431 |
|
without any momentum flux, $10^5$ steps of stablization with an |
432 |
|
imposed momentum transfer to create a gradient, and $10^6$ steps of |
433 |
|
data collection under RNEMD. |
434 |
+ |
|
435 |
+ |
\subsubsection*{Thermal Conductivity} |
436 |
|
|
437 |
|
Our thermal conductivity calculations show that the NIVS method agrees |
438 |
|
well with the swapping method. Four different swap intervals were |
524 |
|
(curves fit for each distribution).} |
525 |
|
\label{thermalHist} |
526 |
|
\end{figure} |
527 |
+ |
|
528 |
+ |
|
529 |
+ |
\subsubsection*{Shear Viscosity} |
530 |
+ |
Our calculations (Table \ref{shearRate}) show that velocity-scaling |
531 |
+ |
RNEMD predicted comparable shear viscosities to swap RNEMD method. All |
532 |
+ |
the scale method results were from simulations that had a scaling |
533 |
+ |
interval of 10 time steps. The average molecular momentum gradients of |
534 |
+ |
these samples are shown in Figure \ref{shear} (a) and (b). |
535 |
+ |
|
536 |
+ |
\begin{table*} |
537 |
+ |
\begin{minipage}{\linewidth} |
538 |
+ |
\begin{center} |
539 |
+ |
|
540 |
+ |
\caption{Shear viscosities of Lennard-Jones fluid at ${T^* = |
541 |
+ |
0.72}$ and ${\rho^* = 0.85}$ using swapping and NIVS methods |
542 |
+ |
at various momentum exchange rates. Uncertainties are |
543 |
+ |
indicated in parentheses. } |
544 |
+ |
|
545 |
+ |
\begin{tabular}{ccccc} |
546 |
+ |
Swapping method & & & NIVS-RNEMD & \\ |
547 |
+ |
\hline |
548 |
+ |
Swap Interval (fs) & $\eta^*_{swap}$ & & Equilvalent $j_p^*(v_x)$ & |
549 |
+ |
$\eta^*_{scale}$\\ |
550 |
+ |
\hline |
551 |
+ |
500 & 3.64(0.05) & & 0.09 & 3.76(0.09)\\ |
552 |
+ |
1000 & 3.52(0.16) & & 0.046 & 3.66(0.06)\\ |
553 |
+ |
2000 & 3.72(0.05) & & 0.024 & 3.32(0.18)\\ |
554 |
+ |
2500 & 3.42(0.06) & & 0.019 & 3.43(0.08)\\ |
555 |
+ |
\hline |
556 |
+ |
\end{tabular} |
557 |
+ |
\label{shearRate} |
558 |
+ |
\end{center} |
559 |
+ |
\end{minipage} |
560 |
+ |
\end{table*} |
561 |
+ |
|
562 |
+ |
\begin{figure} |
563 |
+ |
\includegraphics[width=\linewidth]{shear} |
564 |
+ |
\caption{Average momentum gradients in shear viscosity simulations, |
565 |
+ |
using (a) ``swapping'' method and (b) NIVS-RNEMD method |
566 |
+ |
respectively. (c) Temperature difference among x and y, z dimensions |
567 |
+ |
observed when using NIVS-RNEMD with equivalent exchange interval of |
568 |
+ |
500 fs.} |
569 |
+ |
\label{shear} |
570 |
+ |
\end{figure} |
571 |
+ |
|
572 |
+ |
However, observations of temperatures along three dimensions show that |
573 |
+ |
inhomogeneity occurs in scaling RNEMD simulations, particularly in the |
574 |
+ |
two slabs which were scaled. Figure \ref{shear} (c) indicate that with |
575 |
+ |
relatively large imposed momentum flux, the temperature difference among $x$ |
576 |
+ |
and the other two dimensions was significant. This would result from the |
577 |
+ |
algorithm of scaling method. From Eq. \ref{eq:fluxPlane}, after |
578 |
+ |
momentum gradient is set up, $P_c^x$ would be roughly stable |
579 |
+ |
($<0$). Consequently, scaling factor $x$ would most probably larger |
580 |
+ |
than 1. Therefore, the kinetic energy in $x$-dimension $K_c^x$ would |
581 |
+ |
keep increase after most scaling steps. And if there is not enough time |
582 |
+ |
for the kinetic energy to exchange among different dimensions and |
583 |
+ |
different slabs, the system would finally build up temperature |
584 |
+ |
(kinetic energy) difference among the three dimensions. Also, between |
585 |
+ |
$y$ and $z$ dimensions in the scaled slabs, temperatures of $z$-axis |
586 |
+ |
are closer to neighbor slabs. This is due to momentum transfer along |
587 |
+ |
$z$ dimension between slabs. |
588 |
+ |
|
589 |
+ |
Although results between scaling and swapping methods are comparable, |
590 |
+ |
the inherent temperature inhomogeneity even in relatively low imposed |
591 |
+ |
exchange momentum flux simulations makes scaling RNEMD method less |
592 |
+ |
attractive than swapping RNEMD in shear viscosity calculation. |
593 |
+ |
|
594 |
|
|
595 |
|
\subsection{Bulk SPC/E water} |
596 |
|
|
844 |
|
\end{minipage} |
845 |
|
\end{table*} |
846 |
|
|
778 |
– |
\subsection{Shear Viscosity} |
779 |
– |
Our calculations (Table \ref{shearRate}) shows that scale RNEMD method |
780 |
– |
produced comparable shear viscosity to swap RNEMD method. In Table |
781 |
– |
\ref{shearRate}, the names of the calculated samples are devided into |
782 |
– |
two parts. The first number refers to total slabs in one simulation |
783 |
– |
box. The second number refers to the swapping interval in swap method, or |
784 |
– |
in scale method the equilvalent swapping interval that the same |
785 |
– |
momentum flux would theoretically result in swap method. All the scale |
786 |
– |
method results were from simulations that had a scaling interval of 10 |
787 |
– |
time steps. The average molecular momentum gradients of these samples |
788 |
– |
are shown in Figure \ref{shear} (a) and (b). |
847 |
|
|
790 |
– |
\begin{table*} |
791 |
– |
\begin{minipage}{\linewidth} |
792 |
– |
\begin{center} |
793 |
– |
|
794 |
– |
\caption{Calculation results for shear viscosity of Lennard-Jones |
795 |
– |
fluid at ${T^* = 0.72}$ and ${\rho^* = 0.85}$, with swap and scale |
796 |
– |
methods at various momentum exchange rates. Results in reduced |
797 |
– |
unit. Errors of calculations in parentheses. } |
798 |
– |
|
799 |
– |
\begin{tabular}{ccccc} |
800 |
– |
Swapping method & & & NIVS-RNEMD & \\ |
801 |
– |
\hline |
802 |
– |
Swap Interval (fs) & $\eta^*_{swap}$ & & Equilvalent $j_p^*(v_x)$ & |
803 |
– |
$\eta^*_{scale}$\\ |
804 |
– |
\hline |
805 |
– |
500 & 3.64(0.05) & & 0.09 & 3.76(0.09)\\ |
806 |
– |
1000 & 3.52(0.16) & & 0.046 & 3.66(0.06)\\ |
807 |
– |
2000 & 3.72(0.05) & & 0.024 & 3.32(0.18)\\ |
808 |
– |
2500 & 3.42(0.06) & & 0.019 & 3.43(0.08)\\ |
809 |
– |
\hline |
810 |
– |
\end{tabular} |
811 |
– |
\label{shearRate} |
812 |
– |
\end{center} |
813 |
– |
\end{minipage} |
814 |
– |
\end{table*} |
815 |
– |
|
816 |
– |
\begin{figure} |
817 |
– |
\includegraphics[width=\linewidth]{shear} |
818 |
– |
\caption{Average momentum gradients in shear viscosity simulations, |
819 |
– |
using (a) ``swapping'' method and (b) NIVS-RNEMD method |
820 |
– |
respectively. (c) Temperature difference among x and y, z dimensions |
821 |
– |
observed when using NIVS-RNEMD with equivalent exchange interval of |
822 |
– |
500 fs.} |
823 |
– |
\label{shear} |
824 |
– |
\end{figure} |
825 |
– |
|
826 |
– |
However, observations of temperatures along three dimensions show that |
827 |
– |
inhomogeneity occurs in scaling RNEMD simulations, particularly in the |
828 |
– |
two slabs which were scaled. Figure \ref{shear} (c) indicate that with |
829 |
– |
relatively large imposed momentum flux, the temperature difference among $x$ |
830 |
– |
and the other two dimensions was significant. This would result from the |
831 |
– |
algorithm of scaling method. From Eq. \ref{eq:fluxPlane}, after |
832 |
– |
momentum gradient is set up, $P_c^x$ would be roughly stable |
833 |
– |
($<0$). Consequently, scaling factor $x$ would most probably larger |
834 |
– |
than 1. Therefore, the kinetic energy in $x$-dimension $K_c^x$ would |
835 |
– |
keep increase after most scaling steps. And if there is not enough time |
836 |
– |
for the kinetic energy to exchange among different dimensions and |
837 |
– |
different slabs, the system would finally build up temperature |
838 |
– |
(kinetic energy) difference among the three dimensions. Also, between |
839 |
– |
$y$ and $z$ dimensions in the scaled slabs, temperatures of $z$-axis |
840 |
– |
are closer to neighbor slabs. This is due to momentum transfer along |
841 |
– |
$z$ dimension between slabs. |
842 |
– |
|
843 |
– |
Although results between scaling and swapping methods are comparable, |
844 |
– |
the inherent temperature inhomogeneity even in relatively low imposed |
845 |
– |
exchange momentum flux simulations makes scaling RNEMD method less |
846 |
– |
attractive than swapping RNEMD in shear viscosity calculation. |
847 |
– |
|
848 |
|
\section{Conclusions} |
849 |
|
NIVS-RNEMD simulation method is developed and tested on various |
850 |
|
systems. Simulation results demonstrate its validity in thermal |