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11.1 Basic Equations                                      209



                                     11.1.2  Solution Approach

                                            By observing the three differential equations above, the
                                 velocity components u and v should be determined from the x- and
                                 y-momentum  equations.    This  means  the  pressure  p  should  be
                                 obtained  from  the  mass  equation.    However,  the  mass  equation
                                 does not contain the pressure p at all.  Thus, the pressure p must be
                                 determined  together  with  the  velocity  components  u and v in  the
                                 momentum equations such that the mass is also satisfied.
                                            The  idea  above  suggests  that  the  solution  process
                                 should be an iteration process.  The process is continued until the
                                 converged solutions of u, v and p are achieved.
                                            It  is  noted  that  the  x-  and  y-momentum  equations

                                 contain the convection terms which are in form of the first-order
                                 partial  derivative.    These  convective  terms  are  nonlinear  and
                                 require  additional  effort  for  solutions.    These  terms  may  yield
                                 oscillated solutions if the mesh is not fine enough.  Fine mesh is
                                 thus  normally  needed  which  requires  more  computational  time.
                                 These factors must be realized prior to solving flow problems using
                                 any CFD software.


                                 11.2  Finite Volume Method

                                            The  finite  volume  method  is  a  popular  method  for
                                 analyzing  CFD  problems.    The  method  provides  accurate  flow
                                 solution  with  reasonable  computational  effort.    Details  of  the
                                 method  can  be  found  in  many  CFD  textbooks  including  the  one
                                 written by the author.
                                            The  method  starts  from  dividing  the  computational
                                 domain into a number of cells as shown in the figure.  Herein, we
                                 use rectangular cells to simplify explanation of the method.  Each
                                 cell  consists  of  the  three  unknowns  which  are  the  velocity
                                 components u, v and the pressure p.  The cell is surrounded by the
                                 north cell N, the east cell E, the south cell S, and the west cell W.
                                 The concept of staggered grids is applied to reduce error that might
                                 occur during the computation.
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