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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 (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{demoPic}.
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 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}. A series of different coverages was
272 investigated in order to study the relation between coverage and
273 interfacial conductance.
274
275 The capping agent molecules were allowed to migrate during the
276 simulations. They distributed themselves uniformly and sampled a
277 number of three-fold sites throughout out study. Therefore, the
278 initial configuration would not noticeably affect the sampling of a
279 variety of configurations of the same coverage, and the final
280 conductance measurement would be an average effect of these
281 configurations explored in the simulations. [MAY NEED FIGURES]
282
283 After the modified Au-butanethiol surface systems were equilibrated
284 under canonical ensemble, organic solvent molecules were packed in the
285 previously empty part of the simulation cells\cite{packmol}. Two
286 solvents were investigated, one which has little vibrational overlap
287 with the alkanethiol and a planar shape (toluene), and one which has
288 similar vibrational frequencies and chain-like shape ({\it n}-hexane).
289
290 The space filled by solvent molecules, i.e. the gap between
291 periodically repeated Au-butanethiol surfaces should be carefully
292 chosen. A very long length scale for the thermal gradient axis ($z$)
293 may cause excessively hot or cold temperatures in the middle of the
294 solvent region and lead to undesired phenomena such as solvent boiling
295 or freezing when a thermal flux is applied. Conversely, too few
296 solvent molecules would change the normal behavior of the liquid
297 phase. Therefore, our $N_{solvent}$ values were chosen to ensure that
298 these extreme cases did not happen to our simulations. And the
299 corresponding spacing is usually $35 \sim 75$\AA.
300
301 The initial configurations generated by Packmol are further
302 equilibrated with the $x$ and $y$ dimensions fixed, only allowing
303 length scale change in $z$ dimension. This is to ensure that the
304 equilibration of liquid phase does not affect the metal crystal
305 structure in $x$ and $y$ dimensions. Further equilibration are run
306 under NVT and then NVE ensembles.
307
308 After the systems reach equilibrium, NIVS is implemented to impose a
309 periodic unphysical thermal flux between the metal and the liquid
310 phase. Most of our simulations are under an average temperature of
311 $\sim$200K. Therefore, this flux usually comes from the metal to the
312 liquid so that the liquid has a higher temperature and would not
313 freeze due to excessively low temperature. This induced temperature
314 gradient is stablized and the simulation cell is devided evenly into
315 N slabs along the $z$-axis and the temperatures of each slab are
316 recorded. When the slab width $d$ of each slab is the same, the
317 derivatives of $T$ with respect to slab number $n$ can be directly
318 used for $G^\prime$ calculations:
319 \begin{equation}
320 G^\prime = |J_z|\Big|\frac{\partial^2 T}{\partial z^2}\Big|
321 \Big/\left(\frac{\partial T}{\partial z}\right)^2
322 = |J_z|\Big|\frac{1}{d^2}\frac{\partial^2 T}{\partial n^2}\Big|
323 \Big/\left(\frac{1}{d}\frac{\partial T}{\partial n}\right)^2
324 = |J_z|\Big|\frac{\partial^2 T}{\partial n^2}\Big|
325 \Big/\left(\frac{\partial T}{\partial n}\right)^2
326 \label{derivativeG2}
327 \end{equation}
328
329 \subsection{Force Field Parameters}
330 Our simulations include various components. Figure \ref{demoMol}
331 demonstrates the sites defined for both United-Atom and All-Atom
332 models of the organic solvent and capping agent molecules in our
333 simulations. Force field parameter descriptions are needed for
334 interactions both between the same type of particles and between
335 particles of different species.
336
337 \begin{figure}
338 \includegraphics[width=\linewidth]{structures}
339 \caption{Structures of the capping agent and solvents utilized in
340 these simulations. The chemically-distinct sites (a-e) are expanded
341 in terms of constituent atoms for both United Atom (UA) and All Atom
342 (AA) force fields. Most parameters are from
343 Refs. \protect\cite{TraPPE-UA.alkanes,TraPPE-UA.alkylbenzenes} (UA) and
344 \protect\cite{OPLSAA} (AA). Cross-interactions with the Au atoms are given
345 in Table \ref{MnM}.}
346 \label{demoMol}
347 \end{figure}
348
349 The Au-Au interactions in metal lattice slab is described by the
350 quantum Sutton-Chen (QSC) formulation\cite{PhysRevB.59.3527}. The QSC
351 potentials include zero-point quantum corrections and are
352 reparametrized for accurate surface energies compared to the
353 Sutton-Chen potentials\cite{Chen90}.
354
355 For both solvent molecules, straight chain {\it n}-hexane and aromatic
356 toluene, United-Atom (UA) and All-Atom (AA) models are used
357 respectively. The TraPPE-UA
358 parameters\cite{TraPPE-UA.alkanes,TraPPE-UA.alkylbenzenes} are used
359 for our UA solvent molecules. In these models, sites are located at
360 the carbon centers for alkyl groups. Bonding interactions, including
361 bond stretches and bends and torsions, were used for intra-molecular
362 sites not separated by more than 3 bonds. Otherwise, for non-bonded
363 interactions, Lennard-Jones potentials are used. [MORE CITATION?]
364
365 By eliminating explicit hydrogen atoms, these models are simple and
366 computationally efficient, while maintains good accuracy. However, the
367 TraPPE-UA for alkanes is known to predict a lower boiling point than
368 experimental values. Considering that after an unphysical thermal flux
369 is applied to a system, the temperature of ``hot'' area in the liquid
370 phase would be significantly higher than the average, to prevent over
371 heating and boiling of the liquid phase, the average temperature in
372 our simulations should be much lower than the liquid boiling point.
373
374 For UA-toluene model, the non-bonded potentials between
375 inter-molecular sites have a similar Lennard-Jones formulation. For
376 intra-molecular interactions, considering the stiffness of the benzene
377 ring, rigid body constraints are applied for further computational
378 efficiency. All bonds in the benzene ring and between the ring and the
379 methyl group remain rigid during the progress of simulations.
380
381 Besides the TraPPE-UA models, AA models for both organic solvents are
382 included in our studies as well. For hexane, the OPLS-AA\cite{OPLSAA}
383 force field is used. Additional explicit hydrogen sites were
384 included. Besides bonding and non-bonded site-site interactions,
385 partial charges and the electrostatic interactions were added to each
386 CT and HC site. For toluene, the United Force Field developed by
387 Rapp\'{e} {\it et al.}\cite{doi:10.1021/ja00051a040} is
388 adopted. Without the rigid body constraints, bonding interactions were
389 included. For the aromatic ring, improper torsions (inversions) were
390 added as an extra potential for maintaining the planar shape.
391 [MORE CITATION?]
392
393 The capping agent in our simulations, the butanethiol molecules can
394 either use UA or AA model. The TraPPE-UA force fields includes
395 parameters for thiol molecules\cite{TraPPE-UA.thiols} and are used for
396 UA butanethiol model in our simulations. The OPLS-AA also provides
397 parameters for alkyl thiols. However, alkyl thiols adsorbed on Au(111)
398 surfaces do not have the hydrogen atom bonded to sulfur. To adapt this
399 change and derive suitable parameters for butanethiol adsorbed on
400 Au(111) surfaces, we adopt the S parameters from Luedtke and
401 Landman\cite{landman:1998} and modify parameters for its neighbor C
402 atom for charge balance in the molecule. Note that the model choice
403 (UA or AA) of capping agent can be different from the
404 solvent. Regardless of model choice, the force field parameters for
405 interactions between capping agent and solvent can be derived using
406 Lorentz-Berthelot Mixing Rule:
407 \begin{eqnarray}
408 \sigma_{ij} & = & \frac{1}{2} \left(\sigma_{ii} + \sigma_{jj}\right) \\
409 \epsilon_{ij} & = & \sqrt{\epsilon_{ii}\epsilon_{jj}}
410 \end{eqnarray}
411
412 To describe the interactions between metal Au and non-metal capping
413 agent and solvent particles, we refer to an adsorption study of alkyl
414 thiols on gold surfaces by Vlugt {\it et
415 al.}\cite{vlugt:cpc2007154} They fitted an effective Lennard-Jones
416 form of potential parameters for the interaction between Au and
417 pseudo-atoms CH$_x$ and S based on a well-established and widely-used
418 effective potential of Hautman and Klein\cite{hautman:4994} for the
419 Au(111) surface. As our simulations require the gold lattice slab to
420 be non-rigid so that it could accommodate kinetic energy for thermal
421 transport study purpose, the pair-wise form of potentials is
422 preferred.
423
424 Besides, the potentials developed from {\it ab initio} calculations by
425 Leng {\it et al.}\cite{doi:10.1021/jp034405s} are adopted for the
426 interactions between Au and aromatic C/H atoms in toluene. A set of
427 pseudo Lennard-Jones parameters were provided for Au in their force
428 fields. By using the Mixing Rule, this can be used to derive pair-wise
429 potentials for non-bonded interactions between Au and non-metal sites.
430
431 However, the Lennard-Jones parameters between Au and other types of
432 particles, such as All-Atom normal alkanes in our simulations are not
433 yet well-established. For these interactions, we attempt to derive
434 their parameters using the Mixing Rule. To do this, Au pseudo
435 Lennard-Jones parameters for ``Metal-non-Metal'' (MnM) interactions
436 were first extracted from the Au-CH$_x$ parameters by applying the
437 Mixing Rule reversely. Table \ref{MnM} summarizes these ``MnM''
438 parameters in our simulations.
439
440 \begin{table*}
441 \begin{minipage}{\linewidth}
442 \begin{center}
443 \caption{Non-bonded interaction parameters (including cross
444 interactions with Au atoms) for both force fields used in this
445 work.}
446 \begin{tabular}{lllllll}
447 \hline\hline
448 & Site & $\sigma_{ii}$ & $\epsilon_{ii}$ & $q_i$ &
449 $\sigma_{Au-i}$ & $\epsilon_{Au-i}$ \\
450 & & (\AA) & (kcal/mol) & ($e$) & (\AA) & (kcal/mol) \\
451 \hline
452 United Atom (UA)
453 &CH3 & 3.75 & 0.1947 & - & 3.54 & 0.2146 \\
454 &CH2 & 3.95 & 0.0914 & - & 3.54 & 0.1749 \\
455 &CHar & 3.695 & 0.1003 & - & 3.4625 & 0.1680 \\
456 &CRar & 3.88 & 0.04173 & - & 3.555 & 0.1604 \\
457 \hline
458 All Atom (AA)
459 &CT3 & 3.50 & 0.066 & -0.18 & 3.365 & 0.1373 \\
460 &CT2 & 3.50 & 0.066 & -0.12 & 3.365 & 0.1373 \\
461 &CTT & 3.50 & 0.066 & -0.065 & 3.365 & 0.1373 \\
462 &HC & 2.50 & 0.030 & 0.06 & 2.865 & 0.09256 \\
463 &CA & 3.55 & 0.070 & -0.115 & 3.173 & 0.0640 \\
464 &HA & 2.42 & 0.030 & 0.115 & 2.746 & 0.0414 \\
465 \hline
466 Both UA and AA
467 & S & 4.45 & 0.25 & - & 2.40 & 8.465 \\
468 \hline\hline
469 \end{tabular}
470 \label{MnM}
471 \end{center}
472 \end{minipage}
473 \end{table*}
474
475
476 \section{Results and Discussions}
477 [MAY HAVE A BRIEF SUMMARY]
478 \subsection{How Simulation Parameters Affects $G$}
479 [MAY NOT PUT AT FIRST]
480 We have varied our protocol or other parameters of the simulations in
481 order to investigate how these factors would affect the measurement of
482 $G$'s. It turned out that while some of these parameters would not
483 affect the results substantially, some other changes to the
484 simulations would have a significant impact on the measurement
485 results.
486
487 In some of our simulations, we allowed $L_x$ and $L_y$ to change
488 during equilibrating the liquid phase. Due to the stiffness of the
489 crystalline Au structure, $L_x$ and $L_y$ would not change noticeably
490 after equilibration. Although $L_z$ could fluctuate $\sim$1\% after a
491 system is fully equilibrated in the NPT ensemble, this fluctuation, as
492 well as those of $L_x$ and $L_y$ (which is significantly smaller),
493 would not be magnified on the calculated $G$'s, as shown in Table
494 \ref{AuThiolHexaneUA}. This insensivity to $L_i$ fluctuations allows
495 reliable measurement of $G$'s without the necessity of extremely
496 cautious equilibration process.
497
498 As stated in our computational details, the spacing filled with
499 solvent molecules can be chosen within a range. This allows some
500 change of solvent molecule numbers for the same Au-butanethiol
501 surfaces. We did this study on our Au-butanethiol/hexane
502 simulations. Nevertheless, the results obtained from systems of
503 different $N_{hexane}$ did not indicate that the measurement of $G$ is
504 susceptible to this parameter. For computational efficiency concern,
505 smaller system size would be preferable, given that the liquid phase
506 structure is not affected.
507
508 Our NIVS algorithm allows change of unphysical thermal flux both in
509 direction and in quantity. This feature extends our investigation of
510 interfacial thermal conductance. However, the magnitude of this
511 thermal flux is not arbitary if one aims to obtain a stable and
512 reliable thermal gradient. A temperature profile would be
513 substantially affected by noise when $|J_z|$ has a much too low
514 magnitude; while an excessively large $|J_z|$ that overwhelms the
515 conductance capacity of the interface would prevent a thermal gradient
516 to reach a stablized steady state. NIVS has the advantage of allowing
517 $J$ to vary in a wide range such that the optimal flux range for $G$
518 measurement can generally be simulated by the algorithm. Within the
519 optimal range, we were able to study how $G$ would change according to
520 the thermal flux across the interface. For our simulations, we denote
521 $J_z$ to be positive when the physical thermal flux is from the liquid
522 to metal, and negative vice versa. The $G$'s measured under different
523 $J_z$ is listed in Table \ref{AuThiolHexaneUA} and
524 \ref{AuThiolToluene}. These results do not suggest that $G$ is
525 dependent on $J_z$ within this flux range. The linear response of flux
526 to thermal gradient simplifies our investigations in that we can rely
527 on $G$ measurement with only a couple $J_z$'s and do not need to test
528 a large series of fluxes.
529
530 \begin{table*}
531 \begin{minipage}{\linewidth}
532 \begin{center}
533 \caption{Computed interfacial thermal conductivity ($G$ and
534 $G^\prime$) values for the 100\% covered Au-butanethiol/hexane
535 interfaces with UA model and different hexane molecule numbers
536 at different temperatures using a range of energy
537 fluxes. Error estimates indicated in parenthesis.}
538
539 \begin{tabular}{ccccccc}
540 \hline\hline
541 $\langle T\rangle$ & $N_{hexane}$ & Fixed & $\rho_{hexane}$ &
542 $J_z$ & $G$ & $G^\prime$ \\
543 (K) & & $L_x$ \& $L_y$? & (g/cm$^3$) & (GW/m$^2$) &
544 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
545 \hline
546 200 & 266 & No & 0.672 & -0.96 & 102(3) & 80.0(0.8) \\
547 & 200 & Yes & 0.694 & 1.92 & 129(11) & 87.3(0.3) \\
548 & & Yes & 0.672 & 1.93 & 131(16) & 78(13) \\
549 & & No & 0.688 & 0.96 & 125(16) & 90.2(15) \\
550 & & & & 1.91 & 139(10) & 101(10) \\
551 & & & & 2.83 & 141(6) & 89.9(9.8) \\
552 & 166 & Yes & 0.679 & 0.97 & 115(19) & 69(18) \\
553 & & & & 1.94 & 125(9) & 87.1(0.2) \\
554 & & No & 0.681 & 0.97 & 141(30) & 78(22) \\
555 & & & & 1.92 & 138(4) & 98.9(9.5) \\
556 \hline
557 250 & 200 & No & 0.560 & 0.96 & 75(10) & 61.8(7.3) \\
558 & & & & -0.95 & 49.4(0.3) & 45.7(2.1) \\
559 & 166 & Yes & 0.570 & 0.98 & 79.0(3.5) & 62.9(3.0) \\
560 & & No & 0.569 & 0.97 & 80.3(0.6) & 67(11) \\
561 & & & & 1.44 & 76.2(5.0) & 64.8(3.8) \\
562 & & & & -0.95 & 56.4(2.5) & 54.4(1.1) \\
563 & & & & -1.85 & 47.8(1.1) & 53.5(1.5) \\
564 \hline\hline
565 \end{tabular}
566 \label{AuThiolHexaneUA}
567 \end{center}
568 \end{minipage}
569 \end{table*}
570
571 Furthermore, we also attempted to increase system average temperatures
572 to above 200K. These simulations are first equilibrated in the NPT
573 ensemble under normal pressure. As stated above, the TraPPE-UA model
574 for hexane tends to predict a lower boiling point. In our simulations,
575 hexane had diffculty to remain in liquid phase when NPT equilibration
576 temperature is higher than 250K. Additionally, the equilibrated liquid
577 hexane density under 250K becomes lower than experimental value. This
578 expanded liquid phase leads to lower contact between hexane and
579 butanethiol as well.[MAY NEED SLAB DENSITY FIGURE]
580 And this reduced contact would
581 probably be accountable for a lower interfacial thermal conductance,
582 as shown in Table \ref{AuThiolHexaneUA}.
583
584 A similar study for TraPPE-UA toluene agrees with the above result as
585 well. Having a higher boiling point, toluene tends to remain liquid in
586 our simulations even equilibrated under 300K in NPT
587 ensembles. Furthermore, the expansion of the toluene liquid phase is
588 not as significant as that of the hexane. This prevents severe
589 decrease of liquid-capping agent contact and the results (Table
590 \ref{AuThiolToluene}) show only a slightly decreased interface
591 conductance. Therefore, solvent-capping agent contact should play an
592 important role in the thermal transport process across the interface
593 in that higher degree of contact could yield increased conductance.
594
595 \begin{table*}
596 \begin{minipage}{\linewidth}
597 \begin{center}
598 \caption{Computed interfacial thermal conductivity ($G$ and
599 $G^\prime$) values for a 90\% coverage Au-butanethiol/toluene
600 interface at different temperatures using a range of energy
601 fluxes. Error estimates indicated in parenthesis.}
602
603 \begin{tabular}{ccccc}
604 \hline\hline
605 $\langle T\rangle$ & $\rho_{toluene}$ & $J_z$ & $G$ & $G^\prime$ \\
606 (K) & (g/cm$^3$) & (GW/m$^2$) & \multicolumn{2}{c}{(MW/m$^2$/K)} \\
607 \hline
608 200 & 0.933 & 2.15 & 204(12) & 113(12) \\
609 & & -1.86 & 180(3) & 135(21) \\
610 & & -3.93 & 176(5) & 113(12) \\
611 \hline
612 300 & 0.855 & -1.91 & 143(5) & 125(2) \\
613 & & -4.19 & 135(9) & 113(12) \\
614 \hline\hline
615 \end{tabular}
616 \label{AuThiolToluene}
617 \end{center}
618 \end{minipage}
619 \end{table*}
620
621 Besides lower interfacial thermal conductance, surfaces in relatively
622 high temperatures are susceptible to reconstructions, when
623 butanethiols have a full coverage on the Au(111) surface. These
624 reconstructions include surface Au atoms migrated outward to the S
625 atom layer, and butanethiol molecules embedded into the original
626 surface Au layer. The driving force for this behavior is the strong
627 Au-S interactions in our simulations. And these reconstructions lead
628 to higher ratio of Au-S attraction and thus is energetically
629 favorable. Furthermore, this phenomenon agrees with experimental
630 results\cite{doi:10.1021/j100035a033,doi:10.1021/la026493y}. Vlugt
631 {\it et al.} had kept their Au(111) slab rigid so that their
632 simulations can reach 300K without surface reconstructions. Without
633 this practice, simulating 100\% thiol covered interfaces under higher
634 temperatures could hardly avoid surface reconstructions. However, our
635 measurement is based on assuming homogeneity on $x$ and $y$ dimensions
636 so that measurement of $T$ at particular $z$ would be an effective
637 average of the particles of the same type. Since surface
638 reconstructions could eliminate the original $x$ and $y$ dimensional
639 homogeneity, measurement of $G$ is more difficult to conduct under
640 higher temperatures. Therefore, most of our measurements are
641 undertaken at $\langle T\rangle\sim$200K.
642
643 However, when the surface is not completely covered by butanethiols,
644 the simulated system is more resistent to the reconstruction
645 above. Our Au-butanethiol/toluene system had the Au(111) surfaces 90\%
646 covered by butanethiols, but did not see this above phenomena even at
647 $\langle T\rangle\sim$300K. The empty three-fold sites not occupied by
648 capping agents could help prevent surface reconstruction in that they
649 provide other means of capping agent relaxation. It is observed that
650 butanethiols can migrate to their neighbor empty sites during a
651 simulation. Therefore, we were able to obtain $G$'s for these
652 interfaces even at a relatively high temperature without being
653 affected by surface reconstructions.
654
655 \subsection{Influence of Capping Agent Coverage on $G$}
656 To investigate the influence of butanethiol coverage on interfacial
657 thermal conductance, a series of different coverage Au-butanethiol
658 surfaces is prepared and solvated with various organic
659 molecules. These systems are then equilibrated and their interfacial
660 thermal conductivity are measured with our NIVS algorithm. Figure
661 \ref{coverage} demonstrates the trend of conductance change with
662 respect to different coverages of butanethiol. To study the isotope
663 effect in interfacial thermal conductance, deuterated UA-hexane is
664 included as well.
665
666 It turned out that with partial covered butanethiol on the Au(111)
667 surface, the derivative definition for $G^\prime$
668 (Eq. \ref{derivativeG}) was difficult to apply, due to the difficulty
669 in locating the maximum of change of $\lambda$. Instead, the discrete
670 definition (Eq. \ref{discreteG}) is easier to apply, as the Gibbs
671 deviding surface can still be well-defined. Therefore, $G$ (not
672 $G^\prime$) was used for this section.
673
674 From Figure \ref{coverage}, one can see the significance of the
675 presence of capping agents. Even when a fraction of the Au(111)
676 surface sites are covered with butanethiols, the conductivity would
677 see an enhancement by at least a factor of 3. This indicates the
678 important role cappping agent is playing for thermal transport
679 phenomena on metal / organic solvent surfaces.
680
681 Interestingly, as one could observe from our results, the maximum
682 conductance enhancement (largest $G$) happens while the surfaces are
683 about 75\% covered with butanethiols. This again indicates that
684 solvent-capping agent contact has an important role of the thermal
685 transport process. Slightly lower butanethiol coverage allows small
686 gaps between butanethiols to form. And these gaps could be filled with
687 solvent molecules, which acts like ``heat conductors'' on the
688 surface. The higher degree of interaction between these solvent
689 molecules and capping agents increases the enhancement effect and thus
690 produces a higher $G$ than densely packed butanethiol arrays. However,
691 once this maximum conductance enhancement is reached, $G$ decreases
692 when butanethiol coverage continues to decrease. Each capping agent
693 molecule reaches its maximum capacity for thermal
694 conductance. Therefore, even higher solvent-capping agent contact
695 would not offset this effect. Eventually, when butanethiol coverage
696 continues to decrease, solvent-capping agent contact actually
697 decreases with the disappearing of butanethiol molecules. In this
698 case, $G$ decrease could not be offset but instead accelerated. [NEED
699 SNAPSHOT SHOWING THE PHENOMENA]
700
701 A comparison of the results obtained from differenet organic solvents
702 can also provide useful information of the interfacial thermal
703 transport process. The deuterated hexane (UA) results do not appear to
704 be much different from those of normal hexane (UA), given that
705 butanethiol (UA) is non-deuterated for both solvents. These UA model
706 studies, even though eliminating C-H vibration samplings, still have
707 C-C vibrational frequencies different from each other. However, these
708 differences in the infrared range do not seem to produce an observable
709 difference for the results of $G$. [MAY NEED SPECTRA FIGURE]
710
711 Furthermore, results for rigid body toluene solvent, as well as other
712 UA-hexane solvents, are reasonable within the general experimental
713 ranges[CITATIONS]. This suggests that explicit hydrogen might not be a
714 required factor for modeling thermal transport phenomena of systems
715 such as Au-thiol/organic solvent.
716
717 However, results for Au-butanethiol/toluene do not show an identical
718 trend with those for Au-butanethiol/hexane in that $G$ remains at
719 approximately the same magnitue when butanethiol coverage differs from
720 25\% to 75\%. This might be rooted in the molecule shape difference
721 for planar toluene and chain-like {\it n}-hexane. Due to this
722 difference, toluene molecules have more difficulty in occupying
723 relatively small gaps among capping agents when their coverage is not
724 too low. Therefore, the solvent-capping agent contact may keep
725 increasing until the capping agent coverage reaches a relatively low
726 level. This becomes an offset for decreasing butanethiol molecules on
727 its effect to the process of interfacial thermal transport. Thus, one
728 can see a plateau of $G$ vs. butanethiol coverage in our results.
729
730 \begin{figure}
731 \includegraphics[width=\linewidth]{coverage}
732 \caption{Comparison of interfacial thermal conductivity ($G$) values
733 for the Au-butanethiol/solvent interface with various UA models and
734 different capping agent coverages at $\langle T\rangle\sim$200K
735 using certain energy flux respectively.}
736 \label{coverage}
737 \end{figure}
738
739 \subsection{Influence of Chosen Molecule Model on $G$}
740 [MAY COMBINE W MECHANISM STUDY]
741
742 In addition to UA solvent/capping agent models, AA models are included
743 in our simulations as well. Besides simulations of the same (UA or AA)
744 model for solvent and capping agent, different models can be applied
745 to different components. Furthermore, regardless of models chosen,
746 either the solvent or the capping agent can be deuterated, similar to
747 the previous section. Table \ref{modelTest} summarizes the results of
748 these studies.
749
750 \begin{table*}
751 \begin{minipage}{\linewidth}
752 \begin{center}
753
754 \caption{Computed interfacial thermal conductivity ($G$ and
755 $G^\prime$) values for interfaces using various models for
756 solvent and capping agent (or without capping agent) at
757 $\langle T\rangle\sim$200K. (D stands for deuterated solvent
758 or capping agent molecules; ``Avg.'' denotes results that are
759 averages of simulations under different $J_z$'s. Error
760 estimates indicated in parenthesis.)}
761
762 \begin{tabular}{llccc}
763 \hline\hline
764 Butanethiol model & Solvent & $J_z$ & $G$ & $G^\prime$ \\
765 (or bare surface) & model & (GW/m$^2$) &
766 \multicolumn{2}{c}{(MW/m$^2$/K)} \\
767 \hline
768 UA & UA hexane & Avg. & 131(9) & 87(10) \\
769 & UA hexane(D) & 1.95 & 153(5) & 136(13) \\
770 & AA hexane & Avg. & 131(6) & 122(10) \\
771 & UA toluene & 1.96 & 187(16) & 151(11) \\
772 & AA toluene & 1.89 & 200(36) & 149(53) \\
773 \hline
774 AA & UA hexane & 1.94 & 116(9) & 129(8) \\
775 & AA hexane & Avg. & 442(14) & 356(31) \\
776 & AA hexane(D) & 1.93 & 222(12) & 234(54) \\
777 & UA toluene & 1.98 & 125(25) & 97(60) \\
778 & AA toluene & 3.79 & 487(56) & 290(42) \\
779 \hline
780 AA(D) & UA hexane & 1.94 & 158(25) & 172(4) \\
781 & AA hexane & 1.92 & 243(29) & 191(11) \\
782 & AA toluene & 1.93 & 364(36) & 322(67) \\
783 \hline
784 bare & UA hexane & Avg. & 46.5(3.2) & 49.4(4.5) \\
785 & UA hexane(D) & 0.98 & 43.9(4.6) & 43.0(2.0) \\
786 & AA hexane & 0.96 & 31.0(1.4) & 29.4(1.3) \\
787 & UA toluene & 1.99 & 70.1(1.3) & 65.8(0.5) \\
788 \hline\hline
789 \end{tabular}
790 \label{modelTest}
791 \end{center}
792 \end{minipage}
793 \end{table*}
794
795 To facilitate direct comparison, the same system with differnt models
796 for different components uses the same length scale for their
797 simulation cells. Without the presence of capping agent, using
798 different models for hexane yields similar results for both $G$ and
799 $G^\prime$, and these two definitions agree with eath other very
800 well. This indicates very weak interaction between the metal and the
801 solvent, and is a typical case for acoustic impedance mismatch between
802 these two phases.
803
804 As for Au(111) surfaces completely covered by butanethiols, the choice
805 of models for capping agent and solvent could impact the measurement
806 of $G$ and $G^\prime$ quite significantly. For Au-butanethiol/hexane
807 interfaces, using AA model for both butanethiol and hexane yields
808 substantially higher conductivity values than using UA model for at
809 least one component of the solvent and capping agent, which exceeds
810 the general range of experimental measurement results. This is
811 probably due to the classically treated C-H vibrations in the AA
812 model, which should not be appreciably populated at normal
813 temperatures. In comparison, once either the hexanes or the
814 butanethiols are deuterated, one can see a significantly lower $G$ and
815 $G^\prime$. In either of these cases, the C-H(D) vibrational overlap
816 between the solvent and the capping agent is removed.
817 [MAY NEED SPECTRA FIGURE] Conclusively, the
818 improperly treated C-H vibration in the AA model produced
819 over-predicted results accordingly. Compared to the AA model, the UA
820 model yields more reasonable results with higher computational
821 efficiency.
822
823 However, for Au-butanethiol/toluene interfaces, having the AA
824 butanethiol deuterated did not yield a significant change in the
825 measurement results. Compared to the C-H vibrational overlap between
826 hexane and butanethiol, both of which have alkyl chains, that overlap
827 between toluene and butanethiol is not so significant and thus does
828 not have as much contribution to the ``Intramolecular Vibration
829 Redistribution''[CITE HASE]. Conversely, extra degrees of freedom such
830 as the C-H vibrations could yield higher heat exchange rate between
831 these two phases and result in a much higher conductivity.
832
833 Although the QSC model for Au is known to predict an overly low value
834 for bulk metal gold conductivity\cite{kuang:164101}, our computational
835 results for $G$ and $G^\prime$ do not seem to be affected by this
836 drawback of the model for metal. Instead, our results suggest that the
837 modeling of interfacial thermal transport behavior relies mainly on
838 the accuracy of the interaction descriptions between components
839 occupying the interfaces.
840
841 \subsection{Mechanism of Interfacial Thermal Conductance Enhancement
842 by Capping Agent}
843 [OR: Vibrational Spectrum Study on Conductance Mechanism]
844
845 [MAY INTRODUCE PROTOCOL IN METHODOLOGY/COMPUTATIONAL DETAIL, EQN'S]
846
847 To investigate the mechanism of this interfacial thermal conductance,
848 the vibrational spectra of various gold systems were obtained and are
849 shown as in the upper panel of Fig. \ref{vibration}. To obtain these
850 spectra, one first runs a simulation in the NVE ensemble and collects
851 snapshots of configurations; these configurations are used to compute
852 the velocity auto-correlation functions, which is used to construct a
853 power spectrum via a Fourier transform.
854
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