Global Description of Flutter Dynamics via Koopman Theory

Jiwoo Song, Daning Huang

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

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.

Original languageEnglish (US)
Title of host publicationAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624107238
DOIs
StatePublished - 2025
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 - Orlando, United States
Duration: Jan 6 2025Jan 10 2025

Publication series

NameAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025

Conference

ConferenceAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Country/TerritoryUnited States
CityOrlando
Period1/6/251/10/25

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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