airfoils in tandem configuration
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?:confused:
I'll be so glad in advance for your help.
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