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

                                                       projectile with Reynolds number equal to 6.6x10⁶.

                                                       NASA-TMX-3558

 

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

                                 * Finite element unstructured grid

 

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