Problem:   Mach 1.6 flow past a blunt-nose-cylinder projectile at 4^o angle of           

                                                          attack (NASA-TMX-3558)

 

                                                   * Create 2D mesh, 3,400 quads        * Rotating the 2D meshes around the axis line to create 3D mesh

                                                                    * Unstructured hybrid grid (20,214 Hexahedrons, 1,800 Prisms and 120 Pyramids)

                                                                    * Inviscid flow results

 

 

 

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