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1  
2  
3 < \chapter{\label{chapt:intro}Introduction and Theoretical Background}
3 > \chapter{\label{chapt:intro}INTRODUCTION AND THEORETICAL BACKGROUND}
4  
5  
6   The techniques used in the course of this research fall under the two
7   main classes of molecular simulation: Molecular Dynamics and Monte
8 < Carlo. Molecular Dynamic simulations integrate the equations of motion
9 < for a given system of particles, allowing the researcher to gain
10 < insight into the time dependent evolution of a system. Diffusion
8 > Carlo. Molecular Dynamics simulations integrate the equations of
9 > motion for a given system of particles, allowing the researcher to
10 > gain insight into the time dependent evolution of a system. Diffusion
11   phenomena are readily studied with this simulation technique, making
12   Molecular Dynamics the main simulation technique used in this
13   research. Other aspects of the research fall under the Monte Carlo
14   class of simulations. In Monte Carlo, the configuration space
15 < available to the collection of particles is sampled stochastically,
16 < or randomly. Each configuration is chosen with a given probability
17 < based on the Maxwell Boltzmann distribution. These types of simulations
18 < are best used to probe properties of a system that are only dependent
19 < only on the state of the system. Structural information about a system
20 < is most readily obtained through these types of methods.
15 > available to the collection of particles is sampled stochastically, or
16 > randomly. Each configuration is chosen with a given probability based
17 > on the Maxwell Boltzmann distribution. These types of simulations are
18 > best used to probe properties of a system that are dependent only on
19 > the state of the system. Structural information about a system is most
20 > readily obtained through these types of methods.
21  
22   Although the two techniques employed seem dissimilar, they are both
23   linked by the overarching principles of Statistical
24 < Thermodynamics. Statistical Thermodynamics governs the behavior of
24 > Mechanics. Statistical Meachanics governs the behavior of
25   both classes of simulations and dictates what each method can and
26   cannot do. When investigating a system, one most first analyze what
27   thermodynamic properties of the system are being probed, then chose
# Line 31 | Line 31 | Statistical Mechanics concepts present in this dissert
31  
32   The following section serves as a brief introduction to some of the
33   Statistical Mechanics concepts present in this dissertation.  What
34 < follows is a brief derivation of Boltzmann weighted statistics, and an
34 > follows is a brief derivation of Boltzmann weighted statistics and an
35   explanation of how one can use the information to calculate an
36   observable for a system.  This section then concludes with a brief
37   discussion of the ergodic hypothesis and its relevance to this
# Line 39 | Line 39 | research.
39  
40   \subsection{\label{introSec:boltzman}Boltzmann weighted statistics}
41  
42 < Consider a system, $\gamma$, with some total energy,, $E_{\gamma}$.
43 < Let $\Omega(E_{\gamma})$ represent the number of degenerate ways
44 < $\boldsymbol{\Gamma}$, the collection of positions and conjugate
45 < momenta of system $\gamma$, can be configured to give
46 < $E_{\gamma}$. Further, if $\gamma$ is in contact with a bath system
47 < where energy is exchanged between the two systems, $\Omega(E)$, where
48 < $E$ is the total energy of both systems, can be represented as
42 > Consider a system, $\gamma$, with total energy $E_{\gamma}$.  Let
43 > $\Omega(E_{\gamma})$ represent the number of degenerate ways
44 > $\boldsymbol{\Gamma}\{r_1,r_2,\ldots r_n,p_1,p_2,\ldots p_n\}$, the
45 > collection of positions and conjugate momenta of system $\gamma$, can
46 > be configured to give $E_{\gamma}$. Further, if $\gamma$ is a subset
47 > of a larger system, $\boldsymbol{\Lambda}\{E_1,E_2,\ldots
48 > E_{\gamma},\ldots E_n\}$, the total degeneracy of the system can be
49 > expressed as,
50 > \begin{equation}
51 > \Omega(\boldsymbol{\Lambda}) = \Omega(E_1) \times \Omega(E_2) \times \ldots
52 >        \Omega(E_{\gamma}) \times \ldots \Omega(E_n)
53 > \label{introEq:SM0.1}
54 > \end{equation}
55 > This multiplicative combination of degeneracies is illustrated in
56 > Fig.~\ref{introFig:degenProd}.
57 >
58 > \begin{figure}
59 > \centering
60 > \includegraphics[width=\linewidth]{omegaFig.eps}
61 > \caption[An explanation of the combination of degeneracies]{Systems A and B both have three energy levels and two indistinguishable particles. When the total energy is 2, there are two ways for each system to disperse the energy. However, for system C, the superset of A and B, the total degeneracy is the product of the degeneracy of each system. In this case $\Omega(\text{C})$ is 4.}
62 > \label{introFig:degenProd}
63 > \end{figure}
64 >
65 > Next, consider the specific case of $\gamma$ in contact with a
66 > bath. Exchange of energy is allowed between the bath and the system,
67 > subject to the constraint that the total energy
68 > ($E_{\text{bath}}+E_{\gamma}$) remain constant. $\Omega(E)$, where $E$
69 > is the total energy of both systems, can be represented as
70   \begin{equation}
71   \Omega(E) = \Omega(E_{\gamma}) \times \Omega(E - E_{\gamma})
72   \label{introEq:SM1}
# Line 285 | Line 306 | sampled from the distribution $\rho_{kT}(\mathbf{r}^N)
306   \end{equation}
307   The difficulty is selecting points $\mathbf{r}^N$ such that they are
308   sampled from the distribution $\rho_{kT}(\mathbf{r}^N)$.  A solution
309 < was proposed by Metropolis et al.\cite{metropolis:1953} which involved
309 > was proposed by Metropolis \emph{et al}.\cite{metropolis:1953} which involved
310   the use of a Markov chain whose limiting distribution was
311   $\rho_{kT}(\mathbf{r}^N)$.
312  
# Line 481 | Line 502 | itself enter on the opposite side (see Fig.~\ref{intro
502   simulation box on an infinite lattice in Cartesian space.  Any given
503   particle leaving the simulation box on one side will have an image of
504   itself enter on the opposite side (see Fig.~\ref{introFig:pbc}).  In
505 < addition, this sets that any given particle pair has an image, real or
506 < periodic, within $fix$ of each other.  A discussion of the method used
507 < to calculate the periodic image can be found in
505 > addition, this sets that any two particles have an image, real or
506 > periodic, within $\text{box}/2$ of each other.  A discussion of the
507 > method used to calculate the periodic image can be found in
508   Sec.\ref{oopseSec:pbc}.
509  
510   \begin{figure}
# Line 557 | Line 578 | q(t-\Delta t)= q(t) - v(t)\Delta t + \frac{F(t)}{2m}\D
578          \mathcal{O}(\Delta t^4)
579   \label{introEq:verletBack}
580   \end{equation}
581 < Adding together Eq.~\ref{introEq:verletForward} and
581 > Where $m$ is the mass of the particle, $q(t)$ is the position at time
582 > $t$, $v(t)$ the velocity, and $F(t)$ the force acting on the
583 > particle. Adding together Eq.~\ref{introEq:verletForward} and
584   Eq.~\ref{introEq:verletBack} results in,
585   \begin{equation}
586 < eq here
586 > q(t+\Delta t)+q(t-\Delta t) =
587 >        2q(t) + \frac{F(t)}{m}\Delta t^2 + \mathcal{O}(\Delta t^4)
588   \label{introEq:verletSum}
589   \end{equation}
590   Or equivalently,
591   \begin{equation}
592 < eq here
592 > q(t+\Delta t) \approx
593 >        2q(t) - q(t-\Delta t) + \frac{F(t)}{m}\Delta t^2
594   \label{introEq:verletFinal}
595   \end{equation}
596   Which contains an error in the estimate of the new positions on the
# Line 573 | Line 598 | with a velocity reformulation of the Verlet method.\ci
598  
599   In practice, however, the simulations in this research were integrated
600   with a velocity reformulation of the Verlet method.\cite{allen87:csl}
601 < \begin{equation}
602 < eq here
603 < \label{introEq:MDvelVerletPos}
604 < \end{equation}
605 < \begin{equation}
581 < eq here
601 > \begin{align}
602 > q(t+\Delta t) &= q(t) + v(t)\Delta t + \frac{F(t)}{2m}\Delta t^2 %
603 > \label{introEq:MDvelVerletPos} \\%
604 > %
605 > v(t+\Delta t) &= v(t) + \frac{\Delta t}{2m}[F(t) + F(t+\Delta t)] %
606   \label{introEq:MDvelVerletVel}
607 < \end{equation}
607 > \end{align}
608   The original Verlet algorithm can be regained by substituting the
609   velocity back into Eq.~\ref{introEq:MDvelVerletPos}.  The Verlet
610   formulations are chosen in this research because the algorithms have
# Line 602 | Line 626 | ensemble average of the observable being measured.  Fr
626   reversible.  The fact that it shadows the true Hamiltonian in phase
627   space is acceptable in actual simulations as one is interested in the
628   ensemble average of the observable being measured.  From the ergodic
629 < hypothesis (Sec.~\ref{introSec:StatThermo}), it is known that the time
629 > hypothesis (Sec.~\ref{introSec:statThermo}), it is known that the time
630   average will match the ensemble average, therefore two similar
631   trajectories in phase space should give matching statistical averages.
632  
633   \subsection{\label{introSec:MDfurther}Further Considerations}
634 +
635   In the simulations presented in this research, a few additional
636   parameters are needed to describe the motions.  The simulations
637 < involving water and phospholipids in Ch.~\ref{chaptLipids} are
637 > involving water and phospholipids in Ch.~\ref{chapt:lipid} are
638   required to integrate the equations of motions for dipoles on atoms.
639   This involves an additional three parameters be specified for each
640   dipole atom: $\phi$, $\theta$, and $\psi$.  These three angles are
641   taken to be the Euler angles, where $\phi$ is a rotation about the
642   $z$-axis, and $\theta$ is a rotation about the new $x$-axis, and
643   $\psi$ is a final rotation about the new $z$-axis (see
644 < Fig.~\ref{introFig:euleerAngles}).  This sequence of rotations can be
645 < accumulated into a single $3 \times 3$ matrix $\mathbf{A}$
644 > Fig.~\ref{introFig:eulerAngles}).  This sequence of rotations can be
645 > accumulated into a single $3 \times 3$ matrix, $\mathbf{A}$,
646   defined as follows:
647   \begin{equation}
648 < eq here
648 > \mathbf{A} =
649 > \begin{bmatrix}
650 >        \cos\phi\cos\psi-\sin\phi\cos\theta\sin\psi &%
651 >        \sin\phi\cos\psi+\cos\phi\cos\theta\sin\psi &%
652 >        \sin\theta\sin\psi \\%
653 >        %
654 >        -\cos\phi\sin\psi-\sin\phi\cos\theta\cos\psi &%
655 >        -\sin\phi\sin\psi+\cos\phi\cos\theta\cos\psi &%
656 >        \sin\theta\cos\psi \\%
657 >        %
658 >        \sin\phi\sin\theta &%
659 >        -\cos\phi\sin\theta &%
660 >        \cos\theta
661 > \end{bmatrix}
662   \label{introEq:EulerRotMat}
663   \end{equation}
664  
665 < The equations of motion for Euler angles can be written down as
666 < \cite{allen87:csl}
667 < \begin{equation}
668 < eq here
669 < \label{introEq:MDeuleeerPsi}
670 < \end{equation}
665 > \begin{figure}
666 > \centering
667 > \includegraphics[width=\linewidth]{eulerRotFig.eps}
668 > \caption[Euler rotation of Cartesian coordinates]{The rotation scheme for Euler angles. First is a rotation of $\phi$ about the $z$ axis (blue rotation). Next is a rotation of $\theta$ about the new $x$ axis (green rotation). Lastly is a final rotation of $\psi$ about the new $z$ axis (red rotation).}
669 > \label{introFig:eulerAngles}
670 > \end{figure}
671 >
672 > The equations of motion for Euler angles can be written down
673 > as\cite{allen87:csl}
674 > \begin{align}
675 > \dot{\phi} &= -\omega^s_x \frac{\sin\phi\cos\theta}{\sin\theta} +
676 >        \omega^s_y \frac{\cos\phi\cos\theta}{\sin\theta} +
677 >        \omega^s_z
678 > \label{introEq:MDeulerPhi} \\%
679 > %
680 > \dot{\theta} &= \omega^s_x \cos\phi + \omega^s_y \sin\phi
681 > \label{introEq:MDeulerTheta} \\%
682 > %
683 > \dot{\psi} &= \omega^s_x \frac{\sin\phi}{\sin\theta} -
684 >        \omega^s_y \frac{\cos\phi}{\sin\theta}
685 > \label{introEq:MDeulerPsi}
686 > \end{align}
687   Where $\omega^s_i$ is the angular velocity in the lab space frame
688   along Cartesian coordinate $i$.  However, a difficulty arises when
689   attempting to integrate Eq.~\ref{introEq:MDeulerPhi} and
690   Eq.~\ref{introEq:MDeulerPsi}. The $\frac{1}{\sin \theta}$ present in
691   both equations means there is a non-physical instability present when
692 < $\theta$ is 0 or $\pi$.
693 <
694 < To correct for this, the simulations integrate the rotation matrix,
695 < $\mathbf{A}$, directly, thus avoiding the instability.
642 < This method was proposed by Dullwebber
643 < \emph{et. al.}\cite{Dullwebber:1997}, and is presented in
692 > $\theta$ is 0 or $\pi$. To correct for this, the simulations integrate
693 > the rotation matrix, $\mathbf{A}$, directly, thus avoiding the
694 > instability.  This method was proposed by Dullweber
695 > \emph{et. al.}\cite{Dullweber1997}, and is presented in
696   Sec.~\ref{introSec:MDsymplecticRot}.
697  
698 < \subsubsection{\label{introSec:MDliouville}Liouville Propagator}
698 > \subsection{\label{introSec:MDliouville}Liouville Propagator}
699  
700   Before discussing the integration of the rotation matrix, it is
701   necessary to understand the construction of a ``good'' integration
702   scheme.  It has been previously
703 < discussed(Sec.~\ref{introSec:MDintegrate}) how it is desirable for an
703 > discussed(Sec.~\ref{introSec:mdIntegrate}) how it is desirable for an
704   integrator to be symplectic, or time reversible.  The following is an
705   outline of the Trotter factorization of the Liouville Propagator as a
706 < scheme for generating symplectic integrators. \cite{Tuckerman:1992}
706 > scheme for generating symplectic integrators.\cite{Tuckerman92}
707  
708   For a system with $f$ degrees of freedom the Liouville operator can be
709   defined as,
710   \begin{equation}
711 < eq here
711 > iL=\sum^f_{j=1} \biggl [\dot{q}_j\frac{\partial}{\partial q_j} +
712 >        F_j\frac{\partial}{\partial p_j} \biggr ]
713   \label{introEq:LiouvilleOperator}
714   \end{equation}
715 < Here, $r_j$ and $p_j$ are the position and conjugate momenta of a
716 < degree of freedom, and $f_j$ is the force on that degree of freedom.
715 > Here, $q_j$ and $p_j$ are the position and conjugate momenta of a
716 > degree of freedom, and $F_j$ is the force on that degree of freedom.
717   $\Gamma$ is defined as the set of all positions and conjugate momenta,
718 < $\{r_j,p_j\}$, and the propagator, $U(t)$, is defined
718 > $\{q_j,p_j\}$, and the propagator, $U(t)$, is defined
719   \begin {equation}
720 < eq here
720 > U(t) = e^{iLt}
721   \label{introEq:Lpropagator}
722   \end{equation}
723   This allows the specification of $\Gamma$ at any time $t$ as
724   \begin{equation}
725 < eq here
725 > \Gamma(t) = U(t)\Gamma(0)
726   \label{introEq:Lp2}
727   \end{equation}
728   It is important to note, $U(t)$ is a unitary operator meaning
# Line 680 | Line 733 | Trotter theorem to yield
733  
734   Decomposing $L$ into two parts, $iL_1$ and $iL_2$, one can use the
735   Trotter theorem to yield
736 < \begin{equation}
737 < eq here
738 < \label{introEq:Lp4}
739 < \end{equation}
740 < Where $\Delta t = \frac{t}{P}$.
736 > \begin{align}
737 > e^{iLt} &= e^{i(L_1 + L_2)t} \notag \\%
738 > %
739 >        &= \biggl [ e^{i(L_1 +L_2)\frac{t}{P}} \biggr]^P \notag \\%
740 > %
741 >        &= \biggl [ e^{iL_1\frac{\Delta t}{2}}\, e^{iL_2\Delta t}\,
742 >        e^{iL_1\frac{\Delta t}{2}} \biggr ]^P +
743 >        \mathcal{O}\biggl (\frac{t^3}{P^2} \biggr ) \label{introEq:Lp4}
744 > \end{align}
745 > Where $\Delta t = t/P$.
746   With this, a discrete time operator $G(\Delta t)$ can be defined:
747 < \begin{equation}
748 < eq here
747 > \begin{align}
748 > G(\Delta t) &= e^{iL_1\frac{\Delta t}{2}}\, e^{iL_2\Delta t}\,
749 >        e^{iL_1\frac{\Delta t}{2}} \notag \\%
750 > %
751 >        &= U_1 \biggl ( \frac{\Delta t}{2} \biggr )\, U_2 ( \Delta t )\,
752 >        U_1 \biggl ( \frac{\Delta t}{2} \biggr )
753   \label{introEq:Lp5}
754 < \end{equation}
755 < Because $U_1(t)$ and $U_2(t)$ are unitary, $G|\Delta t)$ is also
754 > \end{align}
755 > Because $U_1(t)$ and $U_2(t)$ are unitary, $G(\Delta t)$ is also
756   unitary.  Meaning an integrator based on this factorization will be
757   reversible in time.
758  
759   As an example, consider the following decomposition of $L$:
760 + \begin{align}
761 + iL_1 &= \dot{q}\frac{\partial}{\partial q}%
762 + \label{introEq:Lp6a} \\%
763 + %
764 + iL_2 &= F(q)\frac{\partial}{\partial p}%
765 + \label{introEq:Lp6b}
766 + \end{align}
767 + This leads to propagator $G( \Delta t )$ as,
768   \begin{equation}
769 < eq here
770 < \label{introEq:Lp6}
769 > G(\Delta t) =  e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}} \,
770 >        e^{\Delta t\,\dot{q}\frac{\partial}{\partial q}} \,
771 >        e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}}
772 > \label{introEq:Lp7}
773   \end{equation}
774 < Operating $G(\Delta t)$ on $\Gamma)0)$, and utilizing the operator property
774 > Operating $G(\Delta t)$ on $\Gamma(0)$, and utilizing the operator property
775   \begin{equation}
776 < eq here
776 > e^{c\frac{\partial}{\partial x}}\, f(x) = f(x+c)
777   \label{introEq:Lp8}
778   \end{equation}
779 < Where $c$ is independent of $q$.  One obtains the following:  
780 < \begin{equation}
781 < eq here
782 < \label{introEq:Lp8}
783 < \end{equation}
779 > Where $c$ is independent of $x$.  One obtains the following:  
780 > \begin{align}
781 > \dot{q}\biggl (\frac{\Delta t}{2}\biggr ) &=
782 >        \dot{q}(0) + \frac{\Delta t}{2m}\, F[q(0)] \label{introEq:Lp9a}\\%
783 > %
784 > q(\Delta t) &= q(0) + \Delta t\, \dot{q}\biggl (\frac{\Delta t}{2}\biggr )%
785 >        \label{introEq:Lp9b}\\%
786 > %
787 > \dot{q}(\Delta t) &= \dot{q}\biggl (\frac{\Delta t}{2}\biggr ) +
788 >        \frac{\Delta t}{2m}\, F[q(0)] \label{introEq:Lp9c}
789 > \end{align}
790   Or written another way,
791 < \begin{equation}
792 < eq here
793 < \label{intorEq:Lp9}
794 < \end{equation}
791 > \begin{align}
792 > q(t+\Delta t) &= q(0) + \dot{q}(0)\Delta t +
793 >        \frac{F[q(0)]}{m}\frac{\Delta t^2}{2} %
794 > \label{introEq:Lp10a} \\%
795 > %
796 > \dot{q}(\Delta t) &= \dot{q}(0) + \frac{\Delta t}{2m}
797 >        \biggl [F[q(0)] + F[q(\Delta t)] \biggr] %
798 > \label{introEq:Lp10b}
799 > \end{align}
800   This is the velocity Verlet formulation presented in
801 < Sec.~\ref{introSec:MDintegrate}.  Because this integration scheme is
801 > Sec.~\ref{introSec:mdIntegrate}.  Because this integration scheme is
802   comprised of unitary propagators, it is symplectic, and therefore area
803   preserving in phase space.  From the preceding factorization, one can
804   see that the integration of the equations of motion would follow:
# Line 729 | Line 812 | see that the integration of the equations of motion wo
812   \item Repeat from step 1 with the new position, velocities, and forces assuming the roles of the initial values.
813   \end{enumerate}
814  
815 < \subsubsection{\label{introSec:MDsymplecticRot} Symplectic Propagation of the Rotation Matrix}
815 > \subsection{\label{introSec:MDsymplecticRot} Symplectic Propagation of the Rotation Matrix}
816  
817   Based on the factorization from the previous section,
818 < Dullweber\emph{et al.}\cite{Dullweber:1997}~ proposed a scheme for the
818 > Dullweber\emph{et al}.\cite{Dullweber1997}~ proposed a scheme for the
819   symplectic propagation of the rotation matrix, $\mathbf{A}$, as an
820   alternative method for the integration of orientational degrees of
821   freedom. The method starts with a straightforward splitting of the
822   Liouville operator:
823 < \begin{equation}
824 < eq here
825 < \label{introEq:SR1}
826 < \end{equation}
827 < Where $\boldsymbol{\tau}(\mathbf{A})$ are the torques of the system
828 < due to the configuration, and $\boldsymbol{/pi}$ are the conjugate
823 > \begin{align}
824 > iL_{\text{pos}} &= \dot{q}\frac{\partial}{\partial q} +
825 >        \mathbf{\dot{A}}\frac{\partial}{\partial \mathbf{A}}
826 > \label{introEq:SR1a} \\%
827 > %
828 > iL_F &= F(q)\frac{\partial}{\partial p}
829 > \label{introEq:SR1b} \\%
830 > iL_{\tau} &= \tau(\mathbf{A})\frac{\partial}{\partial \pi}
831 > \label{introEq:SR1b} \\%
832 > \end{align}
833 > Where $\tau(\mathbf{A})$ is the torque of the system
834 > due to the configuration, and $\pi$ is the conjugate
835   angular momenta of the system. The propagator, $G(\Delta t)$, becomes
836   \begin{equation}
837 < eq here
837 > G(\Delta t) = e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}} \,
838 >        e^{\frac{\Delta t}{2} \tau(\mathbf{A})\frac{\partial}{\partial \pi}} \,
839 >        e^{\Delta t\,iL_{\text{pos}}} \,
840 >        e^{\frac{\Delta t}{2} \tau(\mathbf{A})\frac{\partial}{\partial \pi}} \,
841 >        e^{\frac{\Delta t}{2} F(q)\frac{\partial}{\partial p}}
842   \label{introEq:SR2}
843   \end{equation}
844   Propagation of the linear and angular momenta follows as in the Verlet
845   scheme.  The propagation of positions also follows the Verlet scheme
846   with the addition of a further symplectic splitting of the rotation
847 < matrix propagation, $\mathcal{G}_{\text{rot}}(\Delta t)$.
847 > matrix propagation, $\mathcal{U}_{\text{rot}}(\Delta t)$, within
848 > $U_{\text{pos}}(\Delta t)$.
849   \begin{equation}
850 < eq here
850 > \mathcal{U}_{\text{rot}}(\Delta t) =
851 >        \mathcal{U}_x \biggl(\frac{\Delta t}{2}\biggr)\,
852 >        \mathcal{U}_y \biggl(\frac{\Delta t}{2}\biggr)\,
853 >        \mathcal{U}_z (\Delta t)\,
854 >        \mathcal{U}_y \biggl(\frac{\Delta t}{2}\biggr)\,
855 >        \mathcal{U}_x \biggl(\frac{\Delta t}{2}\biggr)\,
856   \label{introEq:SR3}
857   \end{equation}
858 < Where $\mathcal{G}_j$ is a unitary rotation of $\mathbf{A}$ and
859 < $\boldsymbol{\pi}$ about each axis $j$.  As all propagations are now
858 > Where $\mathcal{U}_j$ is a unitary rotation of $\mathbf{A}$ and
859 > $\pi$ about each axis $j$.  As all propagations are now
860   unitary and symplectic, the entire integration scheme is also
861   symplectic and time reversible.
862  
863   \section{\label{introSec:layout}Dissertation Layout}
864  
865 < This dissertation is divided as follows:Chapt.~\ref{chapt:RSA}
865 > This dissertation is divided as follows:Ch.~\ref{chapt:RSA}
866   presents the random sequential adsorption simulations of related
867   pthalocyanines on a gold (111) surface. Ch.~\ref{chapt:OOPSE}
868   is about the writing of the molecular dynamics simulation package
869 < {\sc oopse}, Ch.~\ref{chapt:lipid} regards the simulations of
870 < phospholipid bilayers using a mesoscale model, and lastly,
869 > {\sc oopse}. Ch.~\ref{chapt:lipid} regards the simulations of
870 > phospholipid bilayers using a mesoscale model. And lastly,
871   Ch.~\ref{chapt:conclusion} concludes this dissertation with a
872   summary of all results. The chapters are arranged in chronological
873   order, and reflect the progression of techniques I employed during my
874   research.  
875  
876 < The chapter concerning random sequential adsorption
877 < simulations is a study in applying the principles of theoretical
878 < research in order to obtain a simple model capable of explaining the
879 < results.  My advisor, Dr. Gezelter, and I were approached by a
880 < colleague, Dr. Lieberman, about possible explanations for partial
881 < coverage of a gold surface by a particular compound of hers. We
882 < suggested it might be due to the statistical packing fraction of disks
883 < on a plane, and set about to simulate this system.  As the events in
884 < our model were not dynamic in nature, a Monte Carlo method was
885 < employed.  Here, if a molecule landed on the surface without
886 < overlapping another, then its landing was accepted.  However, if there
887 < was overlap, the landing we rejected and a new random landing location
888 < was chosen.  This defined our acceptance rules and allowed us to
889 < construct a Markov chain whose limiting distribution was the surface
890 < coverage in which we were interested.
876 > The chapter concerning random sequential adsorption simulations is a
877 > study in applying Statistical Mechanics simulation techniques in order
878 > to obtain a simple model capable of explaining the results.  My
879 > advisor, Dr. Gezelter, and I were approached by a colleague,
880 > Dr. Lieberman, about possible explanations for the  partial coverage of a
881 > gold surface by a particular compound of hers. We suggested it might
882 > be due to the statistical packing fraction of disks on a plane, and
883 > set about to simulate this system.  As the events in our model were
884 > not dynamic in nature, a Monte Carlo method was employed.  Here, if a
885 > molecule landed on the surface without overlapping another, then its
886 > landing was accepted.  However, if there was overlap, the landing we
887 > rejected and a new random landing location was chosen.  This defined
888 > our acceptance rules and allowed us to construct a Markov chain whose
889 > limiting distribution was the surface coverage in which we were
890 > interested.
891  
892   The following chapter, about the simulation package {\sc oopse},
893   describes in detail the large body of scientific code that had to be
894 < written in order to study phospholipid bilayer.  Although there are
894 > written in order to study phospholipid bilayers.  Although there are
895   pre-existing molecular dynamic simulation packages available, none
896   were capable of implementing the models we were developing.{\sc oopse}
897   is a unique package capable of not only integrating the equations of
# Line 804 | Line 903 | able to parameterize a mesoscale model for phospholipi
903  
904   Bringing us to Ch.~\ref{chapt:lipid}. Using {\sc oopse}, I have been
905   able to parameterize a mesoscale model for phospholipid simulations.
906 < This model retains information about solvent ordering about the
906 > This model retains information about solvent ordering around the
907   bilayer, as well as information regarding the interaction of the
908 < phospholipid head groups' dipole with each other and the surrounding
908 > phospholipid head groups' dipoles with each other and the surrounding
909   solvent.  These simulations give us insight into the dynamic events
910   that lead to the formation of phospholipid bilayers, as well as
911   provide the foundation for future exploration of bilayer phase

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