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Velocity model building

Background. To appreciate the power of the model building approach presented in this chapter, we here present an application of the new approach for geometric mapping of salt domes for velocity model building. To understand why this is a difficult, but import task, we need to understand what a salt dome is, its properties, how to image it and the problems associated with that. [Pg.236]

The magnitudes of concentrations of intermediates and of step velocities appearing in these mechanisms are the parameters in kinetic models that form the next step for further discrimination. A detailed treatment of model building for this purpose is beyond the scope of this article. The subject is briefly discussed here in the context of the methods presented. [Pg.319]

In the development of Model I (plug flow), we took careful note that the assumptions used in this first model building exercise implied turbulent flow conditions, such a state being defined by the magnitude of the Reynolds number (uq d/v), which must always exceed 2100 for this model to be applicable. For slower flows, the velocity is no longer plug shaped, and in fact when Re < 2100, the shape is parabolic... [Pg.8]

A new approach towards model building with the promise of significantly shortening the turnaround time of 3D model building has been presented. By introducing a unifying framework, efficient representation of models throughout the lifecycle of a reservoir is enabled, all the way from velocity to simulation models. [Pg.240]

This section deals mainly with the interaction of thermal models as outlined in Section J 1.3 and airflow models as described in Section 11.4 for the purpose of integrated modeling of thermally induced (stack-driven) natural ventilation, governed by the thermal behavior of the building. For the integrated analysis ol air velocity fields and radiative and thermal effects in the building using CFD codes, see also Section 11.2 and Ott and Schild.-... [Pg.1095]

Adiabatic Reactors. Like isothermal reactors, adiabatic reactors with a flat velocity profile will have no radial gradients in temperature or composition. There are axial gradients, and the axial dispersion model, including its extension to temperature in Section 9.4, can account for axial mixing. As a practical matter, it is difficult to build a small adiabatic reactor. Wall temperatures must be controlled to simulate the adiabatic temperature profile in the reactor, and guard heaters may be needed at the inlet and outlet to avoid losses by radiation. Even so, it is hkely that uncertainties in the temperature profile will mask the relatively small effects of axial dispersion. [Pg.335]

Venneker et al. (2002) used as many as 20 bubble size classes in the bubble size range from 0.25 to some 20 mm. Just like GHOST , their in-house code named DA WN builds upon a liquid-only velocity field obtained with FLUENT, now with an anisotropic Reynolds Stress Model (RSM) for the turbulent momentum transport. To allow for the drastic increase in computational burden associated with using 20 population balance equations, the 3-D FLUENT flow field is averaged azimuthally into a 2-D flow field (Venneker, 1999, used a less elegant simplification )... [Pg.206]

Models to Allow for the Effects of Coastal Sites, Plume Rise, and Buildings on Dispersion of Radionuclides and Guidance on the Value of Deposition Velocity and Washout Coefficients, Fifth Report of a Working Group on Atmospheric Dispersion, National Radiological Protection Board, NRPB-R157, 1983. [Pg.255]

Figure 2.10 Cylindrically symmetric hydrodynamical model of accretion flow with rotation during the early collapse phase, showing the inflow of matter in the meridional plane and the build-up of a flat rotating disk structure after about 1.05 free-fall times. Arrows indicate matter flow direction and velocity, gray lines indicate cuts of isodensity surfaces with meridional plane. Dark crosses outline locations of supersonic to subsonic transition of inflow velocity this corresponds to the position of the accretion shock. Matter falling along the polar axis and within the equatorial plane arrive within 1600 yr almost simultaneously, which results in an almost instantaneous formation of an extended initial accretion disk [new model calculation following the methods in Tscharnuter (1987), figure kindly contributed by W. M. Tscharnuter],... Figure 2.10 Cylindrically symmetric hydrodynamical model of accretion flow with rotation during the early collapse phase, showing the inflow of matter in the meridional plane and the build-up of a flat rotating disk structure after about 1.05 free-fall times. Arrows indicate matter flow direction and velocity, gray lines indicate cuts of isodensity surfaces with meridional plane. Dark crosses outline locations of supersonic to subsonic transition of inflow velocity this corresponds to the position of the accretion shock. Matter falling along the polar axis and within the equatorial plane arrive within 1600 yr almost simultaneously, which results in an almost instantaneous formation of an extended initial accretion disk [new model calculation following the methods in Tscharnuter (1987), figure kindly contributed by W. M. Tscharnuter],...
The gaseous mixture comes into the reactor with uniform radial velocity (plug flow) and the gas velocity increases linearly with temperature inside the reactor. Indeed, we can consider the conversion as a function of r, wt and t (X (r, wx, x)) and, consequently, we can build the model taking r and x into account ... [Pg.125]

Another direction is to build models which will be more realistic. In all these models described above, the exact microscopic mechanism of the failure was not considered. But it seems very likely that the exact nature of the process will influence what happens after the first failure. Yagil et al (1992, 1993) observed that after the first failure (fuse), the resistance of the sample can get decreased or increased depending on the failure process. If increase is what one expects, then the decrease means that the first failure improves the contact between the parts which melt. Thus, only by a detailed analysis of the failure process can one understand it. To come back to the dynamic problem, it is also very likely that the velocity of the failure propagation will depend on the failure mechanism. [Pg.79]

Industrial use of hydrogen has experienced a few accidents, which subsequently have been useful in defining norms and procedures. One occurred in a narrow Stockholm street in 1983, where 13.5 kg of H2 escaped from a set of 20-MPa pressure tanks with defect cormections and exploded (Fig. 5.4a) 16 people were injured, and 10 cars and the adjacent building were heavily damaged. This accident has recently been modelled by computational fluid dynamics methods, giving the distribution of H2 velocities and concentra-... [Pg.240]

There have been recently several papers addressing the polish rate variations for several materials Mth pressure and velocity, and several different relationships have been obtained, depending upon the assumptions of pad-abrasive particle-wafer surface interaction behavior[l]. These difterent results have been obtained because there is no quantitative, detailed interaction model which has been confirmed by experiment and is predictive. The difficulty in achieving this experimental understanding is high, and there is not a good body of knowledge to build upon. [Pg.74]

The dependence on frequency is also explained by our model In order to build up a vector of polarization the ions have to migrate with a finite migration velocity. If the E-field changes too fast, the ions are not able to foOow, i.e. are not able to travel from position A to B in fig. 9. Therefore the maximal polarization can not develop and e decreases with frequency. [Pg.554]


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See also in sourсe #XX -- [ Pg.236 ]




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