icem cfd
 

hi, i am working on the design of a supersonic ramped engine inlet . I did a structured mesh. what are the boundary types i must give. please help?

you need a very big domain at the entrance of the air. use pressure far-field and give it the mach number you want

icem_structured
 

The domain given is a circular one...the boundary conditions are farfield and the pressure outlet. are these conditions suitable for the problem?

yes it does the job.