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Normalized aerodynamic force response to harmonic excitation with linear and nonlinear deformation at two different excitation frequencies
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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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