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226                  Chapter 11  Incompressible Flow Analysis



                                         y
                                                            u    0
                                                                v
                                    (0,10)
                                                 1
                                     u  1         1 . 0                           10
                                     v   0               3           6
                                                                              p   0      x
                                                                 6
                                              10         10             20           10


                                                            u    0               (40, 10)
                                                                v
                                                                                       

                                    The  computed  flow  solutions  in  forms  of  the  velocity
                                     contours and path lines for this latter case are shown in the
                                     figures.  Such solutions highlight benefits and  capabilities
                                     of  the  software  to  handle  complicated  flow  domain
                                     effectively.    The  computed  solutions  provide  insight  into
                                     the  flow  field  to  increase  understanding  of  the  flow
                                     behaviors.
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