Refine
Year of publication
Institute
Has Fulltext
- no (66) (remove)
Document Type
- Conference Proceeding (37)
- Article (19)
- Part of a Book (7)
- Report (2)
- Book (1)
Keywords
- 1P hub loads (1)
- Aeroelasticity (1)
- Aircraft design (1)
- Bumblebees (1)
- Correlations (1)
- Cost function (1)
- Design rules (1)
- Drag (1)
- Flight control (1)
- Flutter (1)
- Geometry (1)
- Green aircraft (1)
- Hybrid-electric aircraft (1)
- MAV (1)
- Multi-objective optimization (1)
- Obstacle avoidance (1)
- Path planning (1)
- Propeller whirl flutter (1)
- Statistics (1)
- UAV (1)
- Unmanned Air Vehicle (1)
- Unsteady aerodynamics (1)
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.
Computational aeroelastic analysis and design of the HIRENASD wind tunnel wing model and tests
(2007)
In the Collaborative Research Center SFB 401 at RWTH Aachen University, the numerical aeroelastic method SOFIA for direct numerical aeroelastic simulation is being progressively developed. Numerical results obtained by applying SOFIA were compared with measured data of static and dynamic aeroelastic wind tunnel tests for an elastic swept wing in subsonic flow.