Dynamic Adaptive Mesh Coarsening
I am using Fluent for calculating a 2D axisymmetric compressible trans-sonic free jet.
My domain is resembles a hemisphere, air jet from left, small length of wall above the jet, outlet is the round boundary above and over the domain, and an axis on the bottom of the boundary. The inlet is a mass-flow inlet, the outlet is a pressure-outlet, and convergence is good, so what am i asking for?
Dynamic adaptive meshing should be used to coarsen the regions of low gradients and refine the areas of high gradients. Every 10 iterations the mesh is adapted.
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