Page 265 - Finite Element Analysis with ANSYS Workbench
P. 265

e
                                                                                      a
                                                                  o
                                                        p
                              256                   Chapter 12  Compressible Flow Analysis



















                                                                  f
                                                         e
                                                                                      o
                                              o
                                         It is noted that the quality of the flow solution strongly
                                              m
                                                                            s
                                    d
                              depends  on  the  mesh.    Herrein, a strucctured  mesh  consistinng  of
                                              s
                                                                                       e
                                                                  h
                                                                            p
                                                        a
                                    9
                              271,539 cells is used in the analysis.  The cell shapes are closed to
                                    g
                                              g
                              rectangle and aligned  with  the  nose  and  cockpit  edges.    Such
                                                                   a
                                    r
                              structured mesh can improve the solution accuracy.
                                              a
                                                                  n
                                                                            h
                                                                   e
                                              o
                                                        a
                                         The computational procedure follows the steps present-
                                                                                      a
                              ed in the preceding examples.  The preddicted density, temperature,
                                                                             i
                                                        s
                                              n
                                    h
                              Mach  number  and pressure  are  shown  in the figures  from  left  to
                                                                                      e
                                              d
                                                                            u
                                    n
                                                         a
                                              .
                                    e
                              right, respectively.
   260   261   262   263   264   265   266   267   268   269   270