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Aircraft optimisation for reduced drag needs to consider fluid-structure interactions. We show that the speed the numerical simulation of the fluid-structure interaction can be negtively affected by the mesh deformation algorithms. A hybrid approach is proposed to speed up the process significantly.

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This page is a summary of: Hybrid Mesh Deformation for Aerodynamic-Structural Coupled Adjoint Optimization, AIAA Journal, February 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j061293.
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