TY - GEN
T1 - Global Description of Flutter Dynamics via Koopman Theory
AU - Song, Jiwoo
AU - Huang, Daning
N1 - Publisher Copyright:
© 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2025
Y1 - 2025
N2 - We introduce a data-driven method for flutter analysis and prediction based on Koopman theory. The Koopman formalism enables the representation of nonlinear dynamics in a higher-dimensional linear space through the lifting of coordinates. The resulting linear model is valid over a broad region, and in some cases, globally, within the state space, offering a powerful tool for extending classical linearized stability analysis to a global stability assessment for flutter. In this paper, we present a extended bilinear model parameterized by flutter parameter to capture nonlinear behavior of flutter dynamics. We then establish a rigorous connection between the eigenvalues and eigenvectors of the extended bilinear model and those of the nonlinear flutter dynamics, addressing both fixed-point (equilibrium) and limit-cycle (flutter) cases. Finally, the proposed methods are applied to a 2D academic example and a more realistic panel flutter problem, highlighting how pre-flutter data can be utilized to characterize the flutter mechanism and predict the flutter boundary in a model-free, data-driven manner.
AB - We introduce a data-driven method for flutter analysis and prediction based on Koopman theory. The Koopman formalism enables the representation of nonlinear dynamics in a higher-dimensional linear space through the lifting of coordinates. The resulting linear model is valid over a broad region, and in some cases, globally, within the state space, offering a powerful tool for extending classical linearized stability analysis to a global stability assessment for flutter. In this paper, we present a extended bilinear model parameterized by flutter parameter to capture nonlinear behavior of flutter dynamics. We then establish a rigorous connection between the eigenvalues and eigenvectors of the extended bilinear model and those of the nonlinear flutter dynamics, addressing both fixed-point (equilibrium) and limit-cycle (flutter) cases. Finally, the proposed methods are applied to a 2D academic example and a more realistic panel flutter problem, highlighting how pre-flutter data can be utilized to characterize the flutter mechanism and predict the flutter boundary in a model-free, data-driven manner.
UR - http://www.scopus.com/inward/record.url?scp=85219583422&partnerID=8YFLogxK
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U2 - 10.2514/6.2025-0423
DO - 10.2514/6.2025-0423
M3 - Conference contribution
AN - SCOPUS:85219583422
SN - 9781624107238
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Y2 - 6 January 2025 through 10 January 2025
ER -