CFD Project Page

Updated 11/20/03

In 2003, I worked on a CFD project to calculate shocks. The flow field is described as an inviscid compressible Eulerian fluid.

Jet exiting from orifice with shock. Mach number shown in color. The dimensions of the mesh are 104x30x30.

Propagation of shock bubble. Density shown in color. The dimensions of the mesh are 40x40x40.