Fast flutter evaluation of very flexible wing using interpolation on an optimal training dataset
Author:
Affiliation:
1. Imperial College London
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1345
Reference35 articles.
1. Structural Loads Analysis for Commercial Transport Aircraft
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1. Data-Driven Modeling for Transonic Aeroelastic Analysis;Journal of Aircraft;2023-10-25
2. Investigation of Geometrically Nonlinear Effects in the Aeroelastic Behavior of a Very Flexible Wing;AIAA SCITECH 2023 Forum;2023-01-19
3. Design of an Aeroelastically Scaled Model in a Compressible Air Wind Tunnel Facility Using Multifidelity Multi-Objective Bayesian Optimization;AIAA SCITECH 2023 Forum;2023-01-19
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