() & 29.4() \\
765 & UA toluene & 1.99 & 70.1() & 65.8() \\
766 \hline\hline
767 \end{tabular}
768 \label{modelTest}
769 \end{center}
770 \end{minipage}
771 \end{table*}
772
773 To facilitate direct comparison, the same system with differnt models
774 for different components uses the same length scale for their
775 simulation cells. Without the presence of capping agent, using
776 different models for hexane yields similar results for both $G$ and
777 $G^\prime$, and these two definitions agree with eath other very
778 well. This indicates very weak interaction between the metal and the
779 solvent, and is a typical case for acoustic impedance mismatch between
780 these two phases.
781
782 As for Au(111) surfaces completely covered by butanethiols, the choice
783 of models for capping agent and solvent could impact the measurement
784 of $G$ and $G^\prime$ quite significantly. For Au-butanethiol/hexane
785 interfaces, using AA model for both butanethiol and hexane yields
786 substantially higher conductivity values than using UA model for at
787 least one component of the solvent and capping agent, which exceeds
788 the upper bond of experimental value range. This is probably due to
789 the classically treated C-H vibrations in the AA model, which should
790 not be appreciably populated at normal temperatures. In comparison,
791 once either the hexanes or the butanethiols are deuterated, one can
792 see a significantly lower $G$ and $G^\prime$. In either of these
793 cases, the C-H(D) vibrational overlap between the solvent and the
794 capping agent is removed. [MAY NEED FIGURE] Conclusively, the
795 improperly treated C-H vibration in the AA model produced
796 over-predicted results accordingly. Compared to the AA model, the UA
797 model yields more reasonable results with higher computational
798 efficiency.
799
800 However, for Au-butanethiol/toluene interfaces, having the AA
801 butanethiol deuterated did not yield a significant change in the
802 measurement results. Compared to the C-H vibrational overlap between
803 hexane and butanethiol, both of which have alkyl chains, that overlap
804 between toluene and butanethiol is not so significant and thus does
805 not have as much contribution to the ``Intramolecular Vibration
806 Redistribution''[CITE HASE]. Conversely, extra degrees of freedom such
807 as the C-H vibrations could yield higher heat exchange rate between
808 these two phases and result in a much higher conductivity.
809
810 Although the QSC model for Au is known to predict an overly low value
811 for bulk metal gold conductivity\cite{kuang:164101}, our computational
812 results for $G$ and $G^\prime$ do not seem to be affected by this
813 drawback of the model for metal. Instead, our results suggest that the
814 modeling of interfacial thermal transport behavior relies mainly on
815 the accuracy of the interaction descriptions between components
816 occupying the interfaces.
817
818 \subsection{Mechanism of Interfacial Thermal Conductance Enhancement
819 by Capping Agent}
820 %OR\subsection{Vibrational spectrum study on conductance mechanism}
821
822 [MAY INTRODUCE PROTOCOL IN METHODOLOGY/COMPUTATIONAL DETAIL, EQN'S]
823
824 To investigate the mechanism of this interfacial thermal conductance,
825 the vibrational spectra of various gold systems were obtained and are
826 shown as in the upper panel of Fig. \ref{vibration}. To obtain these
827 spectra, one first runs a simulation in the NVE ensemble and collects
828 snapshots of configurations; these configurations are used to compute
829 the velocity auto-correlation functions, which is used to construct a
830 power spectrum via a Fourier transform.
831
832 [MAY RELATE TO HASE'S]
833 The gold surfaces covered by
834 butanethiol molecules, compared to bare gold surfaces, exhibit an
835 additional peak observed at a frequency of $\sim$170cm$^{-1}$, which
836 is attributed to the vibration of the S-Au bond. This vibration
837 enables efficient thermal transport from surface Au atoms to the
838 capping agents. Simultaneously, as shown in the lower panel of
839 Fig. \ref{vibration}, the large overlap of the vibration spectra of
840 butanethiol and hexane in the all-atom model, including the C-H
841 vibration, also suggests high thermal exchange efficiency. The
842 combination of these two effects produces the drastic interfacial
843 thermal conductance enhancement in the all-atom model.
844
845 [REDO. MAY NEED TO CONVERT TO JPEG]
846 \begin{figure}
847 \includegraphics[width=\linewidth]{vibration}
848 \caption{Vibrational spectra obtained for gold in different
849 environments (upper panel) and for Au/thiol/hexane simulation in
850 all-atom model (lower panel).}
851 \label{vibration}
852 \end{figure}
853
854 [COMPARISON OF TWO G'S; AU SLAB WIDTHS; ETC]
855 % The results show that the two definitions used for $G$ yield
856 % comparable values, though $G^\prime$ tends to be smaller.
857
858 \section{Conclusions}
859 The NIVS algorithm we developed has been applied to simulations of
860 Au-butanethiol surfaces with organic solvents. This algorithm allows
861 effective unphysical thermal flux transferred between the metal and
862 the liquid phase. With the flux applied, we were able to measure the
863 corresponding thermal gradient and to obtain interfacial thermal
864 conductivities. Our simulations have seen significant conductance
865 enhancement with the presence of capping agent, compared to the bare
866 gold/liquid interfaces. The acoustic impedance mismatch between the
867 metal and the liquid phase is effectively eliminated by proper capping
868 agent. Furthermore, the coverage precentage of the capping agent plays
869 an important role in the interfacial thermal transport process.
870
871 Our measurement results, particularly of the UA models, agree with
872 available experimental data. This indicates that our force field
873 parameters have a nice description of the interactions between the
874 particles at the interfaces. AA models tend to overestimate the
875 interfacial thermal conductance in that the classically treated C-H
876 vibration would be overly sampled. Compared to the AA models, the UA
877 models have higher computational efficiency with satisfactory
878 accuracy, and thus are preferable in interfacial thermal transport
879 modelings.
880
881 Vlugt {\it et al.} has investigated the surface thiol structures for
882 nanocrystal gold and pointed out that they differs from those of the
883 Au(111) surface\cite{vlugt:cpc2007154}. This difference might lead to
884 change of interfacial thermal transport behavior as well. To
885 investigate this problem, an effective means to introduce thermal flux
886 and measure the corresponding thermal gradient is desirable for
887 simulating structures with spherical symmetry.
888
889
890 \section{Acknowledgments}
891 Support for this project was provided by the National Science
892 Foundation under grant CHE-0848243. Computational time was provided by
893 the Center for Research Computing (CRC) at the University of Notre
894 Dame. \newpage
895
896 \bibliography{interfacial}
897
898 \end{doublespace}
899 \end{document}
900