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# Content
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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 interfacial 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 (Figure \ref{demoPic}):
198 \begin{equation}
199 G=\frac{J}{\Delta T}
200 \label{discreteG}
201 \end{equation}
202
203 \begin{figure}
204 \includegraphics[width=\linewidth]{method}
205 \caption{Interfacial conductance can be calculated by applying an
206 (unphysical) kinetic energy flux between two slabs, one located
207 within the metal and another on the edge of the periodic box. The
208 system responds by forming a thermal response or a gradient. In
209 bulk liquids, this gradient typically has a single slope, but in
210 interfacial systems, there are distinct thermal conductivity
211 domains. The interfacial conductance, $G$ is found by measuring the
212 temperature gap at the Gibbs dividing surface, or by using second
213 derivatives of the thermal profile.}
214 \label{demoPic}
215 \end{figure}
216
217 The other approach is to assume a continuous temperature profile along
218 the thermal gradient axis (e.g. $z$) and define $G$ at the point where
219 the magnitude of thermal conductivity $\lambda$ change reach its
220 maximum, given that $\lambda$ is well-defined throughout the space:
221 \begin{equation}
222 G^\prime = \Big|\frac{\partial\lambda}{\partial z}\Big|
223 = \Big|\frac{\partial}{\partial z}\left(-J_z\Big/
224 \left(\frac{\partial T}{\partial z}\right)\right)\Big|
225 = |J_z|\Big|\frac{\partial^2 T}{\partial z^2}\Big|
226 \Big/\left(\frac{\partial T}{\partial z}\right)^2
227 \label{derivativeG}
228 \end{equation}
229
230 With the temperature profile obtained from simulations, one is able to
231 approximate the first and second derivatives of $T$ with finite
232 difference methods and thus calculate $G^\prime$.
233
234 In what follows, both definitions have been used for calculation and
235 are compared in the results.
236
237 To compare the above definitions ($G$ and $G^\prime$), we have modeled
238 a metal slab with its (111) surfaces perpendicular to the $z$-axis of
239 our simulation cells. Both with and without capping agents on the
240 surfaces, the metal slab is solvated with simple organic solvents, as
241 illustrated in Figure \ref{gradT}.
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{A sample of Au-butanethiol/hexane interfacial system and the
255 temperature profile after a kinetic energy flux is imposed to
256 it. The 1st and 2nd derivatives of the temperature profile can be
257 obtained with finite difference approximation (lower panel).}
258 \label{gradT}
259 \end{figure}
260
261 \section{Computational Details}
262 \subsection{Simulation Protocol}
263 The NIVS algorithm has been implemented in our MD simulation code,
264 OpenMD\cite{Meineke:2005gd,openmd}, and was used for our
265 simulations. Different metal slab thickness (layer numbers of Au) were
266 simulated. Metal slabs were first equilibrated under atmospheric
267 pressure (1 atm) and a desired temperature (e.g. 200K). After
268 equilibration, butanethiol capping agents were placed at three-fold
269 sites on the Au(111) surfaces. The maximum butanethiol capacity on Au
270 surface is $1/3$ of the total number of surface Au
271 atoms\cite{vlugt:cpc2007154}[CITE CHEM REV].
272 A series of different coverages was
273 investigated in order to study the relation between coverage and
274 interfacial conductance.
275
276 The capping agent molecules were allowed to migrate during the
277 simulations. They distributed themselves uniformly and sampled a
278 number of three-fold sites throughout out study. Therefore, the
279 initial configuration would not noticeably affect the sampling of a
280 variety of configurations of the same coverage, and the final
281 conductance measurement would be an average effect of these
282 configurations explored in the simulations. [MAY NEED SNAPSHOTS]
283
284 After the modified Au-butanethiol surface systems were equilibrated
285 under canonical ensemble, organic solvent molecules were packed in the
286 previously empty part of the simulation cells\cite{packmol}. Two
287 solvents were investigated, one which has little vibrational overlap
288 with the alkanethiol and a planar shape (toluene), and one which has
289 similar vibrational frequencies and chain-like shape ({\it n}-hexane).
290
291 The space filled by solvent molecules, i.e. the gap between
292 periodically repeated Au-butanethiol surfaces should be carefully
293 chosen. A very long length scale for the thermal gradient axis ($z$)
294 may cause excessively hot or cold temperatures in the middle of the
295 solvent region and lead to undesired phenomena such as solvent boiling
296 or freezing when a thermal flux is applied. Conversely, too few
297 solvent molecules would change the normal behavior of the liquid
298 phase. Therefore, our $N_{solvent}$ values were chosen to ensure that
299 these extreme cases did not happen to our simulations. And the
300 corresponding spacing is usually $35[?] \sim 75$\AA.
301
302 The initial configurations generated are further equilibrated with the
303 $x$ and $y$ dimensions fixed, only allowing length scale change in $z$
304 dimension. This is to ensure that the equilibration of liquid phase
305 does not affect the metal crystal structure in $x$ and $y$ dimensions.
306 To investigate this effect, comparisons were made with simulations
307 allowed to change $L_x$ and $L_y$ during NPT equilibration, and the
308 results are shown in later sections. After ensuring the liquid phase
309 reaches equilibrium at atmospheric pressure (1 atm), further
310 equilibration are followed under NVT and then NVE ensembles.
311
312 After the systems reach equilibrium, NIVS is implemented to impose a
313 periodic unphysical thermal flux between the metal and the liquid
314 phase. Most of our simulations are under an average temperature of
315 $\sim$200K. Therefore, this flux usually comes from the metal to the
316 liquid so that the liquid has a higher temperature and would not
317 freeze due to excessively low temperature. This induced temperature
318 gradient is stablized and the simulation cell is devided evenly into
319 N slabs along the $z$-axis and the temperatures of each slab are
320 recorded. When the slab width $d$ of each slab is the same, the
321 derivatives of $T$ with respect to slab number $n$ can be directly
322 used for $G^\prime$ calculations:
323 \begin{equation}
324 G^\prime = |J_z|\Big|\frac{\partial^2 T}{\partial z^2}\Big|
325 \Big/\left(\frac{\partial T}{\partial z}\right)^2
326 = |J_z|\Big|\frac{1}{d^2}\frac{\partial^2 T}{\partial n^2}\Big|
327 \Big/\left(\frac{1}{d}\frac{\partial T}{\partial n}\right)^2
328 = |J_z|\Big|\frac{\partial^2 T}{\partial n^2}\Big|
329 \Big/\left(\frac{\partial T}{\partial n}\right)^2
330 \label{derivativeG2}
331 \end{equation}
332
333 \subsection{Force Field Parameters}
334 Our simulations include various components. Figure \ref{demoMol}
335 demonstrates the sites defined for both United-Atom and All-Atom
336 models of the organic solvent and capping agent molecules in our
337 simulations. Force field parameter descriptions are needed for
338 interactions both between the same type of particles and between
339 particles of different species.
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 The Au-Au interactions in metal lattice slab is described by the
354 quantum Sutton-Chen (QSC) formulation\cite{PhysRevB.59.3527}. The QSC
355 potentials include zero-point quantum corrections and are
356 reparametrized for accurate surface energies compared to the
357 Sutton-Chen potentials\cite{Chen90}.
358
359 For both solvent molecules, straight chain {\it n}-hexane and aromatic
360 toluene, United-Atom (UA) and All-Atom (AA) models are used
361 respectively. The TraPPE-UA
362 parameters\cite{TraPPE-UA.alkanes,TraPPE-UA.alkylbenzenes} are used
363 for our UA solvent molecules. In these models, sites are located at
364 the carbon centers for alkyl groups. Bonding interactions, including
365 bond stretches and bends and torsions, were used for intra-molecular
366 sites not separated by more than 3 bonds. Otherwise, for non-bonded
367 interactions, Lennard-Jones potentials are used. [MORE CITATION?]
368
369 By eliminating explicit hydrogen atoms, these models are simple and
370 computationally efficient, while maintains good accuracy. However, the
371 TraPPE-UA for alkanes is known to predict a lower boiling point than
372 experimental values. Considering that after an unphysical thermal flux
373 is applied to a system, the temperature of ``hot'' area in the liquid
374 phase would be significantly higher than the average, to prevent over
375 heating and boiling of the liquid phase, the average temperature in
376 our simulations should be much lower than the liquid boiling point.
377
378 For UA-toluene model, the non-bonded potentials between
379 inter-molecular sites have a similar Lennard-Jones formulation. For
380 intra-molecular interactions, considering the stiffness of the benzene
381 ring, rigid body constraints are applied for further computational
382 efficiency. All bonds in the benzene ring and between the ring and the
383 methyl group remain rigid during the progress of simulations.
384
385 Besides the TraPPE-UA models, AA models for both organic solvents are
386 included in our studies as well. For hexane, the OPLS-AA\cite{OPLSAA}
387 force field is used. Additional explicit hydrogen sites were
388 included. Besides bonding and non-bonded site-site interactions,
389 partial charges and the electrostatic interactions were added to each
390 CT and HC site. For toluene, the United Force Field developed by
391 Rapp\'{e} {\it et al.}\cite{doi:10.1021/ja00051a040} is
392 adopted. Without the rigid body constraints, bonding interactions were
393 included. For the aromatic ring, improper torsions (inversions) were
394 added as an extra potential for maintaining the planar shape.
395 [MORE CITATION?]
396
397 The capping agent in our simulations, the butanethiol molecules can
398 either use UA or AA model. The TraPPE-UA force fields includes
399 parameters for thiol molecules\cite{TraPPE-UA.thiols} and are used for
400 UA butanethiol model in our simulations. The OPLS-AA also provides
401 parameters for alkyl thiols. However, alkyl thiols adsorbed on Au(111)
402 surfaces do not have the hydrogen atom bonded to sulfur. To adapt this
403 change and derive suitable parameters for butanethiol adsorbed on
404 Au(111) surfaces, we adopt the S parameters from Luedtke and
405 Landman\cite{landman:1998} and modify parameters for its neighbor C
406 atom for charge balance in the molecule. Note that the model choice
407 (UA or AA) of capping agent can be different from the
408 solvent. Regardless of model choice, the force field parameters for
409 interactions between capping agent and solvent can be derived using
410 Lorentz-Berthelot Mixing Rule:
411 \begin{eqnarray}
412 \sigma_{ij} & = & \frac{1}{2} \left(\sigma_{ii} + \sigma_{jj}\right) \\
413 \epsilon_{ij} & = & \sqrt{\epsilon_{ii}\epsilon_{jj}}
414 \end{eqnarray}
415
416 To describe the interactions between metal Au and non-metal capping
417 agent and solvent particles, we refer to an adsorption study of alkyl
418 thiols on gold surfaces by Vlugt {\it et
419 al.}\cite{vlugt:cpc2007154} They fitted an effective Lennard-Jones
420 form of potential parameters for the interaction between Au and
421 pseudo-atoms CH$_x$ and S based on a well-established and widely-used
422 effective potential of Hautman and Klein\cite{hautman:4994} for the
423 Au(111) surface. As our simulations require the gold lattice slab to
424 be non-rigid so that it could accommodate kinetic energy for thermal
425 transport study purpose, the pair-wise form of potentials is
426 preferred.
427
428 Besides, the potentials developed from {\it ab initio} calculations by
429 Leng {\it et al.}\cite{doi:10.1021/jp034405s} are adopted for the
430 interactions between Au and aromatic C/H atoms in toluene. A set of
431 pseudo Lennard-Jones parameters were provided for Au in their force
432 fields. By using the Mixing Rule, this can be used to derive pair-wise
433 potentials for non-bonded interactions between Au and non-metal sites.
434
435 However, the Lennard-Jones parameters between Au and other types of
436 particles, such as All-Atom normal alkanes in our simulations are not
437 yet well-established. For these interactions, we attempt to derive
438 their parameters using the Mixing Rule. To do this, Au pseudo
439 Lennard-Jones parameters for ``Metal-non-Metal'' (MnM) interactions
440 were first extracted from the Au-CH$_x$ parameters by applying the
441 Mixing Rule reversely. Table \ref{MnM} summarizes these ``MnM''
442 parameters in our simulations.
443
444 \begin{table*}
445 \begin{minipage}{\linewidth}
446 \begin{center}
447 \caption{Non-bonded interaction parameters (including cross
448 interactions with Au atoms) for both force fields used in this
449 work.}
450 \begin{tabular}{lllllll}
451 \hline\hline
452 & Site & $\sigma_{ii}$ & $\epsilon_{ii}$ & $q_i$ &
453 $\sigma_{Au-i}$ & $\epsilon_{Au-i}$ \\
454 & & (\AA) & (kcal/mol) & ($e$) & (\AA) & (kcal/mol) \\
455 \hline
456 United Atom (UA)
457 &CH3 & 3.75 & 0.1947 & - & 3.54 & 0.2146 \\
458 &CH2 & 3.95 & 0.0914 & - & 3.54 & 0.1749 \\
459 &CHar & 3.695 & 0.1003 & - & 3.4625 & 0.1680 \\
460 &CRar & 3.88 & 0.04173 & - & 3.555 & 0.1604 \\
461 \hline
462 All Atom (AA)
463 &CT3 & 3.50 & 0.066 & -0.18 & 3.365 & 0.1373 \\
464 &CT2 & 3.50 & 0.066 & -0.12 & 3.365 & 0.1373 \\
465 &CTT & 3.50 & 0.066 & -0.065 & 3.365 & 0.1373 \\
466 &HC & 2.50 & 0.030 & 0.06 & 2.865 & 0.09256 \\
467 &CA & 3.55 & 0.070 & -0.115 & 3.173 & 0.0640 \\
468 &HA & 2.42 & 0.030 & 0.115 & 2.746 & 0.0414 \\
469 \hline
470 Both UA and AA
471 & S & 4.45 & 0.25 & - & 2.40 & 8.465 \\
472 \hline\hline
473 \end{tabular}
474 \label{MnM}
475 \end{center}
476 \end{minipage}
477 \end{table*}
478
479 \subsection{Vibrational Spectrum}
480
481 [MAY ADD EQN'S]
482 To obtain these
483 spectra, one first runs a simulation in the NVE ensemble and collects
484 snapshots of configurations; these configurations are used to compute
485 the velocity auto-correlation functions, which is used to construct a
486 power spectrum via a Fourier transform.
487
488 \section{Results and Discussions}
489 [MAY HAVE A BRIEF SUMMARY]
490 \subsection{How Simulation Parameters Affects $G$}
491 [MAY NOT PUT AT FIRST]
492 We have varied our protocol or other parameters of the simulations in
493 order to investigate how these factors would affect the measurement of
494 $G$'s. It turned out that while some of these parameters would not
495 affect the results substantially, some other changes to the
496 simulations would have a significant impact on the measurement
497 results.
498
499 In some of our simulations, we allowed $L_x$ and $L_y$ to change
500 during equilibrating the liquid phase. Due to the stiffness of the
501 crystalline Au structure, $L_x$ and $L_y$ would not change noticeably
502 after equilibration. Although $L_z$ could fluctuate $\sim$1\% after a
503 system is fully equilibrated in the NPT ensemble, this fluctuation, as
504 well as those of $L_x$ and $L_y$ (which is significantly smaller),
505 would not be magnified on the calculated $G$'s, as shown in Table
506 \ref{AuThiolHexaneUA}. This insensivity to $L_i$ fluctuations allows
507 reliable measurement of $G$'s without the necessity of extremely
508 cautious equilibration process.
509
510 As stated in our computational details, the spacing filled with
511 solvent molecules can be chosen within a range. This allows some
512 change of solvent molecule numbers for the same Au-butanethiol
513 surfaces. We did this study on our Au-butanethiol/hexane
514 simulations. Nevertheless, the results obtained from systems of
515 different $N_{hexane}$ did not indicate that the measurement of $G$ is
516 susceptible to this parameter. For computational efficiency concern,
517 smaller system size would be preferable, given that the liquid phase
518 structure is not affected.
519
520 Our NIVS algorithm allows change of unphysical thermal flux both in
521 direction and in quantity. This feature extends our investigation of
522 interfacial thermal conductance. However, the magnitude of this
523 thermal flux is not arbitary if one aims to obtain a stable and
524 reliable thermal gradient. A temperature profile would be
525 substantially affected by noise when $|J_z|$ has a much too low
526 magnitude; while an excessively large $|J_z|$ that overwhelms the
527 conductance capacity of the interface would prevent a thermal gradient
528 to reach a stablized steady state. NIVS has the advantage of allowing
529 $J$ to vary in a wide range such that the optimal flux range for $G$
530 measurement can generally be simulated by the algorithm. Within the
531 optimal range, we were able to study how $G$ would change according to
532 the thermal flux across the interface. For our simulations, we denote
533 $J_z$ to be positive when the physical thermal flux is from the liquid
534 to metal, and negative vice versa. The $G$'s measured under different
535 $J_z$ is listed in Table \ref{AuThiolHexaneUA} and
536 \ref{AuThiolToluene}. These results do not suggest that $G$ is
537 dependent on $J_z$ within this flux range. The linear response of flux
538 to thermal gradient simplifies our investigations in that we can rely
539 on $G$ measurement with only a couple $J_z$'s and do not need to test
540 a large series of fluxes.
541
542 \begin{table*}
543 \begin{minipage}{\linewidth}
544 \begin{center}
545 \caption{Computed interfacial thermal conductivity ($G$ and
546 $G^\prime$) values for the 100\% covered Au-butanethiol/hexane
547 interfaces with UA model and different hexane molecule numbers
548 at different temperatures using a range of energy
549 fluxes. Error estimates indicated in parenthesis.}
550
551 \begin{tabular}{ccccccc}
552 \hline\hline
553 $\langle T\rangle$ & $N_{hexane}$ & Fixed & $\rho_{hexane}$ &
554 $J_z$ & $G$ & $G^\prime$ \\
555 (K) & & $L_x$ \& $L_y$? & (g/cm$^3$) & (GW/m$^2$) &
556 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
557 \hline
558 200 & 266 & No & 0.672 & -0.96 & 102(3) & 80.0(0.8) \\
559 & 200 & Yes & 0.694 & 1.92 & 129(11) & 87.3(0.3) \\
560 & & Yes & 0.672 & 1.93 & 131(16) & 78(13) \\
561 & & No & 0.688 & 0.96 & 125(16) & 90.2(15) \\
562 & & & & 1.91 & 139(10) & 101(10) \\
563 & & & & 2.83 & 141(6) & 89.9(9.8) \\
564 & 166 & Yes & 0.679 & 0.97 & 115(19) & 69(18) \\
565 & & & & 1.94 & 125(9) & 87.1(0.2) \\
566 & & No & 0.681 & 0.97 & 141(30) & 78(22) \\
567 & & & & 1.92 & 138(4) & 98.9(9.5) \\
568 \hline
569 250 & 200 & No & 0.560 & 0.96 & 75(10) & 61.8(7.3) \\
570 & & & & -0.95 & 49.4(0.3) & 45.7(2.1) \\
571 & 166 & Yes & 0.570 & 0.98 & 79.0(3.5) & 62.9(3.0) \\
572 & & No & 0.569 & 0.97 & 80.3(0.6) & 67(11) \\
573 & & & & 1.44 & 76.2(5.0) & 64.8(3.8) \\
574 & & & & -0.95 & 56.4(2.5) & 54.4(1.1) \\
575 & & & & -1.85 & 47.8(1.1) & 53.5(1.5) \\
576 \hline\hline
577 \end{tabular}
578 \label{AuThiolHexaneUA}
579 \end{center}
580 \end{minipage}
581 \end{table*}
582
583 Furthermore, we also attempted to increase system average temperatures
584 to above 200K. These simulations are first equilibrated in the NPT
585 ensemble under normal pressure. As stated above, the TraPPE-UA model
586 for hexane tends to predict a lower boiling point. In our simulations,
587 hexane had diffculty to remain in liquid phase when NPT equilibration
588 temperature is higher than 250K. Additionally, the equilibrated liquid
589 hexane density under 250K becomes lower than experimental value. This
590 expanded liquid phase leads to lower contact between hexane and
591 butanethiol as well.[MAY NEED SLAB DENSITY FIGURE]
592 And this reduced contact would
593 probably be accountable for a lower interfacial thermal conductance,
594 as shown in Table \ref{AuThiolHexaneUA}.
595
596 A similar study for TraPPE-UA toluene agrees with the above result as
597 well. Having a higher boiling point, toluene tends to remain liquid in
598 our simulations even equilibrated under 300K in NPT
599 ensembles. Furthermore, the expansion of the toluene liquid phase is
600 not as significant as that of the hexane. This prevents severe
601 decrease of liquid-capping agent contact and the results (Table
602 \ref{AuThiolToluene}) show only a slightly decreased interface
603 conductance. Therefore, solvent-capping agent contact should play an
604 important role in the thermal transport process across the interface
605 in that higher degree of contact could yield increased conductance.
606
607 \begin{table*}
608 \begin{minipage}{\linewidth}
609 \begin{center}
610 \caption{Computed interfacial thermal conductivity ($G$ and
611 $G^\prime$) values for a 90\% coverage Au-butanethiol/toluene
612 interface at different temperatures using a range of energy
613 fluxes. Error estimates indicated in parenthesis.}
614
615 \begin{tabular}{ccccc}
616 \hline\hline
617 $\langle T\rangle$ & $\rho_{toluene}$ & $J_z$ & $G$ & $G^\prime$ \\
618 (K) & (g/cm$^3$) & (GW/m$^2$) & \multicolumn{2}{c}{(MW/m$^2$/K)} \\
619 \hline
620 200 & 0.933 & 2.15 & 204(12) & 113(12) \\
621 & & -1.86 & 180(3) & 135(21) \\
622 & & -3.93 & 176(5) & 113(12) \\
623 \hline
624 300 & 0.855 & -1.91 & 143(5) & 125(2) \\
625 & & -4.19 & 135(9) & 113(12) \\
626 \hline\hline
627 \end{tabular}
628 \label{AuThiolToluene}
629 \end{center}
630 \end{minipage}
631 \end{table*}
632
633 Besides lower interfacial thermal conductance, surfaces in relatively
634 high temperatures are susceptible to reconstructions, when
635 butanethiols have a full coverage on the Au(111) surface. These
636 reconstructions include surface Au atoms migrated outward to the S
637 atom layer, and butanethiol molecules embedded into the original
638 surface Au layer. The driving force for this behavior is the strong
639 Au-S interactions in our simulations. And these reconstructions lead
640 to higher ratio of Au-S attraction and thus is energetically
641 favorable. Furthermore, this phenomenon agrees with experimental
642 results\cite{doi:10.1021/j100035a033,doi:10.1021/la026493y}. Vlugt
643 {\it et al.} had kept their Au(111) slab rigid so that their
644 simulations can reach 300K without surface reconstructions. Without
645 this practice, simulating 100\% thiol covered interfaces under higher
646 temperatures could hardly avoid surface reconstructions. However, our
647 measurement is based on assuming homogeneity on $x$ and $y$ dimensions
648 so that measurement of $T$ at particular $z$ would be an effective
649 average of the particles of the same type. Since surface
650 reconstructions could eliminate the original $x$ and $y$ dimensional
651 homogeneity, measurement of $G$ is more difficult to conduct under
652 higher temperatures. Therefore, most of our measurements are
653 undertaken at $\langle T\rangle\sim$200K.
654
655 However, when the surface is not completely covered by butanethiols,
656 the simulated system is more resistent to the reconstruction
657 above. Our Au-butanethiol/toluene system had the Au(111) surfaces 90\%
658 covered by butanethiols, but did not see this above phenomena even at
659 $\langle T\rangle\sim$300K. The empty three-fold sites not occupied by
660 capping agents could help prevent surface reconstruction in that they
661 provide other means of capping agent relaxation. It is observed that
662 butanethiols can migrate to their neighbor empty sites during a
663 simulation. Therefore, we were able to obtain $G$'s for these
664 interfaces even at a relatively high temperature without being
665 affected by surface reconstructions.
666
667 \subsection{Influence of Capping Agent Coverage on $G$}
668 To investigate the influence of butanethiol coverage on interfacial
669 thermal conductance, a series of different coverage Au-butanethiol
670 surfaces is prepared and solvated with various organic
671 molecules. These systems are then equilibrated and their interfacial
672 thermal conductivity are measured with our NIVS algorithm. Figure
673 \ref{coverage} demonstrates the trend of conductance change with
674 respect to different coverages of butanethiol. To study the isotope
675 effect in interfacial thermal conductance, deuterated UA-hexane is
676 included as well.
677
678 It turned out that with partial covered butanethiol on the Au(111)
679 surface, the derivative definition for $G^\prime$
680 (Eq. \ref{derivativeG}) was difficult to apply, due to the difficulty
681 in locating the maximum of change of $\lambda$. Instead, the discrete
682 definition (Eq. \ref{discreteG}) is easier to apply, as the Gibbs
683 deviding surface can still be well-defined. Therefore, $G$ (not
684 $G^\prime$) was used for this section.
685
686 From Figure \ref{coverage}, one can see the significance of the
687 presence of capping agents. Even when a fraction of the Au(111)
688 surface sites are covered with butanethiols, the conductivity would
689 see an enhancement by at least a factor of 3. This indicates the
690 important role cappping agent is playing for thermal transport
691 phenomena on metal / organic solvent surfaces.
692
693 Interestingly, as one could observe from our results, the maximum
694 conductance enhancement (largest $G$) happens while the surfaces are
695 about 75\% covered with butanethiols. This again indicates that
696 solvent-capping agent contact has an important role of the thermal
697 transport process. Slightly lower butanethiol coverage allows small
698 gaps between butanethiols to form. And these gaps could be filled with
699 solvent molecules, which acts like ``heat conductors'' on the
700 surface. The higher degree of interaction between these solvent
701 molecules and capping agents increases the enhancement effect and thus
702 produces a higher $G$ than densely packed butanethiol arrays. However,
703 once this maximum conductance enhancement is reached, $G$ decreases
704 when butanethiol coverage continues to decrease. Each capping agent
705 molecule reaches its maximum capacity for thermal
706 conductance. Therefore, even higher solvent-capping agent contact
707 would not offset this effect. Eventually, when butanethiol coverage
708 continues to decrease, solvent-capping agent contact actually
709 decreases with the disappearing of butanethiol molecules. In this
710 case, $G$ decrease could not be offset but instead accelerated. [NEED
711 SNAPSHOT SHOWING THE PHENOMENA / SLAB DENSITY ANALYSIS]
712
713 A comparison of the results obtained from differenet organic solvents
714 can also provide useful information of the interfacial thermal
715 transport process. The deuterated hexane (UA) results do not appear to
716 be much different from those of normal hexane (UA), given that
717 butanethiol (UA) is non-deuterated for both solvents. These UA model
718 studies, even though eliminating C-H vibration samplings, still have
719 C-C vibrational frequencies different from each other. However, these
720 differences in the infrared range do not seem to produce an observable
721 difference for the results of $G$. [MAY NEED SPECTRA FIGURE]
722
723 Furthermore, results for rigid body toluene solvent, as well as other
724 UA-hexane solvents, are reasonable within the general experimental
725 ranges[CITATIONS]. This suggests that explicit hydrogen might not be a
726 required factor for modeling thermal transport phenomena of systems
727 such as Au-thiol/organic solvent.
728
729 However, results for Au-butanethiol/toluene do not show an identical
730 trend with those for Au-butanethiol/hexane in that $G$ remains at
731 approximately the same magnitue when butanethiol coverage differs from
732 25\% to 75\%. This might be rooted in the molecule shape difference
733 for planar toluene and chain-like {\it n}-hexane. Due to this
734 difference, toluene molecules have more difficulty in occupying
735 relatively small gaps among capping agents when their coverage is not
736 too low. Therefore, the solvent-capping agent contact may keep
737 increasing until the capping agent coverage reaches a relatively low
738 level. This becomes an offset for decreasing butanethiol molecules on
739 its effect to the process of interfacial thermal transport. Thus, one
740 can see a plateau of $G$ vs. butanethiol coverage in our results.
741
742 \begin{figure}
743 \includegraphics[width=\linewidth]{coverage}
744 \caption{Comparison of interfacial thermal conductivity ($G$) values
745 for the Au-butanethiol/solvent interface with various UA models and
746 different capping agent coverages at $\langle T\rangle\sim$200K
747 using certain energy flux respectively.}
748 \label{coverage}
749 \end{figure}
750
751 \subsection{Influence of Chosen Molecule Model on $G$}
752 In addition to UA solvent/capping agent models, AA models are included
753 in our simulations as well. Besides simulations of the same (UA or AA)
754 model for solvent and capping agent, different models can be applied
755 to different components. Furthermore, regardless of models chosen,
756 either the solvent or the capping agent can be deuterated, similar to
757 the previous section. Table \ref{modelTest} summarizes the results of
758 these studies.
759
760 \begin{table*}
761 \begin{minipage}{\linewidth}
762 \begin{center}
763
764 \caption{Computed interfacial thermal conductivity ($G$ and
765 $G^\prime$) values for interfaces using various models for
766 solvent and capping agent (or without capping agent) at
767 $\langle T\rangle\sim$200K. (D stands for deuterated solvent
768 or capping agent molecules; ``Avg.'' denotes results that are
769 averages of simulations under different $J_z$'s. Error
770 estimates indicated in parenthesis.)}
771
772 \begin{tabular}{llccc}
773 \hline\hline
774 Butanethiol model & Solvent & $J_z$ & $G$ & $G^\prime$ \\
775 (or bare surface) & model & (GW/m$^2$) &
776 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
777 \hline
778 UA & UA hexane & Avg. & 131(9) & 87(10) \\
779 & UA hexane(D) & 1.95 & 153(5) & 136(13) \\
780 & AA hexane & Avg. & 131(6) & 122(10) \\
781 & UA toluene & 1.96 & 187(16) & 151(11) \\
782 & AA toluene & 1.89 & 200(36) & 149(53) \\
783 \hline
784 AA & UA hexane & 1.94 & 116(9) & 129(8) \\
785 & AA hexane & Avg. & 442(14) & 356(31) \\
786 & AA hexane(D) & 1.93 & 222(12) & 234(54) \\
787 & UA toluene & 1.98 & 125(25) & 97(60) \\
788 & AA toluene & 3.79 & 487(56) & 290(42) \\
789 \hline
790 AA(D) & UA hexane & 1.94 & 158(25) & 172(4) \\
791 & AA hexane & 1.92 & 243(29) & 191(11) \\
792 & AA toluene & 1.93 & 364(36) & 322(67) \\
793 \hline
794 bare & UA hexane & Avg. & 46.5(3.2) & 49.4(4.5) \\
795 & UA hexane(D) & 0.98 & 43.9(4.6) & 43.0(2.0) \\
796 & AA hexane & 0.96 & 31.0(1.4) & 29.4(1.3) \\
797 & UA toluene & 1.99 & 70.1(1.3) & 65.8(0.5) \\
798 \hline\hline
799 \end{tabular}
800 \label{modelTest}
801 \end{center}
802 \end{minipage}
803 \end{table*}
804
805 To facilitate direct comparison, the same system with differnt models
806 for different components uses the same length scale for their
807 simulation cells. Without the presence of capping agent, using
808 different models for hexane yields similar results for both $G$ and
809 $G^\prime$, and these two definitions agree with eath other very
810 well. This indicates very weak interaction between the metal and the
811 solvent, and is a typical case for acoustic impedance mismatch between
812 these two phases.
813
814 As for Au(111) surfaces completely covered by butanethiols, the choice
815 of models for capping agent and solvent could impact the measurement
816 of $G$ and $G^\prime$ quite significantly. For Au-butanethiol/hexane
817 interfaces, using AA model for both butanethiol and hexane yields
818 substantially higher conductivity values than using UA model for at
819 least one component of the solvent and capping agent, which exceeds
820 the general range of experimental measurement results. This is
821 probably due to the classically treated C-H vibrations in the AA
822 model, which should not be appreciably populated at normal
823 temperatures. In comparison, once either the hexanes or the
824 butanethiols are deuterated, one can see a significantly lower $G$ and
825 $G^\prime$. In either of these cases, the C-H(D) vibrational overlap
826 between the solvent and the capping agent is removed.
827 [MAY NEED SPECTRA FIGURE] Conclusively, the
828 improperly treated C-H vibration in the AA model produced
829 over-predicted results accordingly. Compared to the AA model, the UA
830 model yields more reasonable results with higher computational
831 efficiency.
832
833 However, for Au-butanethiol/toluene interfaces, having the AA
834 butanethiol deuterated did not yield a significant change in the
835 measurement results. Compared to the C-H vibrational overlap between
836 hexane and butanethiol, both of which have alkyl chains, that overlap
837 between toluene and butanethiol is not so significant and thus does
838 not have as much contribution to the ``Intramolecular Vibration
839 Redistribution''[CITE HASE]. Conversely, extra degrees of freedom such
840 as the C-H vibrations could yield higher heat exchange rate between
841 these two phases and result in a much higher conductivity.
842
843 Although the QSC model for Au is known to predict an overly low value
844 for bulk metal gold conductivity\cite{kuang:164101}, our computational
845 results for $G$ and $G^\prime$ do not seem to be affected by this
846 drawback of the model for metal. Instead, our results suggest that the
847 modeling of interfacial thermal transport behavior relies mainly on
848 the accuracy of the interaction descriptions between components
849 occupying the interfaces.
850
851 \subsection{Role of Capping Agent in Interfacial Thermal Conductance}
852 To investigate the mechanism of this interfacial thermal conductance,
853 the vibrational spectra of various gold systems were obtained and are
854 shown as in Fig. \ref{vibration}.
855 [MAY RELATE TO HASE'S]
856 The gold surfaces covered by butanethiol molecules, compared to bare
857 gold surfaces, exhibit an additional peak observed at the frequency of
858 $\sim$170cm$^{-1}$, which is attributed to the S-Au bonding
859 vibration. This vibration enables efficient thermal transport from
860 surface Au layer to the capping agents.
861 [MAY PUT IN OTHER SECTION] Simultaneously, as shown in
862 the lower panel of Fig. \ref{vibration}, the large overlap of the
863 vibration spectra of butanethiol and hexane in the All-Atom model,
864 including the C-H vibration, also suggests high thermal exchange
865 efficiency. The combination of these two effects produces the drastic
866 interfacial thermal conductance enhancement in the All-Atom model.
867
868 [NEED SEPARATE FIGURE. MAY NEED TO CONVERT TO JPEG]
869 \begin{figure}
870 \includegraphics[width=\linewidth]{vibration}
871 \caption{Vibrational spectra obtained for gold in different
872 environments.}
873 \label{vibration}
874 \end{figure}
875
876 [MAY ADD COMPARISON OF G AND G', AU SLAB WIDTHS, ETC]
877 % The results show that the two definitions used for $G$ yield
878 % comparable values, though $G^\prime$ tends to be smaller.
879
880 \section{Conclusions}
881 The NIVS algorithm we developed has been applied to simulations of
882 Au-butanethiol surfaces with organic solvents. This algorithm allows
883 effective unphysical thermal flux transferred between the metal and
884 the liquid phase. With the flux applied, we were able to measure the
885 corresponding thermal gradient and to obtain interfacial thermal
886 conductivities. Our simulations have seen significant conductance
887 enhancement with the presence of capping agent, compared to the bare
888 gold / liquid interfaces. The acoustic impedance mismatch between the
889 metal and the liquid phase is effectively eliminated by proper capping
890 agent. Furthermore, the coverage precentage of the capping agent plays
891 an important role in the interfacial thermal transport process.
892
893 Our measurement results, particularly of the UA models, agree with
894 available experimental data. This indicates that our force field
895 parameters have a nice description of the interactions between the
896 particles at the interfaces. AA models tend to overestimate the
897 interfacial thermal conductance in that the classically treated C-H
898 vibration would be overly sampled. Compared to the AA models, the UA
899 models have higher computational efficiency with satisfactory
900 accuracy, and thus are preferable in interfacial thermal transport
901 modelings.
902
903 Vlugt {\it et al.} has investigated the surface thiol structures for
904 nanocrystal gold and pointed out that they differs from those of the
905 Au(111) surface\cite{vlugt:cpc2007154}. This difference might lead to
906 change of interfacial thermal transport behavior as well. To
907 investigate this problem, an effective means to introduce thermal flux
908 and measure the corresponding thermal gradient is desirable for
909 simulating structures with spherical symmetry.
910
911
912 \section{Acknowledgments}
913 Support for this project was provided by the National Science
914 Foundation under grant CHE-0848243. Computational time was provided by
915 the Center for Research Computing (CRC) at the University of Notre
916 Dame. \newpage
917
918 \bibliography{interfacial}
919
920 \end{doublespace}
921 \end{document}
922