Problem:   Mach 1.6, 2.3, 4.63 flow past an circular-arc-cylinder-boattail                

                                                          projectile with Reynolds number equal to 6.6x10⁶.

                                                          NASA-TMX-3558

 

                                                   * Supersonic viscous flow                              * Circular-arc-cylinder-boattail projectile

                                                   * Finite element                                             * Unstructured grid

 

 

 

 

BACK                                                                                                 NEXT