I am trying to get a compressible wind tunnel test of a wing. The wing is at an altitude of 43000 ft and a airspeed of 250 m/s (mach 0.85). I want to see if the wing is viable at this speed, and eventually compare three different wing planforms to see which is best.
I filled in all values correctly, I think. I changed pressure and viscosity, k and omega I kept the standard value. But every time i try to simulate it it says “The maximum number of iterations exceeded” Is it possible to simulate such a high airspeed? could the low quality mesh operation has something to doe with it?