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Airfoil NACA 23012 results, transonic flow
Posted May 28, 2013 at 06:38 by skeptik
Tags airfoil, openfoam, rhocentralfoam, transonic
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)
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
linear corrected 1
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
linear corrected 1
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