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June 27, 2016, 06:48
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XFlow Naca 0012 Validation
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New Member
Berkay Yasin YILDIRIM
Join Date: Jun 2016
Posts: 1
Rep Power: 0  |
Hello. I am trying to validate XFlow results. I have started with analyzing NACA 0012 for Re 3000000. I have generated 3D NACA 0012 with 10k points,and analyzed in 2D. I could not get close results to the experimental airfoil data. I used 0.2 resolved scale, around 0.0003m target resolved scale and 0.004m wake resolution. It took 1.5 hours but not a valid result. How can I increase accuracy or what can be wrong about my approach? Thank you
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