Page 145 - Introduction to Computational Fluid Dynamics
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                                                                                    WALL
                                         SYMMETRY                2D CONVECTION – CARTESIAN GRIDS
                                                                                 c
                                                                                         d
                                                                  e
                                 f                                                  j = jn
                                                                             WALL         i = in  Fin
                                                             EXIT
                            INFLOW                                               b
                                                 c                d                       e
                                                                               i = 1
                                                           WALL
                                                   WALL                Fin                WALL
                                                                                     j = 1
                                 a     WALL      b                               a  WALL  f
                                      a) Exit Boundary                      b) Periodic Boundaries
                            Figure 5.5. Exit and periodic boundaries.
                            Wall Boundary
                            At the wall, either   b or its flux q b is specified. For the first type, Equation 5.76
                            applies. If flux is specified, then at the west boundary again,
                                                                   A 1, j q 1, j
                                Su 2, j = Su 2, j + A 1, j q 1, j ,    1, j =  +   2, j ,  AW 2, j = 0,
                                                                    AW 2, j
                                                                                               (5.77)
                            where A 1, j = r j  x 2 j is the boundary area. 9

                            Symmetry Boundary
                            At this boundary, there is no flow normal to the boundary and no diffusion either.
                            Thus, with reference to Figure 5.4, for a scalar  , q 1, j = 0.0. For vectors, the normal
                            velocity component u 1 (1, j)=0and u 2 (1, j) = u 2 (2, j). In all cases, AW 2, j = 0.


                            Outflow Boundary
                            The outflow boundary is one where the fluid leaves the domain of interest. The
                            boundary condition at the outflow or exit plane is most uncertain. To understand
                            the main issues involved, consider Figure 5.5(a) in which de represents the outflow
                            boundary. Now to affect the boundary condition, we may assume that the Peclet
                            number (u 1  x 1 /
)| b is very large. In this case, the AE coefficient of all near-
                            boundary nodes will be zero and, therefore, no explicit boundary condition   b or
                            ∂ /∂n| b is necessary. In many circumstances, this assumption may not be strictly
                            valid. One way to overcome this difficulty is to shift boundary de further down-
                            stream than required in the original domain specification. Thus, one carries out
                            computations over an extended domain and effect AE = 0 at the new location of
                            de. A third alternative is to assume that a fully developed state prevails at de so that
                            both the first as well as the second normal derivatives are zero. Most researchers
                            prefer to set the second-order derivative to zero and extract   b by extrapolation
                            while the transport equation is solved with AE = 0.

                            9  In turbulent flows, the wall boundary requires special attention when the HRE form of the e–
                              model is employed. This matter will be taken up in the next section.
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