I’m doing a simple aerodynamic analysis of a wing, at different flow velocities. In ‘Run 1’, the velocity is set at around 115 m/s and everything works great, with results that converge nicely. However, upon increasing the flow velocity to 150m/s, results did not stabilise. This can be seen in the run called “150 m/s divergent :(” and all the runs after that, especially the last one called “150 again longer”.
I tried refining the mesh but the problem persists. I subsequently realised that since i made the run time much shorter than than that of Run 1, it could be that it simply wasn’t running for long enought to converge, so I increased it in the runs called “150 longer”, but it didn’t help. Other than run time and flow velocity in boundary conditions, no settings or parameters were changed at all, so I don’t understand why the first run worked and the others don’t.
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