In this paper, the accuracy and practical capabilities of three dierent reduced-order models (ROMs) are explored: an enhanced implicit condensation and expansion (EnICE) model, a finite element beam model, and a finite volume beam model are compared for their capability to accurately predict the nonlinear structural response of geometrically nonlinear built-up wing structures. This work briefly outlines the different order reduction methods, highlighting the associated assumptions and computational effort. The ROMs are then used to calculate the wing deflection for different representative load cases and these results are compared with the global finite element model (GFEM) predictions when possible. Overall, the ROMs are found to be able to capture the nonlinear GFEM behavior accurately, but differences are noticed at very large displacements and rotations due to local geometrical effects.
|Journal||The Aeronautical Journal|
|Publication status||Accepted/In press - 14 Jul 2021|