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# Content
1 \documentclass[journal = jpccck, manuscript = article]{achemso}
2 \setkeys{acs}{usetitle = true}
3 \usepackage{achemso}
4 \usepackage{natbib}
5 \usepackage{multirow}
6 \usepackage{wrapfig}
7 \usepackage{fixltx2e}
8 %\mciteErrorOnUnknownfalse
9
10 \usepackage[version=3]{mhchem} % this is a great package for formatting chemical reactions
11 \usepackage{url}
12
13
14 \title{Do the facets of ice $I_\mathrm{h}$ crystals have different
15 friction coefficients? Simulating shear in ice/water interfaces}
16
17 \author{P. B. Louden}
18 \author{J. Daniel Gezelter}
19 \email{gezelter@nd.edu}
20 \affiliation[University of Notre Dame]{251 Nieuwland Science Hall\\
21 Department of Chemistry and Biochemistry\\ University of Notre
22 Dame\\ Notre Dame, Indiana 46556}
23
24 \keywords{}
25
26 \begin{document}
27
28 \begin{abstract}
29 We have investigated the structural properties of the basal and
30 prismatic facets of an SPC/E model of the ice Ih / water interface
31 when the solid phase is being drawn through liquid water (i.e. sheared
32 relative to the fluid phase). To impose the shear, we utilized a
33 reverse non-equilibrium molecular dynamics (RNEMD) method that creates
34 non-equilibrium conditions using velocity shearing and scaling (VSS)
35 moves of the molecules in two physically separated slabs in the
36 simulation cell. This method can create simultaneous temperature and
37 velocity gradients and allow the measurement of friction transport
38 properties at interfaces. We present calculations of the interfacial
39 friction coefficients and the apparent independence of shear rate on
40 interfacial width and show that water moving over a flat ice/water
41 interface is close to the no-slip boundary condition.
42 \end{abstract}
43
44 \newpage
45
46 \section{Introduction}
47
48 %Other people looking at the ice/water interface
49 %Geologists are concerned with the flow of water over ice
50 %Antifreeze protein in fish--Haymet's group has cited this before
51
52 %Paragraph explaining why the ice/water interface is important
53 %Paragraph on what other people have done / lead into what hasn't been done
54 %Paragraph on what I'm going to do
55
56
57
58
59 With the recent development of velocity shearing and scaling reverse non-equilibrium molecular dynamics (VSS-RNEMD), it is now possible to calculate transport properties from heterogeneous systems.\cite{Kuang12} This method can create simultaneous temperature and velocity gradients and allow the measurement of friction and thermal transport properties at interfaces. This allows for the study of the width of the ice/water interface as the ice is sheared through the liquid, while imposing a thermal gradient to prevent frictional heating of the interface.
60
61 as well as determining the friction coefficient of the interface.
62
63 In this paper, we investigate the width and the friction coefficient of the ice/water interface as the ice is sheared through the liquid.
64
65
66
67 \section{Methodology}
68
69 \subsection{Stable ice I$_\mathrm{h}$ / water interfaces}
70
71 The structure of ice I$_\mathrm{h}$ is well understood; it
72 crystallizes in a hexagonal space group P$6_3/mmc$, and the hexagonal
73 crystals of ice have two faces that are commonly exposed, the basal
74 face $\{0~0~0~1\}$, which forms the top and bottom of each hexagonal
75 plate, and the prismatic $\{1~0~\bar{1}~0\}$ face which forms the
76 sides of the plate. Other less-common, but still important, faces of
77 ice I$_\mathrm{h}$ are the secondary prism face, $\{1~1~\bar{2}~0\}$,
78 and the prismatic face, $\{2~0~\bar{2}~1\}$.
79
80 Ice I$_\mathrm{h}$ is normally proton disordered in bulk crystals,
81 although the surfaces probably have a preference for proton ordering
82 along strips of dangling H-atoms and Oxygen lone
83 pairs.\cite{Buch:2008fk}
84
85 For small simulated ice interfaces, it is useful to have a
86 proton-ordered, but zero-dipole crystal that exposes these strips of
87 dangling H-atoms and lone pairs. Also, if we're going to place
88 another material in contact with one of the ice crystalline planes, it
89 is useful to have an orthorhombic (rectangular) box to work with. A
90 recent paper by Hirsch and Ojam\"{a}e describes how to create
91 proton-ordered bulk ice I$_\mathrm{h}$ in alternative orthorhombic
92 cells.\cite{Hirsch04}
93
94 We have using Hirsch and Ojam\"{a}e's structure 6 which is an
95 orthorhombic cell ($P2_12_12_1$) that produces a proton-ordered
96 version of ice Ih. Table \ref{tab:equiv} contains a mapping between
97 the Miller indices in the P$6_3/mmc$ crystal system and those in the
98 Hirsch and Ojam\"{a}e $P2_12_12_1$ system.
99
100 \begin{wraptable}{r}{3.5in}
101 \begin{tabular}{|ccc|} \hline
102 & hexagonal & orthorhombic \\
103 & ($P6_3/mmc$) & ($P2_12_12_1$) \\
104 crystal face & Miller indices & equivalent \\ \hline
105 basal & $\{0~0~0~1\}$ & $\{0~0~1\}$ \\
106 prism & $\{1~0~\bar{1}~0\}$ & $\{1~0~0\}$ \\
107 secondary prism & $\{1~1~\bar{2}~0\}$ & $\{1~3~0\}$ \\
108 pryamidal & $\{2~0~\bar{2}~1\}$ & $\{2~0~1\}$ \\ \hline
109 \end{tabular}
110 \end{wraptable}
111
112 Structure 6 from the Hirsch and Ojam\"{a}e paper has lattice
113 parameters $a = 4.49225$, $b = 7.78080$, $c = 7.33581$ and two water
114 molecules whose atoms reside at the following fractional coordinates:
115
116 \begin{wraptable}{r}{3.25in}
117 \begin{tabular}{|ccccc|} \hline
118 atom label & type & x & y & z \\ \hline
119 O$_{a}$ & O & 0.75 & 0.1667 & 0.4375 \\
120 H$_{1a}$ & H & 0.5735 & 0.2202 & 0.4836 \\
121 H$_{2a}$ & H & 0.7420 & 0.0517 & 0.4836 \\
122 O$_{b}$ & O & 0.25 & 0.6667 & 0.4375 \\
123 H$_{1b}$ & H & 0.2580 & 0.6693 & 0.3071 \\
124 H$_{2b}$ & H & 0.4265 & 0.7255 & 0.4756 \\ \hline
125 \end{tabular}
126 \end{wraptable}
127
128 To construct the basal and prismatic interfaces, the crystallographic
129 coordinates above were used to construct an orthorhombic unit cell
130 which was then replicated in all three dimensions yielding a
131 proton-ordered block of ice I$_{h}$. To expose the desired face, the
132 orthorhombic representation was then cut along the ($001$) or ($100$)
133 planes for the basal and prismatic faces respectively. The resulting
134 block was rotated so that the exposed faces were aligned with the $z$
135 axis normal to the exposed face. The block was then cut along two
136 perpendicular directions in a way that allowed for perfect periodic
137 replication in the $x$ and $y$ axes, creating a slab with either the
138 basal or prismatic faces exposed along the $z$ axis. The slab was
139 then replicated in the $x$ and $y$ dimensions until a desired sample
140 size was obtained.
141
142 Although experimental solid/liquid coexistant temperature under normal
143 pressure are close to 273K, Haymet \emph{et al.} have done extensive
144 work on characterizing the ice/water
145 interface.\cite{Karim88,Karim90,Hayward01,Bryk02,Hayward02} They have
146 found for the SPC/E water model,\cite{Berendsen87} which is also used
147 in this study, the ice/water interface is most stable at
148 225$\pm$5K.\cite{Bryk02} To create a ice / water interface, a box of
149 liquid water that had the same dimensions in $x$ and $y$ was
150 equilibrated at 225 K and 1 atm of pressure in the NPAT ensemble (with
151 the $z$ axis allowed to fluctuate to equilibrate to the correct
152 pressure). The liquid and solid systems were combined by carving out
153 any water molecule from the liquid simulation cell that was within 3
154 \AA\ of any atom in the ice slab.
155
156 Molecular translation and orientational restraints were applied in the
157 early stages of equilibration to prevent melting of the ice slab.
158 These restraints were removed during NVT equilibration, well before
159 data collection was carried out.
160
161 \subsection{Shearing ice / water interfaces without bulk melting}
162
163 As one drags a solid through a liquid, there will be frictional
164 heating that will act to melt the interface. To study the frictional
165 behavior of the interface without causing the interface to melt, it is
166 necessary to apply a weak thermal gradient along with the momentum
167 gradient. This can be accomplished with of the newly-developed
168 approaches to reverse non-equilibrium molecular dynamics (RNEMD). The
169 velocity shearing and scaling (VSS) variant of RNEMD utilizes a series
170 of simultaneous velocity exchanges between two regions within the
171 simulation cell.\cite{Kuang12} One of these regions is centered within
172 the ice slab, while the other is centrally located in the liquid phase
173 region. VSS-RNEMD provides a set of conservation constraints for
174 simultaneously creating either a momentum flux or a thermal flux (or
175 both) between the two slabs. Satisfying the constraint equations
176 ensures that the new configurations are sampled from the same NVE
177 ensemble as previously.
178
179 The VSS moves are applied periodically to scale and shift the particle
180 velocities ($\mathbf{v}_i$ and $\mathbf{v}_j$) in two slabs ($H$ and
181 $C$) which are separated by half of the simulation box,
182 \begin{displaymath}
183 \begin{array}{rclcl}
184
185 & \underline{\mathrm{shearing}} & &
186 \underline{~~~~~~~~~~~~\mathrm{scaling}~~~~~~~~~~~~} \\
187 \mathbf{v}_i \leftarrow &
188 \mathbf{a}_c\ & + & c\cdot\left(\mathbf{v}_i - \langle\mathbf{v}_c
189 \rangle\right) + \langle\mathbf{v}_c\rangle \\
190 \mathbf{v}_j \leftarrow &
191 \mathbf{a}_h & + & h\cdot\left(\mathbf{v}_j - \langle\mathbf{v}_h
192 \rangle\right) + \langle\mathbf{v}_h\rangle .
193
194 \end{array}
195 \end{displaymath}
196 Here $\langle\mathbf{v}_c\rangle$ and $\langle\mathbf{v}_h\rangle$ are
197 the center of mass velocities in the $C$ and $H$ slabs, respectively.
198 Within the two slabs, particles receive incremental changes or a
199 ``shear'' to their velocities. The amount of shear is governed by the
200 imposed momentum flux, $\mathbf{j}_z(\mathbf{p})$
201 \begin{eqnarray}
202 \mathbf{a}_c & = & - \mathbf{j}_z(\mathbf{p}) \Delta t / M_c \label{vss1}\\
203 \mathbf{a}_h & = & + \mathbf{j}_z(\mathbf{p}) \Delta t / M_h \label{vss2}
204 \end{eqnarray}
205 where $M_{\{c,h\}}$ is the total mass of particles within each of the
206 slabs and $\Delta t$ is the interval between two separate operations.
207
208 To simultaneously impose a thermal flux ($J_z$) between the slabs we
209 use energy conservation constraints,
210 \begin{eqnarray}
211 K_c - J_z\Delta t & = & c^2 (K_c - \frac{1}{2}M_c \langle\mathbf{v}_c
212 \rangle^2) + \frac{1}{2}M_c (\langle \mathbf{v}_c \rangle + \mathbf{a}_c)^2 \label{vss3}\\
213 K_h + J_z\Delta t & = & h^2 (K_h - \frac{1}{2}M_h \langle\mathbf{v}_h
214 \rangle^2) + \frac{1}{2}M_h (\langle \mathbf{v}_h \rangle +
215 \mathbf{a}_h)^2 \label{vss4}.
216 \label{constraint}
217 \end{eqnarray}
218 Simultaneous solution of these quadratic formulae for the scaling
219 coefficients, $c$ and $h$, will ensure that the simulation samples from
220 the original microcanonical (NVE) ensemble. Here $K_{\{c,h\}}$ is the
221 instantaneous translational kinetic energy of each slab. At each time
222 interval, it is a simple matter to solve for $c$, $h$, $\mathbf{a}_c$,
223 and $\mathbf{a}_h$, subject to the imposed momentum flux,
224 $j_z(\mathbf{p})$, and thermal flux, $J_z$, values. Since the VSS
225 operations do not change the kinetic energy due to orientational
226 degrees of freedom or the potential energy of a system, configurations
227 after the VSS move have exactly the same energy (and linear
228 momentum) as before the move.
229
230 As the simulation progresses, the VSS moves are performed on a regular
231 basis, and the system develops a thermal and/or velocity gradient in
232 response to the applied flux. In a bulk material it is quite simple
233 to use the slope of the temperature or velocity gradients to obtain
234 the thermal conductivity or shear viscosity.
235
236 The VSS-RNEMD approach is versatile in that it may be used to
237 implement thermal and shear transport simultaneously. Perturbations
238 of velocities away from the ideal Maxwell-Boltzmann distributions are
239 minimal, as is thermal anisotropy. This ability to generate
240 simultaneous thermal and shear fluxes has been previously utilized to
241 map out the shear viscosity of SPC/E water over a wide range of
242 temperatures (90~K) with a single 1 ns simulation.\cite{Kuang12}
243
244 Here we are using this method primarily to generate a shear between
245 the ice slab and the liquid phase, while using a weak thermal gradient
246 to maintaining the interface at the 225K target value. This will
247 insure minimal melting of the bulk ice phase and allows us to control
248 the exact temperature of the interface.
249
250 \subsection{Computational Details}
251 All simulations were performed using OpenMD with a time step of 2 fs,
252 and periodic boundary conditions in all three dimensions. The systems
253 were divided into 100 artificial bins along the $z$-axis for the
254 VSS-RNEMD moves, which were attempted every 50 fs. The gradients were
255 allowed to develop for 1 ns before data collection was began. Once
256 established, snapshots of the system were taken every 1 ps, and the
257 average velocities and densities of each bin were accumulated every
258 attempted VSS-RNEMD move.
259
260 %A paragraph on the equilibration procedure of the system? Shenyu did some amount of equilibration to the files and then I was handed them. I performed 5 ns of NVT at 225K for both systems, then 5 ns of NVE at 225K for both systems, with no gradients imposed.
261 %For the basal, once the thermal gradient was found which gave me the interfacial temperature I wanted (-2.0E-6 kcal/mol/A^2/fs), I equilibrated the file for 5 ns letting this gradient stabilize. Then I continued to use this thermal gradient as I imposed momentum gradients and watched the response of the interface.
262 %For the prismatic, a gradient was not found that would give me the interfacial temperature I desired, so while imposing a thermal gradient that had the interface at 220K, I raised the temperature of the system to 230K. This resulted in a thermal gradient which gave my interface at 225K, equilibrated for ins NVT, then ins NVE while this gradient was still imposed, then I began dragging.
263 %I have run each system for 1 ns under PTgrads to allow them to develop, then ran each system for an additional 2 ns in segments of 0.5 ns in order to calculate statistics of the calculated values.
264
265 \subsection{Measuring the Width of the Interface}
266 In order to characterize the ice/water interface, the local
267 tetrahedral order parameter as described by Kumar\cite{Kumar09} and
268 Errington\cite{Errington01} was used. The local tetrahedral order
269 parameter, $q$, is given by
270 \begin{equation}
271 q_{k} \equiv 1 -\frac{3}{8}\sum_{i=1}^{3} \sum_{j=i+1}^{4} \Bigg[\cos\psi_{ikj}+\frac{1}{3}\Bigg]^2
272 \end{equation}
273 where $\psi_{ikj}$ is the angle formed by the oxygen sites on molecule $k$, and the oxygen site on its two closest neighbors, molecules $i$ and $j$. The local tetrahedral order parameter function has a range of (0,1), where the larger the value $q$ has the more tetrahedral the ordering of the local environment is. A $q$ value of one describes a perfectly tetrahedral environment relative to it and its four nearest neighbors, and the parameter's value decreases as the local ordering becomes less tetrahedral.
274
275 %If the central water molecule has a perfect tetrahedral geometry with its four nearest neighbors, the parameter goes to one, and decreases to zero as the geometry deviates from the ideal configuration.
276
277 The system was divided into 100 bins along the $z$-axis, and a $q$ value was determined for each snapshot of the system for each bin. The $q$ values for each bin were then averaged to give an average tetrahedrally profile of the system about the $z$- axis. The profile was then fit with a hyperbolic tangent function given by
278 \begin{equation}
279 q_{z}=q_{liq}+\frac{q_{ice}-q_{liq}}{2}(\tanh(\alpha(z-I_{L,m}))-\tanh(\alpha(z-I_{R,m})))
280 \end{equation}
281 where $q_{liq}$ and $q_{ice}$ are fitting parameters for the local tetrahedral order parameter for the liquid and ice, $\alpha$ is proportional to the inverse of the width of the interface, and $I_{L,m}$ and $I_{R,m}$ are the midpoints of the left and right interface. During the simulations where a kinetic energy flux was imposed, there was found to be a thermal influence in the liquid phase region of the tetrahedrally profile due to the thermal gradient developed in the system. To maximize the fit of the interface, another term was added to the hyperbolic tangent fitting function,
282 \begin{equation}
283 q_{z}=q_{liq}+\frac{q_{ice}-q_{liq}}{2}(\tanh(\alpha(z-I_{L,m}))-\tanh(\alpha(z-I_{R,m})))+\beta|(z-z_{mid})|
284 \end{equation}
285 where $\beta$ is a fitting parameter and $z_{mid}$ is the midpoint of the z dimension of the simulation box.
286
287
288 \section{Results and discussion}
289
290 %Images to include: 3-long comic strip style of <Vx>, T, q_z as a function of z for the basal and prismatic faces. q_z by z with fit for basal and prismatic. interface width as a function of deltaVx (shear rate) with basal and prismatic on the same plot, error bars in the x and y. <Vx> by flux with basal and prismatic on same graph, back out slope from xmgr and error in slope to get lambda, friction coefficient of interface.
291
292 In Figures \ref{fig:bComic} and \ref{fig:pComic} we see the $z$-dimensional profiles for several parameters for the basal and prismatic systems respectively. In panel (a) of the figures we see the tetrahedrality profile of the systems (black circles). In the liquid region of the system, the local tetrahedral order parameter is approximately 0.75. In the solid region, the parameter is approximately 0.94, indicating a more tetrahedral structure of the water molecules. The hyperbolic tangent function used to fit the tetrahedrality profiles can be found in red and the verticle dotted lines denote the midpoint of the interfaces. The weak thermal gradient applied to the systems in order to keep the interface at a stable temperature, 225$\pm$5K, can be seen in panel (b). Lastly, the velocity gradient across the systems can be seen in panel (c). From panel (c), we can see liquid phase water molecules 5 to 12 \AA\ from the midpoint of the basal and prismatic interfaces are being dragged along with the ice block. This indicates that the shearing of ice water is in the stick boundary condition.
293
294 \begin{figure}
295 \includegraphics[width=\linewidth]{bComicStrip}
296 \caption{\label{fig:bComic} The basal system: (a) The local tetrahedral order parameter,$q$, (black circles) fit by a hyperbolic tangent (red line), (b) the thermal gradient imposed on the system to maintain a stable interfacial temperature, and (c) the velocity gradient imposed on the system. The verticle dotted lines indicate the midpoint of the interfaces.}
297 \end{figure}
298
299 %(a) The local tetrahedral order parameter across the z-dimension of the system (black circles) fit by a hyperbolic tangent (red line). (b) The thermal gradient imposed on the system to maintain a stable interfacial temperature. (c) The velocity gradient imposed on the system. The verticle dotted lines indicate the midpoint of the interfaces.
300
301 \begin{figure}
302 \includegraphics[width=\linewidth]{pComicStrip}
303 \caption{\label{fig:pComic} The prismatic system: (a) The local tetrahedral order parameter,$q$, (black circles) fit by a hyperbolic tangent (red line), (b) the thermal gradient imposed on the system to maintain a stable interfacial temperature, and (c) the velocity gradient imposed on the system.The verticle dotted lines indicate the midpoint of the interfaces.}
304 \end{figure}
305
306
307 \subsection{Interfacial Width}
308 %For the basal and prismatic systems, the ice blocks were sheared through the water at varying rates while an imposed thermal gradient kept the interface at the stable temperature range as described by Byrk and Haymet.
309 We found the interfacial width for the basal and prismatic systems to be 3.2$\pm$0.4 \AA\ and 3.6$\pm$0.2 \AA\ with no applied momentum flux. Over the range of shear rates investigated, 0.6$\pm$0.3 ms\textsuperscript{-1} to 5.3$\pm$0.5 ms\textsuperscript{-1} for the basal system and 0.9$\pm$0.2 ms\textsuperscript{-1} to 4.5$\pm$0.1 ms\textsuperscript{-1}, there was no appreciable change in the interface width found. The calculated values for the interfacial width over all shear rates investigated contained the control values within their error bars.
310
311 \subsection{Coefficient of Friction of the Interface}
312 As the ice is sheared through the liquid, there will be a friction between the ice and the interface. Balasubramanian has shown how to calculate the coefficient of friction for a solid-liquid interface. \cite{Balasubramanian99}
313 \begin{equation}
314 %<F_{x}^{w}>_{NE}(t)=-S\lambda_{wall}v_{x}(y_{wall})
315 \langle F_{x}^{w}\rangle(t)=-S\lambda_{wall}v_{x}(y_{wall})
316 \end{equation}
317 In this equation, $F_{x}^{w}$ is the total force of all the atoms acting on the fluid, $S$ is the surface area the force is being applied upon, and $\lambda_{wall}$ is the coefficient of friction of the interface. Since the imposed momentum flux, $J_{z}(p_{x})$, is known in the VSS-RNEMD simulations, and the $wall$ is the ice block in our simulations, the above equation can be rewritten as
318 \begin{equation}
319 J_{z}(p_{x})=-\lambda_{ice}v_{x}(y_{ice}).
320 \end{equation}
321
322 In Figure \ref{fig:CoeffFric}, the average velocity of the ice is plotted against the imposed momentum flux for the basal (black circles) and prismatic (red circles) systems. From the equation above, the slope of the linear fit of the data is $\lambda_{wall}$. The coefficient of friction of the interface for the basal face was calculated to be 11.0 $\pm$ 0.4 \AA\textsuperscript{-2}fs\textsuperscript{-1}, and the $\lambda_{wall}$ for the prismatic face was determined to be 19.9, $\pm$ 0.5 \AA\textsuperscript{-2}fs\textsuperscript{-1}.
323
324 %Ask dan about truncating versus rounding the values for lambda.
325 %The coefficient of friction of the interface for the basal face was calculated to be 11.02808 $\pm$ 0.4489844 \AA^{-2}fs^{-1}, and the $\lambda_{wall}$ for the prismatic face was determined to be 19.95948, $\pm$ 0.5370894 \AA^{-2}fs^{-1}.
326 \begin{figure}
327 \includegraphics[width=\linewidth]{CoeffFric}
328 \caption{\label{fig:CoeffFric} The average velocity of the ice for the basal (black circles) and prismatic (red circles) systems as a function off applied momentum flux. The slope of the fit line }
329 \end{figure}
330
331 \section{Conclusion}
332 Here we have simulated the basal and prismatic facets of an SPC/E model of the ice Ih / water interface. Using VSS-RNEMD, the ice was sheared relative to the liquid while imposed thermal gradients kept the interface at a stable temperature. Caculation of the local tetrahedrality order parameter has shown an appearant independence of the shear rate on the interfacial width. The coefficient of friction of the interface was also calculated for each of the facets. The $\lambda_{wall}$ for the basal face was calculated to be 11.0 $\pm$ 0.4 \AA\textsuperscript{-2}fs\textsuperscript{-1}, and 19.9, $\pm$ 0.5 \AA\textsuperscript{-2}fs\textsuperscript{-1} for the prismatic facet. For both facets, the shearing ice water was found to be in the no-slip boundary condition.
333
334
335 \begin{acknowledgement}
336 Support for this project was provided by the National Science
337 Foundation under grant CHE-0848243. Computational time was provided
338 by the Center for Research Computing (CRC) at the University of
339 Notre Dame.
340 \end{acknowledgement}
341
342 \newpage
343 \bibstyle{achemso}
344 \bibliography{iceWater}
345
346 \begin{tocentry}
347 \begin{wrapfigure}{l}{0.5\textwidth}
348 \begin{center}
349 \includegraphics[width=\linewidth]{SystemImage.png}
350 \end{center}
351 \end{wrapfigure}
352 An image of our system.
353 \end{tocentry}
354
355 \end{document}
356
357 % basal: slope=11.02808, error in slope = 0.4489844
358 %prismatic: slope = 19.95948, error in slope = 0.5370894