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Old   March 5, 2012, 13:02
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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?
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Old   March 5, 2012, 15:03
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Ghazlani M. Ali
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you need a very big domain at the entrance of the air. use pressure far-field and give it the mach number you want
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New to ICEM CFD, try this document --> http://goo.gl/G2gkE
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Old   March 15, 2012, 07:48
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The domain given is a circular one...the boundary conditions are farfield and the pressure outlet. are these conditions suitable for the problem?
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Old   March 15, 2012, 08:29
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yes it does the job.
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New to ICEM CFD, try this document --> http://goo.gl/G2gkE
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