Hello, thank you for your reply.
I am using the pressure-based solver with coupled method and 2nd-order discretization schemes. I have also tried the density-based solver, but it seems to take many more iterations to get to the same point.
I have attached the contour plots and residuals.
Also, after the shock disappears, the inlet becomes subsonic, which is not what I set.
After fmg initialization:
after 150 iterations:
After 300 iterations:
After 500 :
After convergence:
Residuals and inlet Mach number:
Kindly help, Thanks
You are navigating away from the AIS Discovery experience