|March 2, 2011, 12:00||
Compressible Boundary Condition in mid-filed
Join Date: Feb 2011
Posts: 8Rep Power: 8
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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