Refine
Year of publication
Document Type
- Conference Proceeding (35)
- Article (23)
- Part of a Book (6)
Language
- English (64) (remove)
Keywords
- UAV (3)
- Aeroelasticity (2)
- Obstacle avoidance (2)
- 1P hub loads (1)
- Actuator disk modelling (1)
- Aircraft design (1)
- Aircraft sizing (1)
- Automotive safety approach (1)
- Autonomy (1)
- BET (1)
- Blade element method (1)
- Bumblebees (1)
- CFD (1)
- CFD propeller simulation (1)
- Correlations (1)
- Cost function (1)
- Crashworthiness (1)
- Design rules (1)
- Drag (1)
- Finite element method (1)
Institute
- Fachbereich Luft- und Raumfahrttechnik (64) (remove)
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.