TetrUSS is a time-tested computational aerodynamic capability servicing the configuration aerodynamic needs of NASA's airframe and exploration programs. Present capabilities include rapid grid generation, inviscid and viscous flow analysis and design, special functional boundary conditions, and ease of use.

TetrUSS has a rich history of innovation over the past decade. It has left a wide footprint across many NASA programs, industry projects, and in the inspiring students toward the pursuit of aeronautics. Future goals are focused on improving process automation, better integrating functional capabilities, and increasing its impact on new NASA projects and programs.

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Site developed by Jordan Schwarz

NASA Official Responsible For Content: Dr. Neal T. Frink
Site Curator: The TetrUSS Team
Last Updated: August 25, 2006

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