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December 25, 2011, 09:54 |
airfoils in tandem configuration
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#1 |
New Member
shamsoddin ghiami
Join Date: Nov 2011
Location: IRAN
Posts: 3
Rep Power: 14 |
I have two airfoils in tandem configuration in front of an air stream in mach0.3
I used spalart-almaras as a viscous model to achieve the results.I tried all boundary conditions u think.BUT nothing I could find,I mean I can not achieve the correct periodic pattern of drag coefficient.what are the correct boundary conditions? where is my problem? I'll be so glad in advance for your help. tnx |
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