High fidelity aeroelastic prediction

• Unité de recherche: INNOSUISSE
• Numéro de projet: 14323.2 PFIW-IW
• Titre du projet anglais: High fidelity aeroelastic prediction

Description succincte (Allemand)

High fidelity aeroelastic prediction

Description succincte (Anglais)

High fidelity aeroelastic prediction

Résumé des résultats (Abstract) (Allemand)

The project concerns the development of a prediction method based on high-fidelity simulation tools. it is a first, but|critical, step towards the development of a high-fidelity numerical method able to predict the dynamical behaviour of|EASA-C23 aircraft (Max Take-Off Mass below 3.5 tons). High-fidelity aerodynamic and structural modelling is essential|to keep into account the highly non-linear nature of the physics involved.

Résumé des résultats (Abstract) (Anglais)

The project concerns the development of a prediction method based on high-fidelity simulation tools. it is a first, but|critical, step towards the development of a high-fidelity numerical method able to predict the dynamical behaviour of|EASA-C23 aircraft (Max Take-Off Mass below 3.5 tons). High-fidelity aerodynamic and structural modelling is essential|to keep into account the highly non-linear nature of the physics involved.