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Impermeable wall

The standard k- model simulates the turbulenee in the reaetor. For flow within the porous eatalyst bed, however, we suppress the turbulenee. We enter the appropriate physieal properties of the system, and employ standard boundary eonditions at the impermeable walls and the reaetor outlet. To represent the turbulenee of the feed stream at the inlet, we treat it as pipe-flow turbulenee. These model equations ean then be solved for instanee, via the well-known Simple algorithm [3]. To faeilitate fast eonvergenee, it is useful to make a reasonable initial guess of the pressure drop aeross the eatalyst bed. [Pg.819]

The boundary condition at impermeable walls and symmetry planes at y and y = a a being the width of the combustor exit) is dp/dy = 0. [Pg.189]

Without an impermeable wall behind a biofilm, carbon-containing pollutants would be absorbed. If the pollutant load varies from time to time, the wall could serve as a reservoir for excess pollutants. When the load is smaller, diffusion out to the layer could maintain a viable colony. Also, if low molecular nutrients (micronutrients, for example) are added artificially, they can be stored in the absorptive layer and released on demand. [Pg.112]

A hemispherical polymer matrix that is coated on all surfaces with an impermeable coating except for an aperture in the center face has been demonstrated to provide near constant rate release profiles ( 18). Another approach consists of a cylinder with impermeable wall and a cavity having a circular sector cross section. [Pg.9]

Forced flow, as in water flowing in a tube or a pipe. The impermeable walls of the pipe restrict the flow to the course of the pipe (one-dimensional degree of hydraulic freedom), with only one inflow point and one outflow point (Fig. 2.11c). [Pg.32]

Stagnation (zero flow), as in water in a closed bottle. The impermeable walls of the bottle completely block the mobility of the water (zero degrees of hydraulic freedom) and it stays at rest (Fig. 2.lid). [Pg.32]

At the impermeable wall boundaries of the solution domain, normally a no slip boundary condition is employed. This is achieved by setting the transverse fluid velocity equal to that of the surface and setting the normal velocity to zero. Since the normal velocity at the wall is known, the value of pressure at the wall boundary is not required to be known. For species concentrations or temperatures, any of the following conditions can be specified at the wall boundaries ... [Pg.50]

When simulating the trajectories of dispersed phase particles, appropriate boundary conditions need to be specified. Inlet or outlet boundary conditions require no special attention. At impermeable walls, however, it is necessary to represent collisions between particles and wall. Particles can reflect from the wall via elastic or inelastic collisions. Suitable coefficients of restitution representing the fraction of momentum retained by a particle after a collision need to be specified at all the wall boundaries. In some cases, particles may stick to the wall or may remain very close to the wall after they collide with the wall. Special boundary conditions need to be developed to model these situations (see, for example, the schematic shown in Fig. 4.5). [Pg.97]

At the outlet, extrapolation of the velocity to the boundary (zero gradient at the outlet boundary) can usually be used. At impermeable walls, the normal velocity is set to zero. The wall shear stress is then included in the source terms. In the case of turbulent flows, wall functions are used near walls instead of resolving gradients near the wall (refer to the discussion in Chapter 3). Careful linearization of source terms arising due to these wall functions is necessary for efficient numerical implementation. Other boundary conditions such as symmetry, periodic or cyclic can be implemented by combining the formulations discussed in Chapter 2 with the ideas of finite volume method discussed here. More details on numerical implementation of boundary conditions may be found in Patankar (1980) and Versteeg and Malalasekara (1995). [Pg.172]

FIGURE 3-8 A flow net for a hypothetical aquifer formed in a drowned river valley, which is assumed to be of uniform thickness over its area and located between two water-impermeable walls of bedrock. The hydraulic head varies between 2 m and 4.9 m. Squares A and B and points x and y are used in Example 3-2. [Pg.210]

The steady gas flow in a long macroscopic channel with impermeable walls is basically a Poiseuille flow with the constant velocity determined by the pressure gradient. However, the velocity of the flow in the fuel cell channel varies since there is mass and momentum transfer through the channel/backing layer interface. [Pg.514]

At the impermeable wall, the no-slip condition is generally not appropriate for granular flows. Nevertheless, the granular phase velocity component normal to the wall is normally set to zero. However, the granular phase is usually allowed to slip along the wall. A velocity slip proportional to the velocity gradient at the wall is commonly applied ... [Pg.530]

Problem 8-17. Selective Withdrawal From a Porous Medium. Consider a porous medium that is bounded on one side by a vertical impermeable wall. We assume that Darcy s law applies so that... [Pg.590]

Problem 12-9. Rayleigh-Taylor Instability for a Pair of Superposed Fluids that are Bounded Above and Below by an Impermeable Wall. In this problem, we wish to determine the effect of a pair of horizontal bounding walls that exist at a finite distance above and below a horizontal fluid interface on Rayleigh Taylor instability. We suppose that the interface is located at z = 0 and that the two fluids are inviscid, with the density of the fluid below the interface p being less than the density of the fluid above the interface pi. The boundary above the interface is located at z = hi, whereas that below the interface is at z = —h. Show that... [Pg.884]

The gas in an open-cell foam is normally air, unless the entire foam is enclosed in an Impermeable wall and then filled with a particular gas for a particular purpose. [Pg.482]

The advantages of using a mass transfer system to simulate a heat transfer system include the potential for improved accuracy of measurement and control of boundary conditions. For example, electric current and mass changes can generally be measured with greater accuracy than heat flux. Also, while adiabatic walls are an ideal that, at best, we can only approach, impermeable walls are an everyday reality. Thus, mass transfer systems are gaining popularity in precision experimental studies. [Pg.1221]

Because of the transverse velocity component, the velocity profile is a modification of the usual Poiseuille distribution. This problem has been solved by Berman (1953), including the effect of a constant permeation velocity in altering the velocity profile in the x direction and in causing a streamwise variation in the bulk average velocity. However, when the Reynolds number based on the permeation velocity is small, as it generally is, the streamwise component has the same form as for an impermeable wall and the transverse component is proportional to the constant permeation velocity v -, that is,... [Pg.100]

Microcapsules with impermeable walls are used in products where isolation of active substances is needed, followed by a quick release under defined conditions. The effects achieved with impermeable microcapsules include separation of reactive components, protection of sensitive substances against environmental effects, reduced volatility of highly volatile substances, conversion of liquid ingredients into a solid state, taste and odor masking, and toxicity reduction. [Pg.1070]

Depending on the permeability of the other wall, the semi-infinite transient transfer will evolve toward a stationary transfer (permeable wall) or a thin-layer transfer (impermeable wall). [Pg.472]


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See also in sourсe #XX -- [ Pg.181 ]




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