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Modeled geometry

Some more recent software uses the tensor LEED approximation of Rous and Pen-dry which can save a substantial amount of computer time [2.268-2.270]. In tensor LEED the amplitudes (0) of all escaping electron waves (spots) are first calculated conventionally as described above for a certain reference geometry. Then the derivatives of these amplitudes 5Ag/5ri with respect to small displacements of each atom i in this reference geometry are calculated. These derivatives are the constituents of the "tensor". The wave amplitude for a modified model geometry where atom i is displaced by the vector Aq is then approximately given by ... [Pg.81]

D QuickFill uses STL-format, solid-model geometry to show geometry-specific simulation results on the solid part model. [Pg.603]

Figure 2.3 Model geometry used for the study of surface-roughness effects on rarefied gas flows in micro channels. Figure 2.3 Model geometry used for the study of surface-roughness effects on rarefied gas flows in micro channels.
Figure 2.43 Model geometry for the CFD calculations on flow in curved micro channels (above) and time evolution of two initially vertical fluid lamellae over a cross-section of the channel (below), taken from [139].The secondary flow is visualized by streamlines projected on to the cross-sectional area of the channel. The upper row shows results for fC = 150 and the lower row for K = 300. Figure 2.43 Model geometry for the CFD calculations on flow in curved micro channels (above) and time evolution of two initially vertical fluid lamellae over a cross-section of the channel (below), taken from [139].The secondary flow is visualized by streamlines projected on to the cross-sectional area of the channel. The upper row shows results for fC = 150 and the lower row for K = 300.
Figure 2.51 Two-dimensional model geometry of a micro channel with a reaction occurring at the lower channel wall. Figure 2.51 Two-dimensional model geometry of a micro channel with a reaction occurring at the lower channel wall.
To create a useful CFD simulation the model geometry needs to be defined and the proper boundary conditions applied. Defining the geometry for a CFD simulation of a packed tube implies being able to specify the exact position and, for nonspherical particles, orientation of every particle in the bed. This is not an easy task. Our experience with different types of experimental approaches has convinced us that they are all too inaccurate for use with CFD models. This leads to the conclusion that the tube packing must either be computergenerated or be highly structured so that the particle positions can be calculated analytically. [Pg.325]

File Edit Model Geometry Build Setup Display Options Help... [Pg.152]

Fig. 10.5 Model geometry of a cell stack. There are internal manifolds in the separator, and fuel and air are introduced to each cell through the manifolds. Fig. 10.5 Model geometry of a cell stack. There are internal manifolds in the separator, and fuel and air are introduced to each cell through the manifolds.
Fig. 10.6 Model geometries of a single stack cell and a single unit. A repeating unit with an-ode/electrolyte/cathode and the interconnectors is modeled. Fig. 10.6 Model geometries of a single stack cell and a single unit. A repeating unit with an-ode/electrolyte/cathode and the interconnectors is modeled.
Numerical calculations for the residual stresses in the anode-supported cells are carried out using ABAQUS. After modeling the geometry of the cell of the electro-lyte/anode bi-layer, the residual thermal stresses at room temperature are calculated. The cell model is divided into 10 by 10 meshes in the in-plane direction and 20 submeshes in the out-plane direction. In the calculation, it is assumed that both the electrolyte and anode are constrained each other below 1400°C and that the origin of the residual stresses in the cell is only due to the mismatch of TEC between the electrolyte and anode. The model geometry is 50 mm x 50 mm x 2 mm. The mechanical properties and cell size used for the stress calculation are listed in Table 10.5. [Pg.352]

Fig. 10.41 The calculated distribution of the principal stress in the Lao.8Sro.2Cro.95Nio.o5C>3 3 interconnector for the standard counter-flow case 1 in Table 10.2 (a) the stress is calculated considering both the temperature and distributions in the interconnector, (b) the stress is only the thermal stress. The model geometry with 16-channels is used, and half the model is drawn in the figure. Fig. 10.41 The calculated distribution of the principal stress in the Lao.8Sro.2Cro.95Nio.o5C>3 3 interconnector for the standard counter-flow case 1 in Table 10.2 (a) the stress is calculated considering both the temperature and distributions in the interconnector, (b) the stress is only the thermal stress. The model geometry with 16-channels is used, and half the model is drawn in the figure.
Figure 1.143 Model geometry of the curved square channel used for simulating helical flows. Only half the geometry is shown due to reflection symmetry a and R denote the channel dimension and the radius of curvature, respectively [152]. Figure 1.143 Model geometry of the curved square channel used for simulating helical flows. Only half the geometry is shown due to reflection symmetry a and R denote the channel dimension and the radius of curvature, respectively [152].
In the Moller-Plesset perturbation method, the correlated system is considered to be a perturbation of the Hartree-Fock system. Consequently, each correlated configuration may be expressed as a linear combination of HF configurations. The acronyms MP2, MP3, MP4, etc. indicate Moiler-Plesset methods truncated at the second, third or fourth order of perturbation. Only the MP2 method is of common use. In higher order MP models, geometry must be optimized numerically. [Pg.257]

Fig. 58. Calculated plot of the double layer potential as a function of position and time for a low value of the double layer capacitance. Model geometry ring-shaped WE and CE, symmetric RE close to the CE (weak negative global coupling). (Reproduced form A. Birzu, B. J. Green, N. I. Jaeger, J. L. Hudson, J. Electroanal. Chem. 504 (2001) 126, with permission of Elsevier Science.)... Fig. 58. Calculated plot of the double layer potential as a function of position and time for a low value of the double layer capacitance. Model geometry ring-shaped WE and CE, symmetric RE close to the CE (weak negative global coupling). (Reproduced form A. Birzu, B. J. Green, N. I. Jaeger, J. L. Hudson, J. Electroanal. Chem. 504 (2001) 126, with permission of Elsevier Science.)...
Kodym, R., Bergmann M.E.H. and Bouzek, K. (2005) First results of modelling geometry factors in electrolysis cells for direct drinking water disinfection. Proceedings 56th Annual Meeting of the International Society of Electrochemistry, September 26-30, Busan/Korea, p. 896. [Pg.201]

Figure 8.2 Cylindrical geometry of the Krogh-Erlang model of blood-tissue exchange. The upper panel, from Middleman [141], illustrates the assumed parallel arrangement of capillaries with each vessel independently supplying a surrounding cylinder of tissue. A diagram of the model geometry is provided in the lower panel. Figure in upper panel is reprinted with the permission of John Wiley Sons, Inc. Figure 8.2 Cylindrical geometry of the Krogh-Erlang model of blood-tissue exchange. The upper panel, from Middleman [141], illustrates the assumed parallel arrangement of capillaries with each vessel independently supplying a surrounding cylinder of tissue. A diagram of the model geometry is provided in the lower panel. Figure in upper panel is reprinted with the permission of John Wiley Sons, Inc.

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