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Simulation, space

Fig. 2. Patches divide the simulation space into a regular grid of cubes, each larger than the nonbonded cutoff. Interactions between atoms belonging to neighboring patches are calculated by one of the patches which receives a positions message (p) and returns a force message (f). Shades of gray indicate processors to which patches are assigned. Fig. 2. Patches divide the simulation space into a regular grid of cubes, each larger than the nonbonded cutoff. Interactions between atoms belonging to neighboring patches are calculated by one of the patches which receives a positions message (p) and returns a force message (f). Shades of gray indicate processors to which patches are assigned.
Both the Coulomb cmd Lennard-Jones potentials can be considered examples of this type. In the cell multipole method the simulation space is divided into uniform cubic... [Pg.355]

The application of voting rules leads unavoidably to pattern formation, since its effect is to delete cells in a state that is poorly represented in the local environment and replace them by cells in a state that is common therefore, cells of the same state collect in neighboring regions of the simulation space. Figure 6.13 shows an example. [Pg.186]

Decomposition of Irradiated a-Lead Azide , BNL-6632, Brookhaven Natl Lab, Upton (1963) 112) J.G. Horton, Exploration of Solid Propellant Characteristics under Simulated Space Conditions , Proc 1963 Mtg Inst of Environmental Sciences (1963), 177—84 113) G. [Pg.94]

It was soon realised that at least unequal intervals, crowded closely around the UMDE edge, might help with accuracy, and Heinze was the first to use these in 1986 [300], as well as Bard and coworkers [71] in the same year. Taylor followed in 1990 [545]. Real Crank-Nicolson was used in 1996 [138], in a brute force manner, meaning that the linear system was simply solved by LU decomposition, ignoring the sparse nature of the system. More on this below. The ultimate unequal intervals technique is adaptive FEM, and this too has been tried, beginning with Nann [407] and Nann and Heinze [408,409], and followed more recently by a series of papers by Harriman et al. [287,288,289, 290,291,292,293], some of which studies concern microband electrodes and recessed UMDEs. One might think that FEM would make possible the use of very few sample points in the simulation space however, as an example, Harriman et al. [292] used up to about 2000 nodes in their work. This is similar to the number of points one needs to use with conformal mapping and multi-point approximations in finite difference methods, for similar accuracy. [Pg.211]

At each edge of the simulation space, a boundary condition must be supplied. The common ones are as follows. [Pg.94]

Bulk concentration (Dirichlet boundary) Used to represent edges of the simulation space where the solution has not been perturbed by electrolysis or incoming solution in a hydrodynamic cell. [Pg.95]

Figure 10 The mapping of regions of simulation space to nodes. The arrows show where the sub-cells are needed during the force calculation. The outer layer of sub-cells on each node cell represents the temporary space needed to hold particle position data. (Adapted from [471.)... Figure 10 The mapping of regions of simulation space to nodes. The arrows show where the sub-cells are needed during the force calculation. The outer layer of sub-cells on each node cell represents the temporary space needed to hold particle position data. (Adapted from [471.)...
Amphlett and Denuault (11) have formulated a time-dependent SECM problem based on the same ideas (i.e., the simulation space is expanded beyond the edge of the insulating sheath and diffusion from behind the shield is taken into account). The steady-state responses were calculated as a longtime limit of the tip transient currents. These authors also obtained two equations describing SECM approach curves for a pure positive and negative feedback. The equation for a diffusion-controlled positive feedback is identical to Eq. (30) (this is not surprising because both equations are based on the same approximate expression from Ref. 9). The parameters reported in Ref. 11 for RG = 10.2 and 1.51 are quite close to those obtained in Ref. 7... [Pg.156]

LI, RMAX simulation space limits m0 effective mass transfer coefficient... [Pg.197]

Effects of Simulated Space Environments on Piezoelectric Vinylidene Fluoride-Based Polymers... [Pg.153]

Fig. 3.2. Discrete simulation space-time grid showing concentration terms involved in the equation for Cf using the (a) explicit and (b) implicit methods. Grey squares show the term to be solved for and white circles show the terms that appear in the equation. Fig. 3.2. Discrete simulation space-time grid showing concentration terms involved in the equation for Cf using the (a) explicit and (b) implicit methods. Grey squares show the term to be solved for and white circles show the terms that appear in the equation.
The distribution of the points in the grid can be adjusted by means of the parameters h = ho) and cox- For example, the distribution of nodes corresponding to ujx = 1.1 and h = 0.0001 in the Cottrell experiment are shown in Figure 4.1. The expanding grid enables us to have a very dense grid (Xi — Xo = 0.0001) next to the electrode surface and, at the same time, to cover all the simulation space from X = 0 to 6VTmax with only 92 points. [Pg.76]

Note that the simulation space is now constrained to the region 1 < i < 1 + VTmax, R = 0 is the point at the centre of the electrode (its interior) so naturally the simulation space begins at i = 1 (r = rg), the electrode surface. The time is likewise normalised against the radius ... [Pg.91]

In a one-dimensional system, the simulation space is a line, so the space is bounded by two singular points the electrode surface and the bulk concentration boundary. In this two-dimensional system, the simulation space is a rectangular region of a flat plane, so four boundary lines, each with their own boundary conditions, are required. These boundary lines are r = 0, = 0, r = Tmax and. s =. s iax-... [Pg.178]

The simulation space and boundary conditions for a microband is exactly the same as that for a microdisc, as depicted in Figure 9.3, except for the change of coordinate system. [Pg.195]

Apart from this change in boundary condition, the simulation space for a microdisc array is exactly the same as that used for the single microdisc, depicted in Figure 9.3. [Pg.205]

Fig. 10.8. (a) Unit cell for the partially blocked electrode model (b) simulation space... [Pg.215]

Apart from this change in boundary condition, the simulation space for a microband array is exactly the same as for the single microband, depicted in Figure 9.8. As with the microdisc array, it is necessary to alter the spatial grid in the X-direction so that there is a high concentration of spatial points at this outer boundary to ensure accurate simulation. [Pg.217]

It is possible to develop a simulation model for the IDA system by recognising that like some other systems under study in this chapter, it has translational symmetry. The simulation space for the IDA is a unit cell that encompasses half of each of two neighbouring bands and the space in between them, as shown in Figure 10.13. Note that here for simplicity, we assume that both kinds of band have the same width, w, though this need not be the case. [Pg.220]


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