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Figure 9: The optimized wing geometry has higher pressures on the lower surface than the original wing. (Image create with Tecplot.)
  
From:
Application: Large Scale Aircraft Design Using SU2 and Pointwise
Posted Mon April 20, 2015 @02:07PM
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Application Thomas D. Economon, Francisco Palacios, Juan J. Alonso
Aeronautics & Astronautics Department
Stanford University

SU2 is an open-source collection of C++ and Python-based software for multi-physics simulation and design, and it is particularly well suited for computational fluid dynamics (CFD) and aerodynamic shape design. It is now under active development both by researchers at Stanford University and by individuals and groups at institutions all around the world.

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