Filtern
Dokumenttyp
- Teil eines Buches (Kapitel) (2) (entfernen)
Institut
- Fachbereich Luft- und Raumfahrttechnik (2) (entfernen)
In this part of the MEGADESIGN project, aeroelastic effects are introduced into the aerodynamic analysis of aircrafts by coupling DLR’s flow solvers TAU and FLOWer to a Timoshenko-beam solver. The emerging aeroelastic solvers and a method for the automatic identification of Timoshenko-beam models for wing-box structures were integrated into a simulation environment enabling the combined optimisation of aerodynamic wing shape and structure.