This tutorial demonstrates how to use the density based implicit solver to solve a transient flow through a 3D nozzle and study the pressure, velocity, Mach number, the mass flow rate at the exit of the nozzle. Dynamic mesh adaption was used in the process to refine the mesh during the iterations. To download the 3D geometry, please got to this link: http://www.raefkobeissi.com/index.php/nozzle/
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