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Fluid field

The small-spiral-large-sbaft type (Fig. ll-60b) is inserted in a solids-product line as pipe banks are in a fluid line, solely as a heat-transfer device. It features a thin burden ring carried at a high rotative speed and subjected to two-sided conductance to yield an estimated heat-transfer coefficient of 285 W/(m °C) [50 Btu/(h fU °F)], thereby ranking thermally next to the sheU-fluidizer type. This device for powdered solids is comparable with the Votator ol the fluid field. [Pg.1094]

Most studies on heat- and mass-transfer to or from bubbles in continuous media have primarily been limited to the transfer mechanism for a single moving bubble. Transfer to or from swarms of bubbles moving in an arbitrary fluid field is complex and has only been analyzed theoretically for certain simple cases. To achieve a useful analysis, the assumption is commonly made that the bubbles are of uniform size. This permits calculation of the total interfacial area of the dispersion, the contact time of the bubble, and the transfer coefficient based on the average size. However, it is well known that the bubble-size distribution is not uniform, and the assumption of uniformity may lead to error. Of particular importance is the effect of the coalescence and breakup of bubbles and the effect of these phenomena on the bubble-size distribution. In addition, the interaction between adjacent bubbles in the dispersion should be taken into account in the estimation of the transfer rates... [Pg.361]

Bourne, J. R., F. Brogli, F. Hoch, and W. Regenass, "Heat Transfer from Exothermically Reacting Fluids in Vertical Unstirred Vessels—I. Temperature and Fluid Fields," Chem. Eng. Sci., 42,2183 (1987). [Pg.192]

Figure 5.2 schematically exhibits the structure and reactant flow of a simplified sfack designed by Bac 2 Conductive Composifes Inc. [5] that contains three unit cells. Some components, such as GDLs, are not shown in the simplified diagram. Each unif cell includes an MEA and a plafe (the anode plate, cathode plate, and coolant plate are not differentiated). Gas flow charmels or fluid fields are on fhe surface of each plafe. [Pg.309]

The plate at the two ends of a cell row or stack is called the end plate and has a slightly different structure from that of normal bipolar plates in the stack. The end plate actually is a "single-polar" plate with only the fluid field on the inside surface contacting the anode or the cathode of the unit cell at either end of the stack. The outside surface of the end plate is flat with fluid ports as shown in Figure 5.2. The end plate normally contacts the other cell row or system as electrical and fluid input/output connections. Because the end plate is normally made of the same material through similar processing to that of the bipolar plate in a stack, the bipolar plate and end plate will be called a plate hereafter in this chapter unless their differences are addressed. [Pg.310]

For example, due to the inevitable friction and impact of the channel surface to fluid flows, particularly at the bending part of the flow channels, how to reduce fluid flow rate changes or fluid pressure drop from inlet to outlet has to be considered in the fluid field design. One key part of the flow field... [Pg.310]

For example, the required lower bulk electrical resistance and surface contact resistance are directly related to reducing internal power consumption in fuel cells to achieve maximum power output. The requirements of high flexural strength and flexibility (ultimate strain) are important to assure no distortion of fluid fields and no crack in a plate sustained in the large compressive loading when each unit cell is assembled together as a stack. This is particularly important when the thickness of the plate becomes thinner and thinner (can be close to or less than 1 mm [9]) and the dimension of the fluid field becomes smaller and smaller. Whether it is elastic or plastic, the large... [Pg.312]

One typical example of carbon/carbon composite plates is that made by Oak Ridge National Laboratory (ORNL) in the United States [12]. The composite preform was fabricafed by a slurry-molding process from fhe mixed slurry befween short carbon fibers (graphite fibers were also added in some sample plates) and fhe phenolic resin. The mass rafio between fiber reinforcement and phenolic matrix is 4 3. The phenolic matrix improves the mechanical properties and dimensional stability of the plate. A subsequent vacuum molding process was utilized to fabricate composite plates and fluid fields with relatively high resolution (Figure 5.3, [11]). [Pg.317]

Bubbles and drops tend to deform when subject to external fluid fields until normal and shear stresses balance at the fluid-fluid interface. When compared with the infinite number of shapes possible for solid particles, fluid particles at steady state are severely limited in the number of possibilities since such features as sharp corners or protuberances are precluded by the interfacial force balance. [Pg.22]

A study of the "continuity" of the model when changing from the solid-fluid to the liquid-fluid field for a fixed mixture application and "adjustment" of the group-contribution method. It is this third stage and its results that we present below. [Pg.470]

Prior to the solution of this problem, the fluid fields U(x,z) and V(x,z) should be determined. The numerical investigation of the heat exchange problem was done by the finite-difference method. Its results depend on how the obstruction temperature t(x, z) is parametrized. [Pg.118]

The fluid field U(x,z), V(x,z) is assumed to be known from the fluid mechanical problem (3.85)-(3.87), but six new dimensionless criteria have been appeared... [Pg.134]

Statement of the problem. In the theory of heat exchange between liquid metals (Pr C 1), the fluid field is usually considered on the basis of the ideal fluid model [48], since the hydrodynamic boundary layer lies deep inside the thermal boundary layer. In this case, generally speaking, the Peclet number need not be sufficiently large for the thermal boundary layer approximation to be applicable. [Pg.193]

Traditional methods of simulation in hydrodynamics are based on the description of a fluid field obeying to partial differential equations. Finite difference, finite elements, spectral methods are generally used to approximate the equations and they are represented in the computer by floating point numbers. The implementation of the boundary conditions is the main difficulty of these methods. [Pg.148]

In many respects, at a superficial level, the theory for the chemical reaction problem is much simpler than for the velocity autocorrelation function. The simplifications arise because we are now dealing with a scalar transport phenomenon, and it is the diffusive modes of the solute molecules that are coupled. In the case of the velocity autocorrelation function, the coupling of the test particle motion to the collective fluid fields (e.g., the viscous mode) must be taken into account. At a deeper level, of course, the same effects must enter into the description of the reaction problem, and one is faced with the problem of the microscopic treatment of the correlated motion of a pair of molecules that may react. In the following sections, we attempt to clarify and expand on these parallels. [Pg.108]

As the effect of the fluid field on the stress field, most discussions have just taken into account the hydrostatic pressure, which adopted the effective pressure to solve the coupling problem. However, it has not considered the hydrodynamic pressure on the stress field, which would induce hauling effect. [Pg.929]

To investigate the stress on the fluid flow effect through the gap width variation, and this effect is responded by the permeability change. Numerous study has on the influence of normal stress to the fluid field, and has obtained many experienced formulas, such as. [Pg.929]

But the shear stress to the fluid field has not been so widely studied. For the rock subjected... [Pg.929]

The damping coefficient, c, caused by the drag force exerted on the resonator by the air, can only be determined if the airflow velocities are known. This requires the modeling of the fluid field surrounding the resonator. In the following section several of the flow models that have been used to compute resonator drag are discussed. [Pg.188]

Fw,ave is the surface-averaged temperature at the fluid-solid interface of area Ai t, Tf ave is the volume-averaged temperature of the fluid field, and ki is the thermal conductivity of the pure... [Pg.2165]

Fig. 5.6 Arrhenius plot for hydrothermal reaction rate. Tc is the temperature of transition to the supercritical fluid field... Fig. 5.6 Arrhenius plot for hydrothermal reaction rate. Tc is the temperature of transition to the supercritical fluid field...
In the context of particle motion it is quite common to describe the fluid field in curvilinear coordinates (e.g. spherical coordinates), which leads to a less elegant description of momentum conservation than given in Eq. (B.6) because the direction of the basis coordinates is not fixed (Landau and Lifshitz 1987, pp. 44-51). [Pg.303]


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See also in sourсe #XX -- [ Pg.216 ]




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