In this work, a novel computational tool is introduced for rapid aeroelastic analysis of composite wings, integrating an aerodynamic Vortex Lattice Method with a structural Interior Penalty Discontinuous Galerkin method. After the mathematical description of the aeroelastic model, some results for a composite wing are presented to investigate the influence of varying lamination angles on the wing displacement, twist, and divergence speed. Validation against commercial software confirms the effectiveness of the approach.
D. Campagna, A. Milazzo, I. Benedetti, V. Gulizzi (2024). Coupling VLM and DG methods for the aeroelastic analysis of composite wings. In Aerospace Science and Engineering. IV Aerospace PhD-Days 2024 (pp. 80-83). Association of American Publishers [10.21741/9781644903193-18].
Coupling VLM and DG methods for the aeroelastic analysis of composite wings
D. CampagnaPrimo
;A. MilazzoSecondo
;I. Benedetti
Penultimo
;V. Gulizzi
Ultimo
2024-06-01
Abstract
In this work, a novel computational tool is introduced for rapid aeroelastic analysis of composite wings, integrating an aerodynamic Vortex Lattice Method with a structural Interior Penalty Discontinuous Galerkin method. After the mathematical description of the aeroelastic model, some results for a composite wing are presented to investigate the influence of varying lamination angles on the wing displacement, twist, and divergence speed. Validation against commercial software confirms the effectiveness of the approach.File | Dimensione | Formato | |
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