I am trying to simulate a hypersonic glide missile, that is based of the Falcon HTV-2, traveling at Mach 5 (1715 m/s).
When I simulate it I receive an error that says: “Maximum number of iterations exceeded when calculating temperature from a thermodynamic potential. This may be caused by low-quality mesh producing unrealistic pressure in a few cells or inappropriate boundary conditions, fluid properties or time step. Inspect fields for large values in the last time step.”
I made refinements to different locations on my mesh but still received this error, so I am not sure what changes to make now and how to correct this.
I hope that you can help!
Here is a link to my project: https://www.simscale.com/workbench/?pid=623495458110671126&mi=spec%3A4eb82094-5264-4087-b715-6a8876405bc3%2Cservice%3ASIMULATION%2Cstrategy%3A2
