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Revision 4063 by gezelter, Thu Mar 13 15:44:27 2014 UTC

# Line 2 | Line 2
2   \setkeys{acs}{usetitle = true}
3  
4   \usepackage{caption}
5 % \usepackage{endfloat}
5   \usepackage{geometry}
6   \usepackage{natbib}
7   \usepackage{setspace}
# Line 16 | Line 15
15   \usepackage{tabularx}
16   \usepackage{longtable}
17   \usepackage{graphicx}
19 \usepackage{multirow}
20 \usepackage{multicol}
18   \usepackage{achemso}
19   \usepackage[version=3]{mhchem}  % this is a great package for formatting chemical reactions
23 % \usepackage[square, comma, sort&compress]{natbib}
20   \usepackage{url}
25 \pagestyle{plain} \pagenumbering{arabic} \oddsidemargin 0.0cm
26 \evensidemargin 0.0cm \topmargin -21pt \headsep 10pt \textheight
27 9.0in \textwidth 6.5in \brokenpenalty=10000
21  
22 < % double space list of tables and figures
23 < % \AtBeginDelayedFloats{\renewcomand{\baselinestretch}{1.66}}
31 < \setlength{\abovecaptionskip}{20 pt}
32 < \setlength{\belowcaptionskip}{30 pt}
22 > \title{A method for creating thermal and angular momentum fluxes in
23 >  non-periodic simulations}
24  
34 % \bibpunct{}{}{,}{s}{}{;}
35
36 % \citestyle{nature}
37 % \bibliographystyle{achemso}
38
39 \title{A Method for Creating Thermal and Angular Momentum Fluxes in Non-Periodic Systems}
40
25   \author{Kelsey M. Stocker}
26   \author{J. Daniel Gezelter}
27   \email{gezelter@nd.edu}
# Line 45 | Line 29
29  
30   \begin{document}
31  
32 + \begin{tocentry}
33 +
34 + Some journals require a graphical entry for the Table of Contents.
35 + This should be laid out ``print ready'' so that the sizing of the
36 + text is correct.
37 +
38 + Inside the \texttt{tocentry} environment, the font used is Helvetica
39 + 8\,pt, as required by \emph{Journal of the American Chemical
40 + Society}.
41 +
42 + The surrounding frame is 9\,cm by 3.5\,cm, which is the maximum
43 + permitted for  \emph{Journal of the American Chemical Society}
44 + graphical table of content entries. The box will not resize if the
45 + content is too big: instead it will overflow the edge of the box.
46 +
47 + This box and the associated title will always be printed on a
48 + separate page at the end of the document.
49 +
50 + \includegraphics{toc-entry-graphic} Some text to explain the graphic.
51 +
52 + \end{tocentry}
53 +
54 +
55   \newcolumntype{A}{p{1.5in}}
56   \newcolumntype{B}{p{0.75in}}
57  
# Line 56 | Line 63
63   %       University of Notre Dame\\
64   %       Notre Dame, Indiana 46556}
65  
66 < \date{\today}
66 > %\date{\today}
67  
68 < \maketitle
68 > %\maketitle
69  
70 < \begin{doublespace}
70 > %\begin{doublespace}
71  
72   \begin{abstract}
73  
74 < We have adapted the Velocity Shearing and Scaling Reverse Non-Equilibium Molecular Dynamics (VSS-RNEMD) method
75 < for use with non-periodic system geometries. This new method is capable of creating stable temperature and
76 < angular velocity gradients in heterogeneous non-periodic systems while conserving total energy and angular
77 < momentum. To demonstrate the method, we have computed the thermal conductivities of a gold nanoparticle and
78 < water cluster, the shear viscosity of a water cluster, the interfacial thermal conductivity of a solvated gold
79 < nanoparticle and the interfacial friction of solvated gold nanostructures.
74 >  We present a new reverse non-equilibrium molecular dynamics (RNEMD)
75 >  method that can be used with non-periodic simulation cells. This
76 >  method applies thermal and/or angular momentum fluxes between two
77 >  arbitrary regions of the simulation, and is capable of creating
78 >  stable temperature and angular velocity gradients while conserving
79 >  total energy and angular momentum.  One particularly useful
80 >  application is the exchange of kinetic energy between two concentric
81 >  spherical regions, which can be used to generate thermal transport
82 >  between nanoparticles and the solvent that surrounds them.  The
83 >  rotational couple to the solvent (a measure of interfacial friction)
84 >  is also available via this method.  As demonstrations and tests of
85 >  the new method, we have computed the thermal conductivities of gold
86 >  nanoparticles and water clusters, the shear viscosity of a water
87 >  cluster, the interfacial thermal conductivity ($G$) of a solvated
88 >  gold nanoparticle and the interfacial friction of a variety of
89 >  solvated gold nanostructures.
90  
91   \end{abstract}
92  
# Line 82 | Line 99 | Non-equilibrium Molecular Dynamics (NEMD) methods impo
99   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
100   \section{Introduction}
101  
102 < Non-equilibrium Molecular Dynamics (NEMD) methods impose a temperature or velocity {\it gradient} on a
103 < system,\cite{ASHURST:1975tg,Evans:1982zk,ERPENBECK:1984sp,MAGINN:1993hc,Berthier:2002ij,Evans:2002ai,Schelling:2
104 < 002dp,PhysRevA.34.1449,JiangHao_jp802942v} and use linear response theory to connect the resulting thermal or
105 < momentum flux to transport coefficients of bulk materials. However, for heterogeneous systems, such as phase
106 < boundaries or interfaces, it is often unclear what shape of gradient should be imposed at the boundary between
107 < materials.
102 > Non-equilibrium molecular dynamics (NEMD) methods impose a temperature
103 > or velocity {\it gradient} on a
104 > system,\cite{Ashurst:1975eu,Evans:1982oq,Erpenbeck:1984qe,Evans:1986nx,Vogelsang:1988qv,Maginn:1993kl,Hess:2002nr,Schelling:2002dp,Berthier:2002ai,Evans:2002tg,Vasquez:2004ty,Backer:2005sf,Jiang:2008hc,Picalek:2009rz}
105 > and use linear response theory to connect the resulting thermal or
106 > momentum {\it flux} to transport coefficients of bulk materials,
107 > \begin{equation}
108 > j_z(p_x) = -\eta \frac{\partial v_x}{\partial z},  \hspace{0.5in}
109 > J_z = \lambda \frac{\partial T}{\partial z}.
110 > \end{equation}
111 > Here, $\frac{\partial T}{\partial z}$ and $\frac{\partial
112 >  v_x}{\partial z}$ are the imposed thermal and momentum gradients,
113 > and as long as the imposed gradients are relatively small, the
114 > corresponding fluxes, $J_z$ and $j_z(p_x)$, have a linear relationship
115 > to the gradients.  The coefficients that provide this relationship
116 > correspond to physical properties of the bulk material, either the
117 > shear viscosity $(\eta)$ or thermal conductivity $(\lambda)$.  For
118 > systems which include phase boundaries or interfaces, it is often
119 > unclear what gradient (or discontinuity) should be imposed at the
120 > boundary between materials.
121  
122 < Reverse Non-Equilibrium Molecular Dynamics (RNEMD) methods impose an unphysical {\it flux} between different
123 < regions or ``slabs'' of the simulation box.\cite{MullerPlathe:1997xw,ISI:000080382700030,Kuang2010} The system
124 < responds by developing a temperature or velocity {\it gradient} between the two regions. The gradients which
125 < develop in response to the applied flux are then related (via linear response theory) to the transport
126 < coefficient of interest. Since the amount of the applied flux is known exactly, and measurement of a gradient
127 < is generally less complicated, imposed-flux methods typically take shorter simulation times to obtain converged
128 < results. At interfaces, the observed gradients often exhibit near-discontinuities at the boundaries between
129 < dissimilar materials. RNEMD methods do not need many trajectories to provide information about transport
130 < properties, and they have become widely used to compute thermal and mechanical transport in both homogeneous
131 < liquids and solids~\cite{MullerPlathe:1997xw,ISI:000080382700030,Maginn:2010} as well as heterogeneous
132 < interfaces.\cite{garde:nl2005,garde:PhysRevLett2009,kuang:AuThl}
122 > In contrast, reverse Non-Equilibrium Molecular Dynamics (RNEMD)
123 > methods impose an unphysical {\it flux} between different regions or
124 > ``slabs'' of the simulation
125 > box.\cite{Muller-Plathe:1997wq,Muller-Plathe:1999ao,Patel:2005zm,Shenogina:2009ix,Tenney:2010rp,Kuang:2010if,Kuang:2011ef,Kuang:2012fe,Stocker:2013cl}
126 > The system responds by developing a temperature or velocity {\it
127 >  gradient} between the two regions. The gradients which develop in
128 > response to the applied flux have the same linear response
129 > relationships to the transport coefficient of interest. Since the
130 > amount of the applied flux is known exactly, and measurement of a
131 > gradient is generally less complicated, imposed-flux methods typically
132 > take shorter simulation times to obtain converged results. At
133 > interfaces, the observed gradients often exhibit near-discontinuities
134 > at the boundaries between dissimilar materials. RNEMD methods do not
135 > need many trajectories to provide information about transport
136 > properties, and they have become widely used to compute thermal and
137 > mechanical transport in both homogeneous liquids and
138 > solids~\cite{Muller-Plathe:1997wq,Muller-Plathe:1999ao,Tenney:2010rp}
139 > as well as heterogeneous
140 > interfaces.\cite{Patel:2005zm,Shenogina:2009ix,Kuang:2010if,Kuang:2011ef,Kuang:2012fe,Stocker:2013cl}
141  
142 + The strengths of specific algorithms for imposing the flux between two
143 + different slabs of the simulation cell has been the subject of some
144 + renewed interest.  The original RNEMD approach used kinetic energy or
145 + momentum exchange between particles in the two slabs, either through
146 + direct swapping of momentum vectors or via virtual elastic collisions
147 + between atoms in the two regions.  There have been recent
148 + methodological advances which involve scaling all particle velocities
149 + in both slabs.\cite{Kuang:2010if,Kuang:2012fe} Constraint equations
150 + are simultaneously imposed to require the simulation to conserve both
151 + total energy and total linear momentum.  The most recent and simplest
152 + of the velocity scaling approaches allows for simultaneous shearing
153 + (to provide viscosity estimates) as well as scaling (to provide
154 + information about thermal conductivity).\cite{Kuang:2012fe}
155  
156 + To date, however, the RNEMD methods have only been used in periodic
157 + simulation cells where the exchange regions are physically separated
158 + along one of the axes of the simulation cell. This limits the
159 + applicability to infinite planar interfaces which are perpendicular to
160 + the applied flux.  In order to model steady-state non-equilibrium
161 + distributions for curved surfaces (e.g. hot nanoparticles in contact
162 + with colder solvent), or for regions that are not planar slabs, the
163 + method requires some generalization for non-parallel exchange regions.
164 + In the following sections, we present a new velocity shearing and
165 + scaling (VSS) RNEMD algorithm which has been explicitly designed for
166 + non-periodic simulations, and use the method to compute some thermal
167 + transport and solid-liquid friction at the surfaces of spherical and
168 + ellipsoidal nanoparticles.  
169 +
170   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
171   % **METHODOLOGY**
172   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
173 < \section{Velocity Shearing and Scaling (VSS) for non-periodic systems}
173 > \section{Velocity shearing and scaling (VSS) for non-periodic systems}
174  
175 < The periodic VSS-RNEMD approach uses a series of simultaneous velocity shearing and scaling exchanges between the two
176 < slabs.\cite{Kuang2012} This method imposes energy and momentum conservation constraints while simultaneously
177 < creating a desired flux between the two slabs. These constraints ensure that all configurations are sampled
178 < from the same microcanonical (NVE) ensemble.
175 > The original periodic VSS-RNEMD approach uses a series of simultaneous
176 > velocity shearing and scaling exchanges between the two
177 > slabs.\cite{Kuang:2012fe} This method imposes energy and linear
178 > momentum conservation constraints while simultaneously creating a
179 > desired flux between the two slabs. These constraints ensure that all
180 > configurations are sampled from the same microcanonical (NVE)
181 > ensemble.
182  
183   \begin{figure}
184   \includegraphics[width=\linewidth]{figures/npVSS}
# Line 122 | Line 190 | We have extended the VSS method for use in {\it non-pe
190   \label{fig:VSS}
191   \end{figure}
192  
193 < We have extended the VSS method for use in {\it non-periodic} simulations, in which the ``slabs'' have been
194 < generalized to two separated regions of space. These regions could be defined as concentric spheres (as in
195 < figure \ref{fig:VSS}), or one of the regions can be defined in terms of a dynamically changing ``hull''
196 < comprising the surface atoms of the cluster. This latter definition is identical to the hull used in the
197 < Langevin Hull algorithm.
193 > We have extended the VSS method for use in {\it non-periodic}
194 > simulations, in which the ``slabs'' have been generalized to two
195 > separated regions of space. These regions could be defined as
196 > concentric spheres (as in figure \ref{fig:VSS}), or one of the regions
197 > can be defined in terms of a dynamically changing ``hull'' comprising
198 > the surface atoms of the cluster. This latter definition is identical
199 > to the hull used in the Langevin Hull algorithm.\cite{Vardeman2011}
200 > For the non-periodic variant, the constraints fix both the total
201 > energy and total {\it angular} momentum of the system while
202 > simultaneously imposing a thermal and angular momentum flux between
203 > the two regions.
204  
205 < We present here a new set of constraints that are more general than the VSS constraints. For the non-periodic
206 < variant, the constraints fix both the total energy and total {\it angular} momentum of the system while
207 < simultaneously imposing a thermal and angular momentum flux between the two regions.
208 <
209 < After each $\Delta t$ time interval, the particle velocities ($\mathbf{v}_i$ and $\mathbf{v}_j$) in the two
210 < shells ($A$ and $B$) are modified by a velocity scaling coefficient ($a$ and $b$) and by a rotational shearing
211 < term ($\mathbf{c}_a$ and $\mathbf{c}_b$).
205 > After a time interval of $\Delta t$, the particle velocities
206 > ($\mathbf{v}_i$ and $\mathbf{v}_j$) in the two shells ($A$ and $B$)
207 > are modified by a velocity scaling coefficient ($a$ and $b$) and by a
208 > rotational shearing term ($\mathbf{c}_a$ and $\mathbf{c}_b$).  The
209 > scalars $a$ and $b$ collectively provide a thermal exchange between
210 > the two regions.  One of the values is larger than 1, and the other
211 > smaller. To conserve total energy and angular momentum, the values of
212 > these two scalars are coupled.  The vectors ($\mathbf{c}_a$ and
213 > $\mathbf{c}_b$) provide a relative rotational shear to the velocities
214 > of the particles within the two regions, and these vectors must also
215 > be coupled to constrain the total angular momentum.
216  
217 + Once the values of the scaling and shearing factors are known, the
218 + velocity changes are applied,
219   \begin{displaymath}
220   \begin{array}{rclcl}
221   & \underline{~~~~~~~~\mathrm{scaling}~~~~~~~~} & &
# Line 159 | Line 239 | where $\overleftrightarrow{I}_{\{a,b\}}$ is the moment
239   \mathbf{c}_b & = & + \mathbf{j}_r(\mathbf{L}) \cdot
240   \overleftrightarrow{I_b}^{-1}  \Delta t  + \langle \omega_b \rangle \label{eq:bh}
241   \end{eqnarray}
242 < where $\overleftrightarrow{I}_{\{a,b\}}$ is the moment of inertia tensor for each of the two shells.
242 > where $\overleftrightarrow{I}_{\{a,b\}}$ is the moment of inertia
243 > tensor for each of the two shells.
244  
245 < To simultaneously impose a thermal flux ($J_r$) between the shells we use energy conservation constraints,
245 > To simultaneously impose a thermal flux ($J_r$) between the shells we
246 > use energy conservation constraints,
247   \begin{eqnarray}
248   K_a - J_r \Delta t & = & a^2 \left(K_a - \frac{1}{2}\langle
249   \omega_a \rangle \cdot \overleftrightarrow{I_a} \cdot \langle \omega_a
# Line 178 | Line 260 | As the simulation progresses, the velocity transformat
260   values. The new particle velocities are computed, and the simulation continues. System configurations after the
261   transformations have exactly the same energy ({\it and} angular momentum) as before the moves.
262  
263 < As the simulation progresses, the velocity transformations can be performed on a regular basis, and the system
264 < will develop a temperature and/or angular velocity gradient in response to the applied flux. Using the slope of
265 < the radial temperature or velocity gradients, it is quite simple to obtain both the thermal conductivity
266 < ($\lambda$), interfacial thermal conductance ($G$), or rotational friction coefficients ($\Xi^{rr}$) of any
267 < non-periodic system.
263 > As the simulation progresses, the velocity transformations can be
264 > performed on a regular basis, and the system will develop a
265 > temperature and/or angular velocity gradient in response to the
266 > applied flux. Using the slope of the radial temperature or velocity
267 > gradients, it is straightforward to obtain both the thermal
268 > conductivity ($\lambda$), interfacial thermal conductance ($G$), or
269 > rotational friction coefficients ($\Xi^{rr}$) of any non-periodic
270 > system.
271  
272   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
273   % **COMPUTATIONAL DETAILS**
274   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
275   \section{Computational Details}
276  
277 < The new VSS-RNEMD methodology for non-periodic system geometries has been implemented in our group molecular
278 < dynamics code, OpenMD.\cite{openmd} We have used the new method to calculate the thermal conductance of a gold
279 < nanoparticle and SPC/E water cluster, and compared the results with previous bulk RNEMD values, as well as
280 < experiment. We have also investigated the interfacial thermal conductance and interfacial rotational friction
281 < for gold nanostructures solvated in hexane as a function of nanoparticle size and shape.
277 > The new VSS-RNEMD methodology for non-periodic system geometries has
278 > been implemented in our group molecular dynamics code,
279 > OpenMD.\cite{Meineke:2005gd,openmd} We have tested the new method to
280 > calculate the thermal conductance of a gold nanoparticle and SPC/E
281 > water cluster, and compared the results with previous bulk RNEMD
282 > values, as well as experiment. We have also investigated the
283 > interfacial thermal conductance and interfacial rotational friction
284 > for gold nanostructures solvated in hexane as a function of
285 > nanoparticle size and shape.
286  
287   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
288   % FORCE FIELD PARAMETERS
289   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
290 < \subsection{Force field parameters}
290 > \subsection{Force field}
291  
292 < Gold -- gold interactions are described by the quantum Sutton-Chen (QSC) model.\cite{PhysRevB.59.3527} The QSC
293 < parameters are tuned to experimental properties such as density, cohesive energy, and elastic moduli and
294 < include zero-point quantum corrections.
292 > Gold -- gold interactions are described by the quantum Sutton-Chen
293 > (QSC) model.\cite{PhysRevB.59.3527} The QSC parameters are tuned to
294 > experimental properties such as density, cohesive energy, and elastic
295 > moduli and include zero-point quantum corrections.
296  
297 < We have chosen the SPC/E water model for these simulations, which is particularly useful for method validation
298 < as there are many values for physical properties from previous simulations available for direct
299 < comparison.\cite{Bedrov:2000, Kuang2010}
297 > The SPC/E water model~\cite{Berendsen87} is particularly useful for
298 > validation of conductivities and shear viscosities.  This model has
299 > been used to previously test other RNEMD and NEMD approaches, and
300 > there are reported values for thermal conductivies and shear
301 > viscosities at a wide range of thermodynamic conditions that are
302 > available for direct comparison.\cite{Bedrov:2000,Kuang:2010if}
303  
304 < Hexane molecules are described by the TraPPE united atom model,\cite{TraPPE-UA.alkanes} which provides good
305 < computational efficiency and reasonable accuracy for bulk thermal conductivity values. In this model, sites are
306 < located at the carbon centers for alkyl groups. Bonding interactions, including bond stretches and bends and
307 < torsions, were used for intra-molecular sites closer than 3 bonds. For non-bonded interactions, Lennard-Jones
308 < potentials were used. We have previously utilized both united atom (UA) and all-atom (AA) force fields for
309 < thermal conductivity,\cite{kuang:AuThl,Kuang2012} and since the united atom force fields cannot populate the
310 < high-frequency modes that are present in AA force fields, they appear to work better for modeling thermal
311 < conductivity.
304 > Hexane molecules are described by the TraPPE united atom
305 > model,\cite{TraPPE-UA.alkanes} which provides good computational
306 > efficiency and reasonable accuracy for bulk thermal conductivity
307 > values. In this model, sites are located at the carbon centers for
308 > alkyl groups. Bonding interactions, including bond stretches and bends
309 > and torsions, were used for intra-molecular sites closer than 3
310 > bonds. For non-bonded interactions, Lennard-Jones potentials were
311 > used. We have previously utilized both united atom (UA) and all-atom
312 > (AA) force fields for thermal
313 > conductivity,\cite{Kuang:2011ef,Kuang:2012fe,Stocker:2013cl} and since
314 > the united atom force fields cannot populate the high-frequency modes
315 > that are present in AA force fields, they appear to work better for
316 > modeling thermal conductance at metal/ligand interfaces.
317  
318 < Gold -- hexane nonbonded interactions are governed by pairwise Lennard-Jones parameters derived from Vlugt
319 < \emph{et al}.\cite{vlugt:cpc2007154} They fitted parameters for the interaction between Au and CH$_{\emph x}$
320 < pseudo-atoms based on the effective potential of Hautman and Klein for the Au(111) surface.\cite{hautman:4994}
318 > Gold -- hexane nonbonded interactions are governed by pairwise
319 > Lennard-Jones parameters derived from Vlugt \emph{et
320 >  al}.\cite{vlugt:cpc2007154} They fitted parameters for the
321 > interaction between Au and CH$_{\emph x}$ pseudo-atoms based on the
322 > effective potential of Hautman and Klein for the Au(111)
323 > surface.\cite{hautman:4994}
324  
325   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
326   % NON-PERIODIC DYNAMICS
# Line 242 | Line 343 | In all cases, systems were fully equilibrated under no
343   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
344   \subsection{Simulation protocol}
345  
346 < In all cases, systems were fully equilibrated under non-periodic isobaric-isothermal (NPT) conditions -- using
347 < the Langevin Hull methodology\cite{Vardeman2011} -- before any non-equilibrium methods were introduced. For
348 < heterogeneous systems, the gold nanoparticles and ellipsoid were first created from a bulk lattice and
349 < thermally equilibrated before being solvated in hexane. Packmol\cite{packmol} was used to solvate previously
350 < equilibrated gold nanostructures within a spherical droplet of hexane.
346 > In all cases, systems were equilibrated under non-periodic
347 > isobaric-isothermal (NPT) conditions -- using the Langevin Hull
348 > methodology\cite{Vardeman2011} -- before any non-equilibrium methods
349 > were introduced. For heterogeneous systems, the gold nanoparticles and
350 > ellipsoids were created from a bulk fcc lattice and were thermally
351 > equilibrated before being solvated in hexane.  Packmol\cite{packmol}
352 > was used to solvate previously equilibrated gold nanostructures within
353 > a spherical droplet of hexane.
354  
355 < Once fully equilibrated, a thermal or angular momentum flux was applied for 1 - 2
356 < ns, until a stable temperature or angular velocity gradient had developed. Systems containing liquids were run
357 < under moderate pressure (5 atm) and temperatures (230 K) to avoid the formation of a substantial vapor phase at the boundary of the cluster. Pressure was applied to the system via the non-periodic convex Langevin Hull. Thermal coupling to the external temperature and pressure bath was removed to avoid interference with any
358 < imposed flux.
355 > Once equilibrated, thermal or angular momentum fluxes were applied for
356 > 1 - 2 ns, until stable temperature or angular velocity gradients had
357 > developed. Systems containing liquids were run under moderate pressure
358 > (5 atm) and temperatures (230 K) to avoid the formation of a vapor
359 > layer at the boundary of the cluster.  Pressure was applied to the
360 > system via the non-periodic Langevin Hull.\cite{Vardeman2011} However,
361 > thermal coupling to the external temperature and pressure bath was
362 > removed to avoid interference with the imposed RNEMD flux.
363  
364 < To stabilize the gold nanoparticle under the imposed angular momentum flux we altered the gold atom at the
365 < designated coordinate origin to have $10,000$ times its original mass. The nonbonded interactions remain
366 < unchanged and the heavy atom is excluded from the angular momentum exchange. For rotation of the ellipsoid about
367 < its long axis we have added two heavy atoms along the axis of rotation, one at each end of the rod. We collected angular velocity data for the heterogeneous systems after a brief VSS-RNEMD simulation to initialize rotation of the solvated nanostructure. Doing so ensures that we overcome the initial static friction and calculate only the \emph{dynamic} interfacial rotational friction.
364 > Because the method conserves \emph{total} angular momentum, systems
365 > which contain a metal nanoparticle embedded in a significant volume of
366 > solvent will still experience nanoparticle diffusion inside the
367 > solvent droplet.  To aid in computing the rotational friction in these
368 > systems, a single gold atom at the origin of the coordinate system was
369 > assigned a mass $10,000 \times$ its original mass. The bonded and
370 > nonbonded interactions for this atom remain unchanged and the heavy
371 > atom is excluded from the RNEMD exchanges.  The only effect of this
372 > gold atom is to effectively pin the nanoparticle at the origin of the
373 > coordinate system, while still allowing for rotation. For rotation of
374 > the gold ellipsoids we added two of these heavy atoms along the axis
375 > of rotation, separated by an equal distance from the origin of the
376 > coordinate system.  These heavy atoms prevent off-axis tumbling of the
377 > nanoparticle and allow for measurement of rotational friction relative
378 > to a particular axis of the ellipsoid.
379  
380 + Angular velocity data was collected for the heterogeneous systems
381 + after a brief period of imposed flux to initialize rotation of the
382 + solvated nanostructure. Doing so ensures that we overcome the initial
383 + static friction and calculate only the \emph{dynamic} interfacial
384 + rotational friction.
385 +
386   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
387   % THERMAL CONDUCTIVITIES
388   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
389   \subsection{Thermal conductivities}
390  
391 < Fourier's Law of heat conduction in radial coordinates yields an expression for the heat flow between the
392 < concentric spherical RNEMD shells:
393 <
391 > To compute the thermal conductivities of bulk materials, Fourier's Law
392 > of heat conduction in radial coordinates yields an expression for the
393 > heat flow between the concentric spherical shells:
394   \begin{equation}
395          q_r = - \frac{4 \pi \lambda (T_b - T_a)}{\frac{1}{r_a} - \frac{1}{r_b}}
396   \label{eq:Q}
397   \end{equation}
398 + where $\lambda$ is the thermal conductivity, and $T_{a,b}$ and
399 + $r_{a,b}$ are the temperatures and radii of the two RNEMD regions,
400 + respectively.
401  
402 < where $\lambda$ is the thermal conductivity, and $T_{a,b}$ and $r_{a,b}$ are the temperatures and radii of the
403 < two RNEMD regions, respectively.
404 <
405 < A thermal flux is created using VSS-RNEMD moves, and the temperature in each of the radial shells is recorded.
406 < The resulting temperature profiles are analyzed to yield information about the interfacial thermal conductance.
407 < As the simulation progresses, the VSS moves are performed on a regular basis, and the system develops a thermal
408 < or velocity gradient in response to the applied flux. Once a stable thermal gradient has been established
409 < between the two regions, the thermal conductivity, $\lambda$, can be calculated using a linear regression of
410 < the thermal gradient, $\langle \frac{dT}{dr} \rangle$:
402 > A thermal flux is created using VSS-RNEMD moves, and the temperature
403 > in each of the radial shells is recorded.  The resulting temperature
404 > profiles are analyzed to yield information about the interfacial
405 > thermal conductance.  As the simulation progresses, the VSS moves are
406 > performed on a regular basis, and the system develops a thermal or
407 > velocity gradient in response to the applied flux. Once a stable
408 > thermal gradient has been established between the two regions, the
409 > thermal conductivity, $\lambda$, can be calculated using a linear
410 > regression of the thermal gradient, $\langle \frac{dT}{dr} \rangle$:
411  
412   \begin{equation}
413          \lambda = \frac{r_a}{r_b} \frac{q_r}{4 \pi \langle \frac{dT}{dr} \rangle}
# Line 378 | Line 506 | that the interface exists within ``slip'' boundary con
506   corresponding to rotation about the long axis ($a$), and each of the equivalent short axes ($b$ and $c$), respectively.
507  
508   Previous VSS-RNEMD simulations of the interfacial friction of the planar Au(111) / hexane interface have shown
509 < that the interface exists within ``slip'' boundary conditions.\cite{Kuang2012} Hu and Zwanzig\cite{Zwanzig}
509 > that the interface exists within ``slip'' boundary conditions.\cite{Kuang:2012fe} Hu and Zwanzig\cite{Zwanzig}
510   investigated the rotational friction coefficients for spheroids under slip boundary conditions and obtained
511   numerial results for a scaling factor to be applied to $\Xi^{rr}_{\mathit{stick}}$ as a function of $\tau$, the
512   ratio of the shorter semiaxes and the longer semiaxis of the spheroid. For the sphere and prolate ellipsoid
# Line 435 | Line 563 | flux $J_r$. Calculated thermal conductivity values com
563   \end{longtable}
564  
565   The measured linear slope $\langle \frac{dT}{dr} \rangle$ is linearly dependent on the applied kinetic energy
566 < flux $J_r$. Calculated thermal conductivity values compare well with previous bulk QSC values of 1.08 -- 1.26 W / m $\cdot$ K\cite{Kuang2010}, though still significantly lower than the experimental value
566 > flux $J_r$. Calculated thermal conductivity values compare well with previous bulk QSC values of 1.08 -- 1.26 W / m $\cdot$ K\cite{Kuang:2010if}, though still significantly lower than the experimental value
567   of 320 W / m $\cdot$ K, as the QSC force field neglects significant electronic contributions to
568   heat conduction.
569  
# Line 540 | Line 668 | Most strikingly, this method enables calculation of th
668   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
669   % **ACKNOWLEDGMENTS**
670   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
671 < \section*{Acknowledgments}
671 > \begin{acknowledgement}
672 >  The authors thank Dr. Shenyu Kuang for helpful discussions. Support
673 >  for this project was provided by the National Science Foundation
674 >  under grant CHE-0848243. Computational time was provided by the
675 >  Center for Research Computing (CRC) at the University of Notre Dame.
676 > \end{acknowledgement}
677  
545 We gratefully acknowledge conversations with Dr. Shenyu Kuang. Support for this project was provided by the
546 National Science Foundation under grant CHE-0848243. Computational time was provided by the Center for Research
547 Computing (CRC) at the University of Notre Dame.
678  
679   \newpage
680  
681   \bibliography{nonperiodicVSS}
682  
683 < \end{doublespace}
683 > %\end{doublespace}
684   \end{document}

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