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One of the ways to reduce aerodynamic drag of a wing is to shape it so that turbulence is reduced. In this paper we develop a tool that automatically finds the shape that reduces that turbulence and thus drag the most.

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This page is a summary of: Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach, AIAA Journal, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058944.
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