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Turbulent wedge - a small disturbance with a large effect
05.12.2023
16.11.2023
Propulsion of tomorrow: Introducting the Non-Rotating Annular Test Facility for Aeroelastic Investigations
20.09.2023
Withstand the pressure: NORKA luminaires in wind tunnel test
14.09.2023
New wing concepts for transport aircraft - less CO2 through higher aspect ratios
18.08.2023
Successful demonstration of active flutter suppression
16.06.2023
Flight Vibration Test - Real-Time Data Analysis using Artificial Intelligence
02.06.2023
Model Order Reduction in Geometrically Nonlinear Analyses
04.05.2023
Active wing flutter suppression through multiple flap control
27.04.2023
DLR modernisiert Windkanal für 2,8 Millionen Euro
21.03.2023
Measurements automation in vibroacoustics
08.03.2023
Modern aircraft design - use of sandwich composites in aircraft wingbox
01.02.2023
Surge - When the air flows backwards through the engine
12.01.2023
Wind Turbine Stability Analysis - How do we increase the confidence?
15.12.2022
fs35 Harpyie - Ground Vibration Test for full certification
18.11.2022
Earth observation - aeroelasticity for the design of the High Altitude Platform HAP
03.11.2022
Proven principle new shape - Why rotor blades have a kink
06.10.2022
DLR nimmt neue Forschungsanlage für Flugzeug- und Kraftwerksturbinen in Betrieb
27.09.2022
Bending and twisting – testing high-tech rotor blades
23.09.2022
Windenergy - modal tests on 6 rotor blades
07.09.2022
Vibroacoustic ground test campaign on DLRs ISTAR aircraft
14.07.2022
Rigid helicopter rotor blades – Is this really enough?
06.07.2022
Acceleration sensors for wind measuring mast at the DLR research windfarm (WiValdi)
31.05.2022
Wind energy research - 1500 sensors for the rotor blades of the future
06.05.2022
Revolutionary aircraft concepts: A new stress test for engines
20.04.2022
CO2-neutral flying - how can aeroelasticity contribute to this?
01.04.2022
DLR Göttingen at Volocopter Bruchsal - Ground Vibration Test of Volocity
18.03.2022
Aircraft Configurations with Distributed Propulsion – Effects on Loads, ...
25.02.2022
Semi-active flutter suppression
11.02.2022
New Methods to Analyze the Aeroelastic Stability of Future Lightweight Aero Engine Blades
27.01.2022
No more vibrations - Viscoelastic damping design with elastomers
13.01.2022
Save weight and have a longer service life by deflecting the control surfaces
15.12.2021
Nonlinerar effects in T-tail flutter - Numerical studies on the dynamic aeroelasticity of T-tails
30.11.2021
Novel aeroelastic instabilities on laminar wings
05.11.2021
How much noise? - cabin acoustics of future aircraft
18.10.2021
Highly flexible Wings - How flexible are you?
20.07.2021
German-French research cooperation for test of flexible aircraft wing
02.07.2021
DLR conducts vibration test on ISTAR
19.02.2021
DLR conducts ground vibration test on the Dornier `Seastar` amphibious aircraft
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Prof. Dr.-Ing.
Lorenz Tichy
Head of Institute
German Aerospace Center (DLR)
Bunsenstr. 10
37073
Göttingen
Phone:
+49 551 709-2341
Fax:
+49 551 709-2862
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