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January 17, 2006, 04:53 |
Pressure inlet problems
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#1 |
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Hi all, I have a supersonic compressible flow and am using a UDF to define the the total pressure at the inlet. I started by ignoring the Supersonic/initial gauge pressure and got a result which looked wrong. I then changed the initial(static) pressure to the same as the total pressure and get an error after a few time steps. Any ideas or experience with this sort of problem would help a great deal. Thanks.
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