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I. Stokes flow past a thin screen. II. Viscous flows past porous bodies of finite size

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In the category of porous bodies, Joseph and Tao [ll] addressed the problem of Stokes flow past a porous sphere. As a specific example, the exact solution is derived for Stokes flow past a circular annulus. A general mathematical formulation is given in Chapter II for Stokes flow past a thin screen of finite size.

GENERAL MATHEMATICAL FORMULATION FOR STOKES FLOW PAST A THIN SCREEN OF FINITE SIZE

Our problem of the Stokes flow past a thin screen of finite size is to solve under the boundary conditions. For the present problem, the integral in (2.19) is carried over the wall portion of the screen, W. This simple result is remarkable; it is noted that the drag is directly proportional to the electrostatic capacity of the screen of the associated problem.

STOKES FLOW PAST A CIRCULAR ANNULUS

However, we are also interested in other properties of the current, such as discharge through the ring hole, etc. We then note that the only non-vanishing component of the velocity through the ring hole is given by . Gaussian quadrature is also used in the calculation of the drag coefficient CD (equation 3. 57) ) and the mean velocity ratio u /U (equation The obtained results are.

STOKES FLOW PAST A THIN CIRCULAR SCREEN

It is expected that the magnitude of the jump is somehow related to the local average normal speed through the screen. The magnitude of the permeability k measures the ease with which the flow passes through the screen. It is expected that the permeability only depends on the detailed structure of the screen, such as the hole size i., the hole shapes and the porosity of the screen.

INTRODUCTION

The interface boundary conditions therefore serve to relate the flow variables of Darcy's law applied on one side of the interface to those of the viscous flow equations applied on the other side. This is one of the main reasons why interface conditions have been controversial in recent years. The net effect could well be a slip rather than a no-slip condition for the tangential velocity on the liquid side of the interface.

Their difference, or the tangential velocity jump across the thin layer, was found to be proportional to the tangential normal gradient. From these findings, it appears that if Darcy's law is used to model the flow through the porous region, the interface boundary conditions must relate the flow variables at the two thin film boundaries rather than at the crudely simplified interface with thickness zero. However, instead of only relating the pressures, he also included the viscous normal stresses and required the total normal stresses to be constant across the interface. repeated the analysis of the same problem but adopted a different set of interface boundary conditions.

The reason for the confusion is largely due to the fact that clear definitions of the flow variables for the equivalent mean flow in the porous region and an understanding of the true nature of such flow are still lacking. The establishment of the macroscopic equations mentioned above leads to the correct forms of the interface boundary conditions. Despite the thinness of the layer, the contribution to the tangential speed jump is not small.

An analysis of flow within an interface layer of a general nature actually leads to the complete determination of the interface boundary conditions of the second kind.

EQUATIONS OF MOTION FOR FLOW THROUGH POROUS MEDIA

The microscopic velocity distribution over a diameter of the tube usually has the following form: t. Here the x-axis coincides with the axis of the tube, and u is the x-component of the velocity. 2. 52) is seen to be identical to Darcy's law if p is identified as P, and k as the permeability of the porous medium.

The physical meaning of the macroscopic equation (2. 52), or Darcy's law, states that the average pressure falls over a distance. First, we consider the average of the velocity gradient over the volume £::, vf, that is. This states that the mean of the velocity gradient is equal to the gradient of the mean velocity.

The sum of the surface integrals on the right is therefore exactly the total volume resistance of 6 V. Assuming that D is a slowly varying function above 6 V, we can exclude it from the integral. To understand more about the mechanism of flow through porous media, we will consider the energy balance.

The term on the right-hand side is commonly known to be the energy dissipation per unit volume of the liquid. Next, we observe that the mean value of a product such as pu can be related to the product of the mean value in the following way: .. where the terms are linear in the fluctuating components. From a macroscopic point of view, the apparent work done by the body force takes care of all the contributions of the fluctuating components of velocities and pressures in the corresponding region of the porous medium.

INTERFACE BOUNDARY CONDITIONS

In order for the solution of the governing differential equations not to be indeterminate, it is necessary to establish a set of interface boundary conditions to relate the flow variables across the interface. In fact, the same macroscopic equations can be applied to the entire porous region without separate consideration of the interfacial layer. It is possible to give an estimate of the error involved in the relation (3 .14).

Therefore, the corresponding error included in (3 .14) is expected to be of the same order of magnitude as above, i.e. instead, the equations containing the Reynolds stresses for turbulent flows [15] will be more accurate, especially in the immediate vicinity of the interface where the velocity variation from the mean can be considerable. A nominal thickness o of the interface layer can be defined as the distance through which the velocity difference, q - qz.

The thickness of the interface layer c5 is assumed to be very small compared to a characteristic macroscopic length L. The flow in the interface layer connects on the inside of the layer smoothly to a flow determined by Darcy's law. On the other side of the layer, the flow is related to the mean flow of the viscous fluid region through the interface conditions of the first kind.

The orders of magnitude of the individual terms in the above equations are assigned below each term.

VISCOUS FLOWS PAST POROUS BODIES OF FINITE SIZE

With u0 known, the flow velocity distributions in both regions are given by equations (4.15) and (4.16). With this result, the interface boundary conditions of the second type for a curved porous interface can be approximated to those established for a flat interface, that is, equations (3.79) of. Using these conditions, solutions can be obtained for velocities that satisfy Darcy's law on one side of the interface and (4.4) on the other side.

Naturally, detailed knowledge of the flow within the interface layer is now lost. The graph covers only a very small range of a/..{;ik in which the effect of the porous cylinder is more visible. We assume that the Reynolds number Ud/v is so small that Stokes' equations can be applied to the fluid region.

Consequently, for the flow within the porous sphere the corresponding Reynolds number qd/v is even smaller. Since Darcy's law will be applied within the porous sphere, we will use boundary conditions of the second kind. Here we see that the flow in the porous sphere is uniform and parallel to the x-axis.

In order for the value of a/J to be approximately 200, the distance between the centers of the spherical particles must, according to (2. 53) and (2. 49), be twice the particle diameter (h/). d = 2), when it is assumed that there are 100 small particles along a diameter of the porous.

CONCLUSIONS AND DISCUSSION

The general macroscopic equations of motion together with the boundary conditions of the first order are applied to a. The result shows that the velocity field undergoes a transition from the field given by Darcy's law to the field of external fluid flow. This transition occurs in a very thin layer in the porous region in the immediate vicinity of the interface when the Darcy number is small.

It can be argued that the information obtained about the nature of the transition layer at the interface is not accurate simply because there are insufficient particles present in such a small region to ensure the validity of the macroscopic description. The region of planes can be chosen to include a sufficient number of surface pores, especially if the boundary surface is flat or has a large radius of curvature. Since the thickness 6 of the interlayer is so very small in the case of small Darcy numbers, we can claim that the layer is completely negligible and that Darcy's law can be applied in the entire region of the porous medium.

This variation should then be interpreted as a jump condition for solving the problem to be physically realistic while simultaneously treating it as mentioned above. normal velocity in the fluid region continuously joins the superficial normal velocity in the porous region. To illustrate the use of the interface boundary conditions established in this work and to show the porosity effect of a. However, when the Darcy number is not so small, as for a very porous body, the effect can be noticeable as demonstrated in the reduction of the torque and drag coefficients.

Hasimoto, H., “On the periodic fundamental solutions of the Stokes 1 equations and their application to viscous flow past a cubic series of spheres, 11 J.

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