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  • Compressible Flow Over an Airfoil - Validation

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To make the comparison easier, expand the Appearance options and change Coloring to Banded, then change Number of colors to 20.

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By comparing this to the Stanford’s pressure contour, it is easy to see that they are similar.  Also, the numerical minimum and maximum values are significantly close, by less than within 10%. 

References

Copeland, Sean and Economon, Thomas. "Quick Start Tutorial - SU2 - ADL Software Documentation." Aerospace Design Lab. Stanford University, 1 July 2014. Web. 7 August 2017.

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