Flow Models
The Navier–Stokes equations can be nondimensionalized for a domain whose width (h0) is much smaller than its lateral dimension(s) (l0) (see Ref. 1 for a detailed discussion). When Re(h0/l0)2 << 1, and terms of order (h0/l0)2 and higher are neglected, the Navier–Stokes equations reduce to a modified form of the Stokes equation, which must be considered in conjunction with the continuity relation.
Figure 9-5: The coordinate system employed for the average flow velocity.
The equations are most conveniently expressed in a local coordinate system, in which x' and y' are tangent to the plane of the reference surface, and z' is perpendicular to the surface, as illustrated in Figure 9-5. Using this coordinate system:
Here pfilm is the pressure resulting from the fluid flow, μ is the fluid viscosity, and (vx',vy') is the fluid velocity in the reference plane (which varies in the z' direction).
By making the assumption that the viscosity is constant through the film thickness, these equations can be integrated, yielding the in-plane velocity distributions. The following equations are derived:
(9-4)
(9-5)
The constants C1x', C2x', C1y', and C2y' are determined by the boundary conditions.
Equation 9-4 shows that the flow is a linear combination of laminar Poiseuille and Couette flows. The velocity profile is quadratic in form, as shown in Equation 9-5.
The average flow rate in the reference plane, vav, is given by:
The forces acting on the walls are determined by the normal component of the viscous stress tensor, τ, at the walls (τn, where n is the normal that points out of the fluid domain). The viscous stress tensor takes the form:
Neglecting the gradient terms, which are of order h0/l0, results in the simplified stress tensor:
(9-6)
The components of the stress tensor can be expressed in terms of the velocity and pressure gradients using Equation 9-4. Note that the normals to both the wall and the base are parallel to the z’ direction, to zeroth order in h0/l0. The forces acting on the base and the wall are therefore given by:
General Slip Boundary Condition
Assuming a slip length of Lsw at the wall and a slip length of Lsb at the base, the general slip boundary conditions are given by:
For non-identical slip lengths the constants C1x', C2x', C1y', and C2y' take the following values:
The average flow rate becomes:
which can be expressed in vector notation as:
The above equation can be written on the form:
(9-7)
where vav,c is a term associated with Couette flow, and vav,p is a coefficient associated with Poiseuille flow (see Table 9-2 below).
The forces acting on the two boundaries are given by:
(9-8)
Note that the z' direction corresponds to the nr direction. The x' and y' directions correspond to the two tangent vectors in the plane. Using vector notation the forces become:
In Equation 9-8 it is assumed that nw = nr and nb = nr. In COMSOL Multiphysics, the accuracy of the force terms is improved slightly over the usual approximation (which neglects the slope of the wall and base as it is of order h0/l0) by using the following equations for nw and nb:
These definitions are derived from Equation 9-4 and Equation 9-5 and include the additional area that the pressure acts on as a result of the wall slope.
The force terms can be written on vector notation:
(9-9)
where fw,p is the Poiseuille coefficient for the force on the wall, and fw,c incorporates the Couette and normal forces (due to the pressure) on the wall. Similarly, fb,p is the Poiseuille coefficient for the force on the base, and fb,c incorporates the Couette and normal forces (due to the pressure) on the base.
The cases of identical slip length and non-slip are limiting cases of the formulas derived above. The main results are summarized in Table 9-2, where the constants defined in Equation 9-7 and Equation 9-9 are used.