High fidelity aeroelastic prediction

• Research unit: INNOSUISSE
• Project number: 14323.2 PFIW-IW

Short description (German)

High fidelity aeroelastic prediction

Short description (English)

High fidelity aeroelastic prediction

Abstract (German)

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.

Abstract (English)

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.