Optimal Sparsity in Nonlinear Reduced Order Models Applied to an All-Movable Wing with Freeplay in Transonic Flow
Author:
Affiliation:
1. RMIT University
2. Self
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-1266
Reference31 articles.
1. NONLINEAR BEHAVIOR OF A TYPICAL AIRFOIL SECTION WITH CONTROL SURFACE FREEPLAY: A NUMERICAL AND EXPERIMENTAL STUDY
2. Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos
3. Identification of freeplay and aerodynamic nonlinearities in a 2D aerofoil system with via higher-order spectra
4. Characterization of a 3DOF aeroelastic system with freeplay and aerodynamic nonlinearities – Part I: Higher-order spectra
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Optimal Sparsity in Nonlinear Nonparametric Reduced Order Models for Transonic Aeroelastic Systems;AIAA Journal;2024-09-02
2. Parameterization of nonlinear aeroelastic reduced order models via direct interpolation of Taylor partial derivatives;Nonlinear Dynamics;2024-07-19
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