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Airfoil NACA 23012 results, transonic flow

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Airfoil NACA 23012 results, transonic flow

Posted May 28, 2013 at 05:38 by skeptik

What i've got about my airfoil (exp and Fluent data were extracted from article, but it's in russian. originally exp data from TZAGI report)
Click image for larger version

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So there present oscillations, they were caused by second order schemes. I'll simulate it on upwind later.

The differences in p fields are showed here:

upwind
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linear corrected 1
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