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March 2, 2011, 11:00
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Compressible Boundary Condition in mid-filed
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#1 |
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New Member
Join Date: Feb 2011
Posts: 8
Rep Power: 15  |
good morning to everybody.
I want to simulate a compressible flow on airfoil on a reducted domain, says, at 2 chord on a c -grid from the profile. in which way i can impose the correct bc's? Velocity- inlet is not correct in compressible flow. The far-field is not applicable by definition... thank you in advance |
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March 7, 2011, 04:52
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#2 |
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New Member
Join Date: Feb 2011
Posts: 8
Rep Power: 15 |
What abour the general non-reflective BC'S?
Anyone use it? |
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