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Aeroelastic optimization of flight structures typically requires a modal approximation. We explore different ways in which gradients can be accommodated in that modal approximation.
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This page is a summary of: Fixed- and Free-Mode Flutter Derivatives During Aeroelastic Optimization, AIAA Journal, December 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064166.
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