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Revision 3992 by kstocke1, Wed Jan 8 22:24:46 2014 UTC vs.
Revision 3994 by kstocke1, Tue Jan 14 19:47:08 2014 UTC

# Line 88 | Line 88 | boundary between materials.
88   is often unclear what shape of gradient should be imposed at the
89   boundary between materials.
90  
91 < % \begin{figure}
92 < % \includegraphics[width=\linewidth]{figures/VSS}
93 < % \caption{Schematics of periodic (left) and non-periodic (right)
94 < %   Velocity Shearing and Scaling RNEMD. A kinetic energy or momentum
95 < %   flux is applied from region B to region A. Thermal gradients are
96 < %   depicted by a color gradient. Linear or angular velocity gradients
97 < %   are shown as arrows.}
98 < % \label{fig:VSS}
99 < % \end{figure}
91 > \begin{figure}
92 > \includegraphics[width=\linewidth]{figures/npVSS}
93 > \caption{Schematics of periodic (left) and non-periodic (right)
94 >  Velocity Shearing and Scaling RNEMD. A kinetic energy or momentum
95 >  flux is applied from region B to region A. Thermal gradients are
96 >  depicted by a color gradient. Linear or angular velocity gradients
97 >  are shown as arrows.}
98 > \label{fig:VSS}
99 > \end{figure}
100  
101   Reverse Non-Equilibrium Molecular Dynamics (RNEMD) methods impose an
102   unphysical {\it flux} between different regions or ``slabs'' of the
# Line 132 | Line 132 | concentric spheres (as in figure \ref{fig:VSS}), or on
132   We have extended the VSS method for use in {\it non-periodic}
133   simulations, in which the ``slabs'' have been generalized to two
134   separated regions of space.  These regions could be defined as
135 < concentric spheres (as in figure \ref{fig:VSS}), or one of the regions
135 > concentric spheres (as in figure \ref{fig:npVSS}), or one of the regions
136   can be defined in terms of a dynamically changing ``hull'' comprising
137   the surface atoms of the cluster.  This latter definition is identical
138   to the hull used in the Langevin Hull algorithm.
# Line 426 | Line 426 | Table \ref{table:couple} shows the calculated rotation
426   Table \ref{table:couple} shows the calculated rotational friction coefficients $\Xi^{rr}$ for spherical gold nanoparticles and a prolate ellipsoidal gold nanorod in TraPPE-UA hexane. An angular momentum flux was applied between the A and B regions defined as the gold structure and hexane molecules beyond a certain radius, respectively. The resulting angular velocity gradient causes the gold structure to rotate about the prescribed axis.
427          
428   \begin{longtable}{lcccc}
429 < \caption{Comparison of rotational friction coefficients under ideal ``stick'' conditions ($\Xi^{rr}_{stick}$) calculated via Stokes' and Perrin's laws and effective rotational friction coefficients ($\Xi^{rr}_{\mathit{eff}}$) of gold nanostructures solvated in TraPPE-UA hexane at 230 K. The ellipsoid is oriented with the long axis along the $z$ direction.}
429 > \caption{Comparison of rotational friction coefficients under ideal ``stick'' conditions ($\Xi^{rr}_{\mathit{stick}}$) calculated via Stokes' and Perrin's laws and effective rotational friction coefficients ($\Xi^{rr}_{\mathit{eff}}$) of gold nanostructures solvated in TraPPE-UA hexane at 230 K. The ellipsoid is oriented with the long axis along the $z$ direction.}
430   \\ \hline \hline
431 < {Structure} & {Axis of Rotation} & {$\Xi^{rr}_{stick}$} & {$\Xi^{rr}_{\mathit{eff}}$} & {$\Xi^{rr}_{\mathit{eff}}$ / $\Xi^{rr}_{stick}$}\\
431 > {Structure} & {Axis of Rotation} & {$\Xi^{rr}_{\mathit{stick}}$} & {$\Xi^{rr}_{\mathit{eff}}$} & {$\Xi^{rr}_{\mathit{eff}}$ / $\Xi^{rr}_{\mathit{stick}}$}\\
432   {} & {} & {\small(amu A$^2$ fs$^{-1}$)} & {\small(amu A$^2$ fs$^{-1}$)} & \\  \hline
433   Sphere (r = 20 \AA) & {$x = y = z$} & {3314} & {2386} & {0.720}\\
434   Sphere (r = 30 \AA) & {$x = y = z$} & {11749} & {8415} & {0.716}\\
# Line 439 | Line 439 | Prolate Ellipsoid & {$z$} & {1993} & {1590} & {0.798}\
439   \label{table:couple}
440   \end{longtable}
441  
442 +
443 +
444   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
445   % **DISCUSSION**
446   %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

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