Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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Authors Index

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Author Manuscripts
Andrea dr Da Ronch
University of Southampton
61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
Yuting Dai
32 Stall flutter suppression with active camber morphing based on reinforcement learning
Kristopher Davies
German Aerospace Center (DLR)
120 Numerical Analysis of the Unsteady Wing-Tailplane Interaction in Two-Dimensional Flows
Tim De Troyer
Vrije Universiteit Brussel
197 Explainable nonlinear state-space modelling: analysing the GVT of a battery-operated aircraft
Joshua Deaton
Air Force Research Laboratory
2 Modal Design Optimization for Panel Flutter and Buckling
138 A Panel-Free Aeroelastic Solver with Adjoint Sensitivities
Samet Dede
University of Bristol
129 Aeroelastic analysis of distributed electric propulsion flexible wings
Lina Dehmlow
149 Constrained flexible wing with folding wingtip dynamics model based on Lagrange's method
Sylvie Dequand
ONERA
155 T-tail transonic flutter wind tunnel test. Part 2: Numerical restitution
Pierre-Emmanuel Des Boscs
ONERA/DAAA
162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
Joshua Deslich
United States Air Force Research Laboratory
13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
12 Including Gradient-based Transient Gust Optimization in ASTROS
Emilio Di Lorenzo
Siemens Digital Industry Software NV
225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Benjamin Diaz Villa
The University of Texas at Austin
172 Measurement of Natural Frequency and Damping of a Slender Model in Mach 5 Flow
Oliver Dieterich
Airbus Helicopters
215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
Johannes Dillinger
German Aerospace Center (DLR), Institute of Aeroelasticity
121 Design, manufacturing and identification of an active controlled flexible wing for subsonic wind tunnel testing
202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
106 Design and Experimental Characterization of a Gust-Generator Concept with Rotating-Slotted Cylinders in the Low-Speed Wind Tunnel DNW-NWB
107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
Grigorios Dimitriadis
199 Application of the unsteady compressible source and doublet panel method to flutter calculations
145 Gust load alleviation of electric aircraft with distributed propulsors using thrust vectoring
Douglas Domingues Bueno
186 Nonlinear analysis of a flexible half-wing model tested in a subsonic wind tunnel with control-surface freeplay and preloading
Mauricio Donadon
Aeronautics Institute of Technology - ITA
59 Aeroelastic analysis of a smart SMA-composite wing
70 Application of Shape Memory Alloys for Flutter Suppression in a Propeller-Driven Typical Section
Dylan Dooner
UNSW Canberra
187 Hot-wall shock-wave boundary layer interaction of a compliant cantilever in hypersonic flow
Alex Dos Reis De Souza
DTIS, ONERA, Universite de Toulouse, 31000, Toulouse, France
227 Wind Tunnel Tests for Gust Load Investigation in transonic flows – Part 2: Experimental results and control demonstration
Earl Dowell
Duke University
81 Limit Cycle Oscillation of a Plate with Piezoelectric Elements in Supersonic Flow
16 Exploring the Effect of Different Shock Impingement Angles on Aeroelastic Response for a Thin Panel
Devon Downes
National Research Council Canada
73 Testing and Analysis of a Simplified Nonlinear Horizontal Stabilator of an Aircraft
Alain Dugeai
ONERA/DAAA
62 Highly Flexible Aircraft Flight Dynamics using CFD
162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
Rebecca Durst
University of Pittsburgh
218 Adaptive Euler - efficient and predictive aerodynamics: validation and prototype development toward aeroelasticity
Stefanie Düssler
Imperial College London
29 Modelling complex actuator and sensor architectures for gust alleviation systems of flexible aircraft
28 Effect of gust models on the response prediction of a very flexible wind tunnel wing model

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