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Unsteady aerodynamics with respect to large motion are difficult to predict for generic airfoil geometries. This work seeks to determine what aspects of the unsteady separation process are similar and disparate for varying airfoil geometry.
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This page is a summary of: Parametric Modal Decomposition of Dynamic Stall, AIAA Journal, January 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057077.
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