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1 \documentclass[11pt]{article}
2 \usepackage{amsmath}
3 \usepackage{amssymb}
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5 \usepackage{endfloat}
6 \usepackage{caption}
7 %\usepackage{tabularx}
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12 \usepackage[ref]{overcite}
13 \pagestyle{plain} \pagenumbering{arabic} \oddsidemargin 0.0cm
14 \evensidemargin 0.0cm \topmargin -21pt \headsep 10pt \textheight
15 9.0in \textwidth 6.5in \brokenpenalty=10000
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17 % double space list of tables and figures
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22 \renewcommand\citemid{\ } % no comma in optional referenc note
23
24 \begin{document}
25
26 \title{A gentler approach to RNEMD: Non-isotropic Velocity Scaling for computing Thermal Conductivity and Shear Viscosity}
27
28 \author{Shenyu Kuang and J. Daniel
29 Gezelter\footnote{Corresponding author. \ Electronic mail: gezelter@nd.edu} \\
30 Department of Chemistry and Biochemistry,\\
31 University of Notre Dame\\
32 Notre Dame, Indiana 46556}
33
34 \date{\today}
35
36 \maketitle
37
38 \begin{doublespace}
39
40 \begin{abstract}
41
42 \end{abstract}
43
44 \newpage
45
46 %\narrowtext
47
48 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
49 % BODY OF TEXT
50 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
51
52
53
54 \section{Introduction}
55 The original formulation of Reverse Non-equilibrium Molecular Dynamics
56 (RNEMD) obtains transport coefficients (thermal conductivity and shear
57 viscosity) in a fluid by imposing an artificial momentum flux between
58 two thin parallel slabs of material that are spatially separated in
59 the simulation cell.\cite{MullerPlathe97,MullerPlathe99} The
60 artificial flux is typically created by periodically "swapping" either
61 the entire momentum vector $\vec{p}$ or single components of this
62 vector ($p_x$) between molecules in each of the two slabs. If the two
63 slabs are separated along the z coordinate, the imposed flux is either
64 directional ($J_z(p_x)$) or isotropic ($J_z$), and the response of a
65 simulated system to the imposed momentum flux will typically be a
66 velocity or thermal gradient. The transport coefficients (shear
67 viscosity and thermal conductivity) are easily obtained by assuming
68 linear response of the system,
69 \begin{eqnarray}
70 J_z(p_x) & = & -\eta \frac{\partial v_x}{\partial z}\\
71 J & = & \lambda \frac{\partial T}{\partial z}
72 \end{eqnarray}
73 RNEMD been widely used to provide computational estimates of thermal
74 conductivities and shear viscosities in a wide range of materials,
75 from liquid copper to monatomic liquids to molecular fluids
76 (e.g. ionic liquids).
77
78 RNEMD is preferable in many ways to the forward NEMD methods because
79 it imposes what is typically difficult to measure (a flux or stress)
80 and it is typically much easier to compute momentum gradients or
81 strains (the response). For similar reasons, RNEMD is also preferable
82 to slowly-converging equilibrium methods for measuring thermal
83 conductivity and shear viscosity (using Green-Kubo relations or the
84 Helfand moment approach of Viscardy {\it et
85 al.}\cite{Viscardy2007a,Viscardy2007b}) because these rely on
86 computing difficult to measure quantities.
87
88 Another attractive feature of RNEMD is that it conserves both total
89 linear momentum and total energy during the swaps (as long as the two
90 molecules have the same identity), so the swapped configurations are
91 typically samples from the same manifold of states in the
92 microcanonical ensemble.
93
94 Recently, Tenney and Maginn have discovered some problems with the
95 original RNEMD swap technique. Notably, large momentum fluxes
96 (equivalent to frequent momentum swaps between the slabs) can result
97 in "notched", "peaked" and generally non-thermal momentum
98 distributions in the two slabs, as well as non-linear thermal and
99 velocity distributions along the direction of the imposed flux ($z$).
100 Tenney and Maginn obtained reasonable limits on imposed flux and
101 self-adjusting metrics for retaining the usability of the method.
102
103 In this paper, we develop and test a method for non-isotropic velocity
104 scaling (NIVS-RNEMD) which retains the desirable features of RNEMD
105 (conservation of linear momentum and total energy, compatibility with
106 periodic boundary conditions) while establishing true thermal
107 distributions in each of the two slabs. In the next section, we
108 develop the method for determining the scaling constraints. We then
109 test the method on both single component, multi-component, and
110 non-isotropic mixtures and show that it is capable of providing
111 reasonable estimates of the thermal conductivity and shear viscosity
112 in these cases.
113
114 \section{Methodology}
115 We retain the basic idea of Muller-Plathe's RNEMD method; the periodic
116 system is partitioned into a series of thin slabs along a particular
117 axis ($z$). One of the slabs at the end of the periodic box is
118 designated the ``hot'' slab, while the slab in the center of the box
119 is designated the ``cold'' slab. The artificial momentum flux will be
120 established by transferring momentum from the cold slab and into the
121 hot slab.
122
123 Rather than using momentum swaps, we use a series of velocity scaling
124 moves. For molecules $\{i\}$ located within the hot slab,
125 \begin{equation}
126 \vec{v}_i \leftarrow \left( \begin{array}{c}
127 x \\
128 y \\
129 z \\
130 \end{array} \right) \cdot \vec{v}_i
131 \end{equation}
132 where ${x, y, z}$ are a set of 3 scaling variables for each of the
133 three directions in the system. Likewise, the molecules $\{j\}$
134 located in the cold bin will see a concomitant scaling of velocities,
135 \begin{equation}
136 \vec{v}_j \leftarrow \left( \begin{array}{c}
137 x^\prime \\
138 y^\prime \\
139 z^\prime \\
140 \end{array} \right) \cdot \vec{v}_j
141 \end{equation}
142
143 Conservation of linear momentum in each of the three directions
144 ($\alpha = x,y,z$) ties the values of the hot and cold bin scaling
145 parameters together:
146 \begin{equation}
147 P_h^\alpha + P_c^\alpha = \alpha P_h^\alpha + \alpha^\prime P_c^\alpha
148 \end{equation}
149 where
150 \begin{equation}
151 \begin{array}{rcl}
152 P_h^\alpha & = & \sum_{i = 1}^{N_h} m_i \left[\vec{v}_i\right]_\alpha \\
153 P_c^\alpha & = & \sum_{j = 1}^{N_c} m_j \left[\vec{v}_j\right]_\alpha
154 \\
155 \end{array}
156 \label{eq:momentumdef}
157 \end{equation}
158 Therefore, for each of the three directions, the cold scaling
159 parameters are a simple function of the hot scaling parameters and
160 the instantaneous linear momentum in each of the two slabs.
161 \begin{equation}
162 \alpha^\prime = 1 + (1 - \alpha) \frac{P_h^\alpha}{P_c^\alpha}.
163 \label{eq:hotcoldscaling}
164 \end{equation}
165
166 Conservation of total energy also places constraints on the scaling:
167 \begin{equation}
168 \sum_{\alpha = x,y,z} K_h^\alpha + K_c^\alpha = \sum_{\alpha = x,y,z}
169 \alpha^2 K_h^\alpha + \left(\alpha^\prime\right)^2 K_c^\alpha.
170 \end{equation}
171 where the kinetic energies, $K_h^\alpha$ and $K_c^\alpha$, are computed
172 for each of the three directions in a similar manner to the linear momenta
173 (Eq. \ref{eq:momentumdef}). Substituting in the expressions for the
174 cold scaling parameters ($\alpha^\prime$) from
175 Eq. (\ref{eq:hotcoldscaling}), we obtain the {\it constraint ellipsoid}:
176 \begin{equation}
177 C_x (1+x)^2 + C_y (1+y)^2 + C_z (1+z)^2 = 0,
178 \label{eq:constraintEllipsoid}
179 \end{equation}
180 where the constants are obtained from the instantaneous values of the
181 linear momenta and kinetic energies for the hot and cold slabs,
182 \begin{equation}
183 C_\alpha = \left( K_h^\alpha + K_c^\alpha
184 \left(\frac{P_h^\alpha}{P_c^\alpha}\right)^2\right)
185 \label{eq:constraintEllipsoidConsts}
186 \end{equation}
187 This ellipsoid defines the set of hot slab scaling parameters which can be
188 applied while preserving both linear momentum in all three directions
189 as well as total energy.
190
191 The goal of using velocity scaling variables is to transfer linear
192 momentum or kinetic energy from the cold slab to the hot slab. If the
193 hot and cold slabs are separated along the z-axis, the energy flux is
194 given simply by the increase in kinetic energy of the hot bin:
195 \begin{equation}
196 (x^2-1) K_h^x + (y^2-1) K_h^y + (z^2-1) K_h^z = J_z
197 \end{equation}
198 The expression for the energy flux can be re-written as another
199 ellipsoid centered on $(x,y,z) = 0$:
200 \begin{equation}
201 x^2 K_h^x + y^2 K_h^y + z^2 K_h^z = (J_z + K_h^x + K_h^y + K_h^z)
202 \label{eq:fluxEllipsoid}
203 \end{equation}
204 The spatial extent of the {\it flux ellipsoid} is governed both by a
205 targetted value, $J_z$ as well as the instantaneous values of the
206 kinetic energy components in the hot bin.
207
208 To satisfy an energetic flux as well as the conservation constraints,
209 it is sufficient to determine the points ${x,y,z}$ which lie on both
210 the constraint ellipsoid (Eq. \ref{eq:constraintEllipsoid}) and the
211 flux ellipsoid (Eq. \ref{eq:fluxEllipsoid}), i.e. the intersection of
212 the two ellipsoids in 3-space.
213
214
215 One may also define momentum flux (say along the x-direction) as:
216 \begin{equation}
217 (x-1) P_h^x = j_z(p_x)
218 \end{equation}
219
220
221
222
223
224 \section{Acknowledgments}
225 Support for this project was provided by the National Science
226 Foundation under grant CHE-0848243. Computational time was provided by
227 the Center for Research Computing (CRC) at the University of Notre
228 Dame. \newpage
229
230 \bibliographystyle{jcp2}
231 \bibliography{nivsRnemd}
232 \end{doublespace}
233 \end{document}
234