Isomerization reaction in a Lennard-Jones solvent next up previous
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Isomerization reaction in a Lennard-Jones solvent

 

As a simple paradigm for solution phase chemical processes, we consider a simple isomerization reaction of a diatomic molecule solvated in a Lennard-Jones liquid. The intramolecular potential of the diatomic is characterized by a single coordinate tex2html_wrap_inline1657 , the distance between the two atoms comprising the diatomic. The intramolecular potential is, again, given by a quartic double well form:

  equation343

so that the total potential is given by

  equation347

In this case, the potential parameters are tex2html_wrap_inline1659 10 tex2html_wrap_inline1661 K/Å tex2html_wrap_inline1663 , a= 0.22 Å, and tex2html_wrap_inline1667 4.26 Å. With these parameters, the diatomic can exist in two stable conformations characterized by bond lengths of tex2html_wrap_inline1669 , which leads to tex2html_wrap_inline1671 = 4.48 Å and tex2html_wrap_inline1673 4.04 Å. The two conformations are separated by a 46.5 kcal/mol potential barrier at tex2html_wrap_inline1675 . The diatomic is solvated in a bath of 108 Lennard-Jones particles with tex2html_wrap_inline1677 90 K, tex2html_wrap_inline1679 3.405 Å and mass m=39.94 amu. The masses of the two atoms in the diatomic are both the same as the mass of the Lennard-Jones particles. The density and temperature of the system are tex2html_wrap_inline1683 0.844 and T= 300 K.

In this example, the reaction coordinate is r, the diatomic bond length. The AFED method requires that the equations of motion be formulated in a coordinate system in which r is an explicit coordinate and is given both a large mass and temperature. To see how this is accomplished, consider the Lagrangian of the system:

  equation353

where tex2html_wrap_inline1691 is the kinetic energy of the Lennard-Jones bath particles. First, we transform to center of mass and relative coordinates for the diatomic, tex2html_wrap_inline1693 and tex2html_wrap_inline1695 , yielding:

  equation363

where M=2m and tex2html_wrap_inline1699 are the total and reduced masses of the diatomic, respectively. Finally, we transform to spherical polar coordinates tex2html_wrap_inline1701 in the relative coordinate giving:

  eqnarray375

where the unit vector tex2html_wrap_inline1703 is the bond orientation vector. The adiabaticity condition is imposed by choosing a temperature tex2html_wrap_inline1705 associated with the radial degree of freedom only and by redefining the Lagrangian in Eq. (25) according to

  eqnarray390

where tex2html_wrap_inline1707 is a mass associated with the r degree of freedom only.

It is important to note that, although it is necessary to work with the coordinate r explicitly, it is not necessary to work directly with the angular degrees of freedom tex2html_wrap_inline1713 and tex2html_wrap_inline1715 . Rather, we work with the Cartesian components tex2html_wrap_inline1717 the vector tex2html_wrap_inline1719 directly so that the kinetic energy term involving tex2html_wrap_inline1719 becomes:

  equation407

When this is done, the equations of motion generated by Eq. (26) will be in terms of r and the three Cartesian components of tex2html_wrap_inline1719 . In order to ensure that tex2html_wrap_inline1719 remains a unit vector as the system evolves in time, it is necessary to add a simple constraint to the equations of motion that tex2html_wrap_inline1729 . Details of how the equations of motion are integrated and how the constraint is implemented are given in Appendix B.

AFED simulations were carried out using temperatures tex2html_wrap_inline1315 K and tex2html_wrap_inline1317 K. At tex2html_wrap_inline1735 , masses of tex2html_wrap_inline1737 10 tex2html_wrap_inline1739 amu and tex2html_wrap_inline1741 10 tex2html_wrap_inline1739 amu were used with a time step of tex2html_wrap_inline1745 5 fs. At tex2html_wrap_inline1747 , masses of tex2html_wrap_inline1749 amu and 35953 amu were used. AFED simulation lengths of various lengths were performed in order to test convergence. In addition, bluemoon ensemble simulations were carried out using 11 evenly spaced fixed values of r between 4.0 Å and 4.50 Å. (This was found to be the minimum number of points needed to generate an accurate free energy profile.) Each bluemoon simulation consisted of tex2html_wrap_inline1757 steps with a time step of tex2html_wrap_inline1759 fs for a total run time of 2.2 ns. Although this is somewhat longer than is actually needed to generate the free energy profile via the bluemoon ensemble method, such a long run ensures a highly converged free energy profile against which the AFED method can be benchmarked. In Fig. 4, the free energy profiles obtained from the AFED calculations for the various mass and temperature choices and that obtained from the bluemoon calculation are shown.

   figure421

Figure 4: Adiabatic Dynamics free energy profile for an isomerization reaction of a diatomic in a Lennard-Jones solvent. The figure shows the convergence as a function of the mass tex2html_wrap_inline1761 (cf. Eq. (26)) with tex2html_wrap_inline1315 K (a) and for tex2html_wrap_inline1317 K (b). In both panels, the solid line is the free energy profile obtained employing the ``bluemoon ensemble'' method [5, 6]. In all cases m=39.94 amu and the temperature and density are T=300 K and tex2html_wrap_inline1323 , respectively.

It can be seen that for tex2html_wrap_inline1735 and tex2html_wrap_inline1775 240 tex2html_wrap_inline1589 10 tex2html_wrap_inline1739 amu, the agreement between the two methods is good, and for tex2html_wrap_inline1747 and tex2html_wrap_inline1783 amu, the agreement between the two methods is also good. In the latter case, a 600 ps run yields the best agreement for tex2html_wrap_inline1785 , however, even a 200 ps run reproduces the free energy barrier to within about 5%. For tex2html_wrap_inline1787 , a 600 ps run is insufficiently long to converge the free energy profile, as can be see in Fig. 4(b), however, if the trajectory is allowed to run for 2 ns, it is found that the correct free energy profile is obtained.

In order to compare the efficiency of the AFED and bluemoon methods, the following analysis was carried out. First, note in Fig. 4, that the AFED method actually generates a larger range of r than the bluemoon method. Of course, the bluemoon method can be made to sample the same range of r by carrying out more simulations. In this case, 22 evenly spaced points would be required, hence, 22 simulation. Next, an AFED simulation using 22 bins for the histogram of P(r) was carried out, and the error bar on the force tex2html_wrap_inline1795 on r in one of the bins computed and compared to the error bar obtained from the bluemoon ensemble method for the same value of r. It was found that, in order to obtain an error bar of size 8 tex2html_wrap_inline1801 au, an AFED simulation of 880 ps was needed compared to a bluemoon calculation of 80 ps. However, since one AFED simulation generates the full free energy profile, while 22 individual bluemoon simulation are needed, the total simulation time for the bluemoon method would then be tex2html_wrap_inline1803 ns. Thus, comparing the total simulation times, shows that the AFED method is nearly twice as efficient as the bluemoon method. In practice, one might be content with a restricted range for the reaction coordinate in the bluemoon method. In the present example, the above analysis shows that, in this case, the two method are, then, of equal efficiency, however, the AFED method gives a more complete picture of the free energy profile.


next up previous
Next: Discussion Up: Model problems and results Previous: One-dimensional quartic double well

Mark Tuckerman
Mon Mar 26 04:23:46 EST 2001