Page 266 - Finite Element Analysis with ANSYS Workbench
P. 266

12.4 Application                                          257



                                            Pressure  and  temperature  distributions  are  shown  in
                                 more details in the figures.  By using the fine mesh, the nose bow
                                 shock  is  quite  sharp  and  the  flow  behaviors  behind  it  change
                                 smoothly.    The  nose  bow  shock  hits  the  shock  from  the  cockpit
                                 creating the shock-shock interaction phenomenon.
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