Fast Nonlinear Static Aeroelasticity Method for High-Aspect-Ratio Wings at Different Mach Regimes
Author:
Affiliation:
1. Airbus Operations SAS, 31060 Toulouse, France
2. ICA, University of Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, CNRS, 31400 Toulouse, France
3. ISAE-SUPAERO, 31055 Toulouse, France
Abstract
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C037052
Reference38 articles.
1. Turboelectric distributed propulsion benefits on the N3-X vehicle
2. Aeroelasticity of Nonconventional Airplane Configurations-Past and Future
3. The X-53 A Summary of the Active Aeroelastic Wing Flight Research Program
4. Flying on Flexible Wings
5. Robust Gust Alleviation and Stabilization of Very Flexible Aircraft
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1. Fast unsteady method for non-linear aeroelastic responses of flexible aircraft wings encountering wind gusts;Journal of Fluids and Structures;2024-05
2. Aeroelastic reduced-order modeling for efficient static aeroelastic analysis considering geometric nonlinearity;Journal of Fluids and Structures;2024-01
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