Reduced Order Modeling and Analysis of Airfoil Flutter Using Dynamics-Based Autoencoders
Year: 2025
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j064881
Institutions: University of Southern California, University of Michigan
Language: English
Subfield: Statistical and Nonlinear Physics
Field: Physics and Astronomy
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4410729693