vedama
Subscriber
It's flow over an axisymmetric airfoil. I have a very fine, grid-independent result that has a lot of cells. I'm trying to arrive at the same result with fewer cells. I start with a coarse grid and adapt the solution using pressure, density and velocity gradients, and also allowing the geometry to adapt based on the grid-independent solution so the curvature of the airfoil is accurately captured.
You are navigating away from the AIS Discovery experience