Reply To: convergence issue for transonic flow

[vamshigundla003]

No, my inlet is not supersonic the flow is reaching 0.918Mach with this the pressure ratio 0.58 according to isentropic equations which means my inlet velocity is 315m/s.

I have kept 1 atm as supersonic pressure and 0.58 atm as outlet pressure (1 atm as inlet pressure) and tried but still the solution is not converging