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. Campagna
Primo
;
A. Milazzo
Secondo
;
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.
giu-2024
Settore IIND-01/D - Costruzioni e strutture aerospaziali
9781644903186
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].
File in questo prodotto:
File Dimensione Formato  
DG_VLM_phdDays2024.pdf

accesso aperto

Tipologia: Versione Editoriale
Dimensione 609.23 kB
Formato Adobe PDF
609.23 kB Adobe PDF Visualizza/Apri

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/10447/664754
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 0
  • ???jsp.display-item.citation.isi??? 0
social impact