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Normalized aerodynamic force response to harmonic excitation with linear and nonlinear deformation at two different excitation frequencies
Model Order Reduction in Geometrically Nonlinear Analyses
Active wing flutter suppression through multiple flap control
Measurements automation in vibroacoustics
Modern aircraft design - use of sandwich composites in aircraft wingbox
Surge - When the air flows backwards through the engine
Wind Turbine Stability Analysis - How do we increase the confidence?
fs35 Harpyie - Ground Vibration Test for full certification
Earth observation - aeroelasticity for the design of the High Altitude Platform HAP
Proven principle new shape - Why rotor blades have a kink
DLR nimmt neue Forschungsanlage für Flugzeug- und Kraftwerksturbinen in Betrieb
Bending and twisting – testing high-tech rotor blades
Windenergy - modal tests on 6 rotor blades
Vibroacoustic ground test campaign on DLRs ISTAR aircraft
Acceleration sensors for wind measuring mast at the DLR research windfarm (WiValdi)
Rigid helicopter rotor blades – Is this really enough?
Wind energy research: 1500 sensors for the rotor blades of the future
Revolutionary aircraft concepts: A new stress test for engines
Co2-neutral flying - how can aeroelasticity contribute to this?
Aircraft Configurations with Distributed Propulsion – Effects on Loads, Structural Mass, and Aeroelasticity
Semi-active flutter suppression - Improvement of the flutter stability of an aircraft by steady spoilers deflection
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