“…These flexible aero-structures pose a considerable modeling challenge, as they involve highly coupled and nonlinear interactions between the aerodynamic and structural dynamics. A range of aeroelastic modeling methods exist, from high-fidelity models able to simulate the coupled fluid flow fields and the deformation of the wing structure (Goza & Colonius, 2017;Mittal & Iaccarino, 2005;Peskin, 2002), to controloriented data-driven models including viscous and unsteady effects (Brunton et al, 2013;Hemati et al, 2017;Hickner et al, 2022), and lower-fidelity models such as doublet-lattice methods (Albano & Rodden, 1969), strip theory (Kim et al, 2008), and panel methods (Fasel et al, 2021;Fonzi et al, 2020;Murua et al, 2012). These methods provide accurate models of aeroelastic effects; however, computationally more efficient models are often necessary for optimization and control, even at the expense of some fidelity.…”