SimScale simulation projects by efecanbatur | Page 1

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The inlet Mach number is 3, and the wedge angle is 20 degrees. In this validation case, we also compare the dependence of the solution on the mesh resolution.  We also show two methods to capture the shock wave, namely, numerical Schlieren (gradient of density), and numerical shadowgraph (Laplacian of the gradient). - Copy

Retardation of flow within the boundary layer causes a reduction in the
momentum flux too. - Copy

This is an attempt to recreate a classic, well-known problem in Fluid Mechanics, the turbulent boundary layer created by steady-state, laminar flow over a flat plate. - Copy

Tutorial project for a flow analysis of a pipe junction. The project only provides the geometry to start with. See our tutorials section to have a look at the step-by-step instructions to set up the simulation.

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