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Aerodynamic design often requires a large number of expensive CFD simulations. This expense can become impractical when there are a large number of design variables, particularly when adjoint techniques are not available. We propose a deep generative model for compactly and sufficiently representing aerodynamic geometry. It allows fast design space exploration and empirically accelerates airfoil optimization convergence by at least two times compared to state-of-the-art parameterization methods.

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This page is a summary of: Airfoil Design Parameterization and Optimization Using Bézier Generative Adversarial Networks, AIAA Journal, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059317.
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