Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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Nicolò Fabbiane
ONERA
157 Aeroelastic design of a drone for research on active flutter control
Nicolo Fabbiane
17 Aeroelastic reliability based optimisation of composite plates via surrogate modeling
Christian Fagiano
17 Aeroelastic reliability based optimisation of composite plates via surrogate modeling
Touraj Farsadi
14 Gust load alleviation efficiency in an optimized composite wing through the integration of wingtip devices: Incorporating folding and twist strategies
15 Optimizing high aspect ratio composite wings through geometrically nonlinear aeroelastic tailoring
Michael Fehrs
German Aerospace Center (DLR)
54 Effect of Turbulent Wedges on the Steady and Unsteady Aerodynamics of a Forward Swept Laminar Wing
120 Numerical Analysis of the Unsteady Wing-Tailplane Interaction in Two-Dimensional Flows
Johan Feldwisch
German Aerospace Center DLR, Institute of Aeroelasticity, Bunsenstraße 10, 37073, Göttingen Germany
205 High-Fidelity Multidisciplinary Maneuver Simulations of the Falcon 2000LX ISTAR
Johan Moritz Feldwisch
DLR Institute of Aeroelasticity
193 Effect of flow separation on discrete gust loads for a free-flying elastic aircraft
Nicolas Fezans
DLR (German Aerospace Center)
191 Automated Tuning of a Baseline Flight Control System with Maneuver Load Alleviation for an Energy-Efficient Passenger Airplane
163 Lidar-based gust load alleviation – increasing the load reduction potential through a two-degree-of-freedom controller architecture
Sebastiano Fichera
33 Aeroelastic hybrid testing for industrial applications
Evangelos Filippou
Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS Delft, The Netherlands
207 Application of aeroelastic tailoring for control surface reversal
Nicolas Forestier
104 Flutter prediction correlations with wind tunnel measurements on a T-tail flutter mock-up
Stephane Fournier
University of Bristol
80 Aeroelastic optimisation of a cantilevered plate with local damping application
Maxim Freydin
Technion
81 Limit Cycle Oscillation of a Plate with Piezoelectric Elements in Supersonic Flow
Michael Friswell
33 Aeroelastic hybrid testing for industrial applications
Balazs Fritsch
HUN-REN SZTAKI
116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
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