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shanu iyer March 5, 2012 13:02

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?

diamondx March 5, 2012 15:03

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

shanu iyer March 15, 2012 07:48

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

diamondx March 15, 2012 08:29

yes it does the job.

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