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
Biagio De Maio Leoanardo	95 Ground resonance test and aeroelastic model validation of an innovative regional aircraft fitted with innovative wing tip (IWT) and adaptive morphing winglet (AMW)
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
Salvatore Di Cristofaro Leonardo	95 Ground resonance test and aeroelastic model validation of an innovative regional aircraft fitted with innovative wing tip (IWT) and adaptive morphing winglet (AMW)
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 DEUTSCHLAND GmbH	215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior 49 Research shake test on an Airbus helicopter technology demonstrator
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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