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The safe design of panels against aeroelastic instability is driven by the determination of critical aerodynamic conditions. We show an improved numerical strategy to tackle the aeroelastic problem using tow-steered composite panels considering a multi-criterion optimization framework and manufacturing constraints.

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This page is a summary of: Supersonic Flutter and Buckling Optimization of Tow-Steered Composite Plates, AIAA Journal, January 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057282.
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