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Coarseness coarse grids

When a coarse grid is used, wall functions are used for imposing boundary conditions near the walls (Section 11.2.3.3). The nondimensional wall distance should be 30 < y < ]Q0, where y = u,y/p. We cannot compute the friction velocity u. before doing the CFD simulation, because the friction velocity is dependent on the flow. However, we would like to have an estimation of y" to be able to locate the first grid node near the wall at 30 < y < 100. If we can estimate the maximum velocity in the boundary layer, the friction velocity can be estimated as n, — 0.04rj, . . After the computation has been carried out, we can verify that 30 nodes adjacent to the walls. [Pg.1032]

Figure 8.7 shows these results for = 1 and compares them with the analytical solution. The numerical approximation is quite good, even for a coarse grid with 7=4 and 7=16. This is the exception rather than the rule. Convergence should be tested using a hner grid size. [Pg.296]

If a coarse grid with a mesh size H H=lh, for example) is employed to evaluate the same integration (25), its discrete form can be written as... [Pg.123]

The idea of MLMI method is to calculate the integration first on the coarse grid (//), and then to evaluate the on the fine grid h) through an interpolation. [Pg.123]

A method for smoothing the residual obtained on the fine grid in order to compute the corresponding residual on the coarse grid. In the terminology of the multigrid method, this step is called restriction. [Pg.168]

A method for interpolating the update to the solution obtained on the coarse grid to the fine one. The interpolation step is denoted prolongation. [Pg.168]

In one cycle of the multigrid method, first a few iterations are performed on the fine grid in order to obtain a comparatively smooth iteration error. After that the obtained residual is restricted to the coarse grid, where further iterations are performed in order to damp out the long-wave components of the solution error. Subsequently the coarse-grid solution is interpolated to the fine grid and the solution on the fine grid is updated. [Pg.168]

The first term on the right hand side of equation (7-40), the weight function derivatives, will vanish in the limit of an infinite grid. However, in practical applications we must consider that the atomic weights depend explicitly on the nuclear coordinates and therefore their derivative will not be zero. In particular if coarse grids are used, the contributions of... [Pg.125]

Fig. 21. The product D-atom velocity-flux contour map, d Fig. 21. The product D-atom velocity-flux contour map, d <j/dv d(cos0), in a 3D isometric representation. Each contour is constructed directly from a total of 28 slices of the Doppler-selected TOF measurements, as exemplified in Fig. 20. For clarity, a coarse grid size is used here. The zero degree is defined as the initial center-of-mass velocity of the HD beam from which the D-atom product is originated. Note the dominance of the HF(V = 2) co-product for all cases, yet the dramatic variations in angular distributions with a slight change in collision energy ( 0.1 kcal/moll).
First of all, the increased computer power makes it possible to switch to transient simulations and to increase spatial resolution. One no longer has to be content with steady flow simulations on relatively coarse grids comprising 104-105 nodes. Full-scale Large Eddy Simulations (LES) on fine grids of 106—107 nodes currently belong to the possibilities and deliver realistic reproductions of transient flow and transport phenomena. Comparisons with quantitative experimental data have increased the confidence in LES. The present review stresses that this does not only apply to the hydrodynamics but relates to the physical operations and chemical processes carried out in stirred vessels as well. Examples of LES-based simulations of such operations and processes are due to Flollander et al. (2001a,b, 2003), Venneker et al. (2002), Van Vliet et al. (2005, 2006), and Flartmann et al. (2006). [Pg.157]

Fig. 9.22 a) SEM micrograph of polystyrene brushes generated via SIP on a substrate that was irradiated through a stencil mask with a coarse grid with 50 pm periodicity. Each square contains an array of circular holes of 1.5 pm dots (2.5 pm periodicity), b) SPM... [Pg.412]

To meet the industrial demand for both large-scale computation and good predictability, the reasonable way out is not to simulate from the beginning of the micro-scale, but to use coarse-grid simulation with meso-scale modeling for the effects of structure. This kind of approach can be termed the "multi-scale CFD." It is entitled "multi-scale," not because the problem it solves is multi-scale, but because its meso-scale model contains multi-scale structure parameters. [Pg.12]

Limited to computing capability, the following analysis confines the DNS to the fine-grid TFM simulation, which offers meso-scale closures for the correlative, coarse-grid TFM simulations. For comparison, the variational type of multi-scale CFD takes the EMMS-based models to close TFM simulations. [Pg.16]

Figure 5 Effect of grid resolution (A.) on the time-averaged dimensionless slip velocity (us/uT). Geldart group A particles are used. The ordinate is scaled with the terminal velocity of single particles (uT 21.84 cm/s) and the abscissa is scaled with the particle diameter dp. The domain size is 1.5 x 6 cm2, comparable to the coarse-grid used in normal simulations. Figure 5 Effect of grid resolution (A.) on the time-averaged dimensionless slip velocity (us/uT). Geldart group A particles are used. The ordinate is scaled with the terminal velocity of single particles (uT 21.84 cm/s) and the abscissa is scaled with the particle diameter dp. The domain size is 1.5 x 6 cm2, comparable to the coarse-grid used in normal simulations.

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See also in sourсe #XX -- [ Pg.152 , Pg.153 , Pg.154 , Pg.155 , Pg.156 , Pg.157 , Pg.158 ]




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