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224                  Chapter 11  Incompressible Flow Analysis



















                                    To perform the flow analysis, click on the Fluent Launcher
                                     and enter the Density as 1.0 and the Viscosity as 0.1 in the
                                     same way as in the preceding example.
                                    The  boundary  conditions  are  then  applied  by  clicking  on
                                     Inlet (the  name  assigned  earlier)  and  enter  the  Velocity

                                     Magnitude as 1.0.
                                    Click on Outlet and enter the Pressure as 0.0.
                                    On the Cylinder, the boundary condition is selected as No
                                     Slip.
                                    We follow the same procedure as explained in the preced-
                                     ing  example  to  execute  the  problem  for  solutions.    The
                                     solution residuals associated with the continuity and the two
                                     momentum  equations  decrease  with  the  number  of
                                     iterations are shown in the figure.
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