Problem: Mach 1.2 and 0.2 flow past the Javelin rocket at 10 and 5 degrees angle of

                                                          attack.

 

                                             * Build 2D mesh, 13,400 elements, 13,721 nodes            *Assign tail surface and wing cross section shape

                                             * Sweep 2D mesh around the axis to generate 3D mesh.

                     * 64 pyramids, 2880 prisms and 425,88 hexahedron.

 

2D mesh with tail surface                                              Surface mesh after sweeping around the axis

 

Pressure contour                                                        Mach number contour

 

 

Velocity plot contour              Mach number contour

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