Authors Index

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [Q] [R] [S] [T] [V] [W] [X] [Y] [Z]

Author	Manuscripts
Jos Aalbers Netherlands Aerospace Centre	230 Unsteady RANS-based Computational Aeroelastic Simulations of X-56A Flutter for the Third Aeroelastic Prediction Workshop
Stephan Adden IBK Innovation	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
Frederico Afonso Instituto Superior Tecnico	237 Topology Optimization of Aeroelastically Scaled Wing Models based on Additive Manufacturing
Majid Ahmadi	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
Rafic Ajaj Khalifa University	145 Gust load alleviation of electric aircraft with distributed propulsors using thrust vectoring 100 On the aeroelasticity of high aspect ratio strut-braced wings: A parametric study
Farbod Alijani	142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction
Hamad Almarzooqi Khalifa University	100 On the aeroelasticity of high aspect ratio strut-braced wings: A parametric study
Anna Altkuckatz German Aerospace Center (DLR) - Institute of Aeroelasticity	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
Muhittin Altug AIRBUS HELICOPTERS DEUTSCHLAND GmbH	49 Research shake test on an Airbus helicopter technology demonstrator
Muhittin-Nami Altug Airbus Helicopters	215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
Xavier Amandolese CNAM	160 Design and experimental tests of a flexible wing of high-aspect ratio for investigating flutter mechanisms
Mohammadreza Amoozgar	145 Gust load alleviation of electric aircraft with distributed propulsors using thrust vectoring
Chao An	92 Hypersonic flutter analysis based on three-dimensional local piston theory 83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
Hao Wei, Elijah Ang	108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Carlo Aquilini Airbus Defence & Space GmbH	47 From Multivariate Random Loads To Deterministic Load Distributions: An Exact Method For Aeroelastic Design 44 Robust design through identification of main components from multivariate random loads
Felix Arevalo Airbus Defence and Space	170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project 171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Jürgen Arnold DLR Institut für Aeroelastik	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft 66 Design of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics
Jérôme BAZILE AIRBUS	8 Wind Law Proposal for Aircraft Control in Turbulence
Davide Balatti	33 Aeroelastic hybrid testing for industrial applications
Roger Ballester Claret	17 Aeroelastic reliability based optimisation of composite plates via surrogate modeling
ignacio Ballesteros Ruiz Airbus UK	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Daniel Balogh SZTAKI	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
Guilherme C. Barbosa TU-Berlin	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Milán Barczi SZTAKI, Budapest, Kende u. 13-17, 1111, Hungary	10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement
Arnaud Barnique Cedrat Technologies	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Leonardo Barros da Luz Instituto Tecnológico de Aeronáutica	118 Rayleigh-Ritz method with multibody dynamics for highly flexible structures
Julius Bartasevicius TU Munich	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Martin Bauer German Aerospace Center DLR, Institute of Aerodynamics and Flow Technology, Lilienthalplatz 7, 38108, Braunschweig Germany	205 High-Fidelity Multidisciplinary Maneuver Simulations of the Falcon 2000LX ISTAR
Antônio Bernardo Guimarães Neto Instituto Tecnológico de Aeronáutica	132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
Ying Bi	38 Deep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities 37 Nonlinear Aeroelastic Response Analysis of Unmanned Multi-body Aircraft with Free Play 39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Anna Biancotto Royal Netherlands Aerospace Centre	101 Integrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip
Laurent Blanc LTDS	150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Hans Martin Bleecke Airbus Operations	30 Machine learning to forecast unsteady, motion-induced unsteady forces
Hans Bleecke Airbus Operations	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft
Brianna Blocher The University of Texas at Austin	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
Peter Blom Netherlands Aerospace Centre	230 Unsteady RANS-based Computational Aeroelastic Simulations of X-56A Flutter for the Third Aeroelastic Prediction Workshop
Christophe Blondeau ONERA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA 34 A modular TSM solver for aeroelastic analysis and optimizations
Bernd Boche Technische Universität Berlin	195 On the preparation of a flexible real-time aircraft model for a flight simulator
Stefan de Boer TU Delft	57 Continuous parametrisation of wing movable layout for design optimisation
Vitor Borges Santos Instituto Tecnológico de Aeronáutica	132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
Vincent Bouillaut DAAA, ONERA, Institut Polytechnique de Paris, 92320 Chatillon, France	157 Aeroelastic design of a drone for research on active flutter control 227 Wind Tunnel Tests for Gust Load Investigation in transonic flows – Part 2: Experimental results and control demonstration
Carsten Braun FH Aachen University of Applied Sciences	89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
Marc Braune German Aerospace Center (DLR) - Institute of Aeroelasticity	200 Shape Identification of a wing model by additive manufacturing for transonic 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
Roeland de Breuker Delft University of Technology	198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
Roeland De Breuker Delft University of Technology	142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction 57 Continuous parametrisation of wing movable layout for design optimisation 207 Application of aeroelastic tailoring for control surface reversal 164 Mechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators
Elsa Bréus Dassault Aviation	165 T-tail transonic flutter wind tunnel test part 1: Sealing system design and model testing 104 Flutter prediction correlations with wind tunnel measurements on a T-tail flutter mock-up
Ralf Buchbach DLR German Aerospace Center	49 Research shake test on an Airbus helicopter technology demonstrator
Gabriel Buendia Airbus Defence	171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Thomas Buete German Aerospace Center	200 Shape Identification of a wing model by additive manufacturing for transonic tunnel testing
Heiko Böhlken	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
Nils Böhnisch FH Aachen University of Applied Sciences	89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
Marc Böswald DLR German Aerospace Center	113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter 114 An Incremental Modal Shape Sensing Method for Geometrically Non-Linear Deformed Wings 77 A Procedure for Flutter Analysis with Nonlinear Experimental Modal Parameters 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior 49 Research shake test on an Airbus helicopter technology demonstrator
Thomas Büte	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
Italo CAFARELLI ONERA	67 Analysis of the impact of forced pitching oscillations in transonic flow on the transition onset and the aeroelastic behaviour of an airfoil
Natale Calvi 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)
Wesley Cantwell Khalifa University	100 On the aeroelasticity of high aspect ratio strut-braced wings: A parametric study
Xiaolong Cao Institute of Beijing Mechanics and Electronics	5 The simulation and flight verification of active aeroelastic control
Flávio Cardoso-Ribeiro Instituto Tecnológico de Aeronáutica	118 Rayleigh-Ritz method with multibody dynamics for highly flexible structures 117 Comparative analysis of flight maneuver loads between flexible and rigid aircraft
Flávio Luiz Cardoso-Ribeiro Instituto Tecnológico de Aeronáutica	132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks 222 Identification of Flexible Aircraft Parameters with Varying Flexibility Configurations: Integrating Elastic Effects and Sensor Data
Andrea Castrichini Airbus Operations Ltd.	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device 26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation 96 Parametric nonlinear flutter analysis of the semi-aeroelastic hinges during manoeuvres and gust encounters 33 Aeroelastic hybrid testing for industrial applications 137 Nonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings
Guilherme Castrignano Tavares Embraer S.A	71 Flight flutter test modal identification by using nature inspired algorithms: A classical mathematical modeling
Breno Castro Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Alvaro Cea Imperial College London	82 Differentiable Aeroelastic Framework Suitable for Industrial Modelling of Nonlinear Loads on Accelerators 137 Nonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings
Jiri Cecrdle Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Carlos E. S. Cesnik University of Michigan	79 Finite element model update of a very flexible wing using ground vibration testing data 105 Investigation on Sensor Selection Applied on a Vehicle-as-a-Sensor Concept in High-Speed Flight
Carlos Cesnik University of Michigan	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle 35 Evaluation of Aeroelastic Models for Gust Response Prediction in Very Flexible Wings
Xie Changchuan	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
An Chao	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Guilherme Chaves Barbosa Technische Universität Berlin	42 Aeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study 98 Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
Song Chen	136 The Design and Analysis of Tensegrity Morphing Wing
Zhiying Chen	87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles
Kelvin Chi-Wing Cheng Imperial College London	137 Nonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings
Massimiliano Chillemi University of Messina	225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Haeseong Cho Jeonbuk National University	135 Machine learning-based parametric model order reduction for the gust load analysis
Pawel Chwalowski NASA LaRC	20 Transonic limit cycle oscillations of the benchmark supercritical wing
Noel Clemens The University of Texas at Austin	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle 172 Measurement of Natural Frequency and Damping of a Slender Model in Mach 5 Flow
Declan Clifford University of Southampton	61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips 168 Model order reduction for nonlinear aeroelastic dynamical system using automatic differentiation
Hector Climent Airbus Defence and Space	170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project 171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Vasco Coelho Instituto Superior Tecnico	237 Topology Optimization of Aeroelastically Scaled Wing Models based on Additive Manufacturing
Marta Colella Sapienza University of Rome - Department of Mechanical and Aerospace Engineering	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device
Jonathan E. Cooper University of Bristol	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Jonathan Cooper University of Bristol	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration 145 Gust load alleviation of electric aircraft with distributed propulsors using thrust vectoring 125 Active flutter suppression and gust load alleviation of wings incorporating floating wingtips 122 Wing mounted hydrogen fuel tanks: mitigating the aeroelastic penalties of dry wing configurations? 129 Aeroelastic analysis of distributed electric propulsion flexible wings 80 Aeroelastic optimisation of a cantilevered plate with local damping application
Josh Coppin Airbus UK	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Giuliano Coppotelli Università of Rome “La Sapienza”	65 Experimental investigation of a highly flexible wing
Enzo Cosentino Airbus UK	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Kaique Silveira Viana Costa Instituto Tecnológico de Aeronáutica	222 Identification of Flexible Aircraft Parameters with Varying Flexibility Configurations: Integrating Elastic Effects and Sensor Data
Péter Zoltán Csurcsia Vrije Universiteit Brussel	197 Explainable nonlinear state-space modelling: analysing the GVT of a battery-operated aircraft
Yongdong Cui	108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Sunpeth Cumnuantip DLR – Institute of Aeroelasticity, Bunsenstrasse 10, 37073 Goettingen, Germany	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft 4 Influence of Cruise Altitude Variation on the Turbulence Loads of a Medium-Range Transport Configuration 7 Assessment of aeroelastic stability of high aspect wing aircraft during the preliminary design
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
Marc Eitner The University of Texas at Austin	172 Measurement of Natural Frequency and Damping of a Slender Model in Mach 5 Flow
Anders Ellmo Saab AB	43 Ground Vibration Testing and Model Update of a Transonic Flutter Wind Tunnel Model
Holger Ernst	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
Bart Eussen Netherlands Aerospace Centre	198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
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
Álvaro Antonio García Quesada Technische Universität Berlin	42 Aeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study 98 Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
Eric Garrigues	104 Flutter prediction correlations with wind tunnel measurements on a T-tail flutter mock-up
Vincent de Gaudemaris ONERA/LTDS	150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Ilya Genkin	110 Estimation of slender body elastic rates and accelerations using a combination of measured data
Nicholas Giannelis University of New South Wales, Canberra	187 Hot-wall shock-wave boundary layer interaction of a compliant cantilever in hypersonic flow 189 Transonic aeroelastic limit cycles and their dependence on freestream conditions
Christian Gogu ISAE-Supaero	25 Control surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria
Demian Gomes da Silva Embraer S.A	71 Flight flutter test modal identification by using nature inspired algorithms: A classical mathematical modeling
Pedro J. González TU-Berlin	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Pedro José González Technische Universität Berlin	42 Aeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study
Pedro González	149 Constrained flexible wing with folding wingtip dynamics model based on Lagrange's method
Pedro José González Ramirez Technische Universität Berlin	98 Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
Yves Govers DLR	113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Donato Grassi Politecnico di Milano	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
Gabriele Grasso Airbus Defence and Space GmbH	47 From Multivariate Random Loads To Deterministic Load Distributions: An Exact Method For Aeroelastic Design
Huaiyuan Gu University of Bristol	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration 125 Active flutter suppression and gust load alleviation of wings incorporating floating wingtips 122 Wing mounted hydrogen fuel tanks: mitigating the aeroelastic penalties of dry wing configurations?
Yingsong Gu NPU	210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
Nicolas Guerin ONERA	103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Janto Gundlach German Aerospace Center (DLR), Institute of Aeroelasticity	114 An Incremental Modal Shape Sensing Method for Geometrically Non-Linear Deformed Wings
Nicolas Guérin	190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Hamed Haddad Khodaparast	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 33 Aeroelastic hybrid testing for industrial applications
Michael Hadjipantelis University of Bath	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Zhang Haibo	136 The Design and Analysis of Tensegrity Morphing Wing
Vega Handojo DLR German Aerospace Center	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft 4 Influence of Cruise Altitude Variation on the Turbulence Loads of a Medium-Range Transport Configuration
Charlotte Hanke German Aerospace Center (DLR), Institute of Aeroelasticity	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings 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
Patrick Hartl	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
Oleh Havaza National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”	235 Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
Longfei He	63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis
Fintan Healy University of Bristol	125 Active flutter suppression and gust load alleviation of wings incorporating floating wingtips 122 Wing mounted hydrogen fuel tanks: mitigating the aeroelastic penalties of dry wing configurations?
Tobias Hecken German Aerospace Center (DLR)	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
Benjamin Herrmann Hamburg University of Technology	46 Doublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters
Pedro Higino Cabral Embraer S. A.	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Jonathan Hilger DLR	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Mirko Hornung Technical University of Munich	24 Experimental and numerical assessment on the aeroelastic behavior of a NLF airfoil with oscillating control surfaces 10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement 116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
Vladimír Hostinský Brno University of Technology - FME - Institute of Aerospace Engineering	133 Unified model of sandwich panel core and faces for aeroelastic optimization
Yingyou Hou	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Kunhui Huang	11 Wind tunnel test of gust response for distributed propeller-wing system 156 Measurement and Control System Design for Propeller-Wing System Experiments
Maria Francesca Illiano Leonardo Helicopters	21 Nonlinear aeroelastic modeling workflow using Simcenter Nastran
Kevin Jacobson NASA LaRC	69 Gradient-based Optimization of the Common Research Model Wing Subject to CFD-based Gust and Flutter Constraints 20 Transonic limit cycle oscillations of the benchmark supercritical wing
Kijoo Jang Samsung Electronics Company	135 Machine learning-based parametric model order reduction for the gust load analysis
Karl Janssens Siemens Digital Industry Software NV	225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Johan Jansson KTH	218 Adaptive Euler - efficient and predictive aerodynamics: validation and prototype development toward aeroelasticity
Sanuja Jayatilake University of Bristol	166 Analysis of inertial gust load relief characteristics of high aspect ratio wings
Ivo Jebáček Brno University of Technology - FME - Institute of Aerospace Engineering	133 Unified model of sandwich panel core and faces for aeroelastic optimization
Chen Ji	179 Experimental study on transonic buffeting of launch vehicles with large-diameter fairing using elastic models 240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Shakir Jiffri	33 Aeroelastic hybrid testing for industrial applications
Yi Jin Guangdong BODA Electronic Technology Co., Ltd	5 The simulation and flight verification of active aeroelastic control
Zdenek Johan	104 Flutter prediction correlations with wind tunnel measurements on a T-tail flutter mock-up
Völker Johannes	88 Aircraft vibration from React to Predict
Nicholas Jones PCKrause & Associates	13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
Cédric Julien	17 Aeroelastic reliability based optimisation of composite plates via surrogate modeling
Andres Jurisson Netherlands Aerospace Centre	198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
TAEHYOUN KIM University of Washington Bothell, USA	232 Prediction of Limit Cycle Oscillations Based on Dynamic Eigen Decomposition of Flight Test Data
Christoph Kaiser DLR, Institute of Aeroelasticity	112 A general solver for the prediction of flutter and buffet onset 54 Effect of Turbulent Wedges on the Steady and Unsteady Aerodynamics of a Forward Swept Laminar Wing 123 Analysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver
Seung-Hoon Kang Seoul National University	135 Machine learning-based parametric model order reduction for the gust load analysis
Mordechay Karpel Karpel Dynamic Consulting Ltd.	170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project
Marlus Kerninski Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Thiemo Kier	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 141 Assessment of Active Load Control Approaches for Transport Aircraft – Simulation and Wind Tunnel Test 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV 99 Flexible aircraft conceptual co-design based on the RCE framework 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Thiemo M. Kier German Aerospace Center (DLR), Institute of System Dynamics and Control	107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
Spyridon Kilimtzidis University of Patras	199 Application of the unsteady compressible source and doublet panel method to flutter calculations
Thomas Klimmek German Aerospace Center (DLR)	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
Johannes Knebusch DLR German Aerospace Center	215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior 49 Research shake test on an Airbus helicopter technology demonstrator
Christopher Koch German Aerospace Center (DLR), Institute of Aeroelasticity	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft 18 Whirl flutter analysis using linearized propeller transfer matrices
Martin Kolar Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Raymond Kolonay United States Air Force Research Laboratory	12 Including Gradient-based Transient Gust Optimization in ASTROS
Ramesh Konatala	103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Vassilis Kostopoulos University of Patras	199 Application of the unsteady compressible source and doublet panel method to flutter calculations
Wolf R. Krueger DLR Institute of Aeroelasticity	7 Assessment of aeroelastic stability of high aspect wing aircraft during the preliminary design 141 Assessment of Active Load Control Approaches for Transport Aircraft – Simulation and Wind Tunnel Test
Eduardo Krupa Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Wolf R. Krüger German Aerospace Center (DLR) - Institute of Aeroelasticity	121 Design, manufacturing and identification of an active controlled flexible wing for subsonic wind tunnel testing 58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings 106 Design and Experimental Characterization of a Gust-Generator Concept with Rotating-Slotted Cylinders in the Low-Speed Wind Tunnel DNW-NWB
Wolf Krüger	142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction
Cedric LIAUZUN ONERA	67 Analysis of the impact of forced pitching oscillations in transonic flow on the transition onset and the aeroelastic behaviour of an airfoil
Yang Lan	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Valentin Lanari ONERA	165 T-tail transonic flutter wind tunnel test part 1: Sealing system design and model testing 155 T-tail transonic flutter wind tunnel test. Part 2: Numerical restitution
Vito Laraspata Politecnico di Bari	199 Application of the unsteady compressible source and doublet panel method to flutter calculations
Fernando Lau Instituto Superior Tecnico	237 Topology Optimization of Aeroelastically Scaled Wing Models based on Additive Manufacturing
Nicolò Laureti Sapienza University of Rome	161 Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics
Alessandro Laurini Siemens Digital Industry Software NV	225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
SiHun Lee Samsung Electronics Company	135 Machine learning-based parametric model order reduction for the gust load analysis
Sangmin Lee Seoul National University	135 Machine learning-based parametric model order reduction for the gust load analysis
Bernardo Leite Instituto Superior Tecnico	237 Topology Optimization of Aeroelastically Scaled Wing Models based on Additive Manufacturing
Jieli, Daryl Leo	108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Arnaud Lepage DAAA, ONERA, Institut Polytechnique de Paris, 92320 Chatillon, France	165 T-tail transonic flutter wind tunnel test part 1: Sealing system design and model testing 157 Aeroelastic design of a drone for research on active flutter control 231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig 227 Wind Tunnel Tests for Gust Load Investigation in transonic flows – Part 2: Experimental results and control demonstration
Cate Leszcz University of Colorado, Boulder	2 Modal Design Optimization for Panel Flutter and Buckling
Chang Li	87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles 84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method 63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Gongde Li	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Keyu Li	63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Jinying Li	32 Stall flutter suppression with active camber morphing based on reinforcement learning
Guo Li Chinese Academy of Aerospace Aerodynamics	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Zhuoneng Li University of Southampton	61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
Cedric Liauzun ONERA	34 A modular TSM solver for aeroelastic analysis and optimizations
Cédric Liauzun ONERA/DAAA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
Manoela Lima Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Zhu Lipeng	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Chenyu Liu Beihang University	93 Gust response analysis of supersonic aircraft based on three-dimensional piston theory 92 Hypersonic flutter analysis based on three-dimensional local piston theory
Dawei Liu	11 Wind tunnel test of gust response for distributed propeller-wing system
Yi Liu Institute of Beijing Mechanics and Electronics	5 The simulation and flight verification of active aeroelastic control
Gertjan Looye	109 Decentralized Control of Ailerons for Gust Load Alleviation 107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Mark Lowenberg University of Bristol	166 Analysis of inertial gust load relief characteristics of high aspect ratio wings
Raul Lozano Vargas Airbus UK	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Pascal Lubrina ONERA	190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Didier Lucor	17 Aeroelastic reliability based optimisation of composite plates via surrogate modeling
Christopher Lupp U.S. Air Force Research Laboratory	9 Aeroelastic Mission Optimization of Very Flexible Vehicles including Take-Off and Climb Constraints
Wellington Luziano Paulo Junior	186 Nonlinear analysis of a flexible half-wing model tested in a subsonic wind tunnel with control-surface freeplay and preloading
Yasser M. Meddaikar DLR - Institute of Aeroelasticity	99 Flexible aircraft conceptual co-design based on the RCE framework
Liang Ma	84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method 63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Xiaoping Ma	38 Deep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities 37 Nonlinear Aeroelastic Response Analysis of Unmanned Multi-body Aircraft with Free Play
Terence Macquart University of Bristol	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Holger Mai German Aerospace Center (DLR) - Institute of Aeroelasticity	121 Design, manufacturing and identification of an active controlled flexible wing for subsonic wind tunnel testing 200 Shape Identification of a wing model by additive manufacturing for transonic tunnel testing 141 Assessment of Active Load Control Approaches for Transport Aircraft – Simulation and Wind Tunnel Test 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
Jyoti Majhi Indian Institute of Science	175 Prediction of transonic buffet in an axial flow fan using global stability analysis
Vadim Maltsev University of Southampton	61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
William Mansey University of Bristol	125 Active flutter suppression and gust load alleviation of wings incorporating floating wingtips
Paolo Mantegazza Politecnico di Milano	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
Luca Marchetti Politecnico di Milano	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
Luca Marino TU Delft	183 Nonlinear analysis of combined rate and acceleration limits effect on actuator performance
Sylvie Marquier Airbus Operations SAS	25 Control surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria
Pier Marzocca RMIT University Melbourne	89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
Paolo Mastracci Airbus UK	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device 96 Parametric nonlinear flutter analysis of the semi-aeroelastic hinges during manoeuvres and gust encounters
Franco Mastroddi Sapienza University of Rome	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device 161 Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics
Davide Mastrodicasa Siemens Digital Industry Software NV	225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Kevin McHugh United States Air Force Research Laboratory	2 Modal Design Optimization for Panel Flutter and Buckling 13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings 12 Including Gradient-based Transient Gust Optimization in ASTROS
Yasser Meddaikar DLR	10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
Tobias Meier DLR - German Aerospace Center	215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
David Meier DLR - German Aerospace Center	215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
Ana C. Meinicke University of Michigan	105 Investigation on Sensor Selection Applied on a Vehicle-as-a-Sensor Concept in High-Speed Flight
Ana Cristine Meinicke University of Michigan	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
Eduardo de Melo Pinto Instituto Tecnológico de Aeronáutica	117 Comparative analysis of flight maneuver loads between flexible and rigid aircraft
Yang Meng Beihang University	5 The simulation and flight verification of active aeroelastic control 93 Gust response analysis of supersonic aircraft based on three-dimensional piston theory 94 IMU-based deformation reconstruction for highly flexible wings 41 Aerodynamic analysis of aircraft wings using a coupled PM-BL approach 27 Nonlinear aeroelastic analysis of large wind turbine blades
Christoph Mertens Netherlands Aerospace Centre	101 Integrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip 28 Effect of gust models on the response prediction of a very flexible wind tunnel wing model
Kolja Michel German Aerospace Center (DLR), Institute of System Dynamics and Control	109 Decentralized Control of Ailerons for Gust Load Alleviation 107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
Boris Micheli DLR Institut für Aeroelastik	66 Design of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics
Francesco M. A. Mitrotta University of Bristol	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Iren Ani Mkhoyan Netherlands Aerospace Centre	230 Unsteady RANS-based Computational Aeroelastic Simulations of X-56A Flutter for the Third Aeroelastic Prediction Workshop
Amir Hossein Modarres Aval University of Southampton	61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
Eduardo Molina Embraer S.A.	226 Comparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating wing
Charly Mollet ONERA/DAAA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
Reza Moosavi University of Hertfordshire, UK	139 Aeroelasticity of smart wing in supersonic flow
Joseph Morlier ISAE-Supaero	25 Control surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria
Breno Moura Castro Embraer S.A.	186 Nonlinear analysis of a flexible half-wing model tested in a subsonic wind tunnel with control-surface freeplay and preloading
Daniel Muradas Odriozola Airbus Operations SAS	25 Control surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria
Vincenzo Muscarello RMIT University Melbourne	89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
Thulasi Mylvaganam Imperial College London	29 Modelling complex actuator and sensor architectures for gust alleviation systems of flexible aircraft
Martin Müller	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
Florian Müller German Aerospace Center (DLR)	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
Dor Naftaly	78 Flight-dynamics aeroelastic coupling in flexible and very flexible wings
Misi Nagy SZTAKI	119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Mihaly Nagy HUN-REN SZTAKI	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
Eisuke Nakagawa University of Tokyo	85 Elastic wind tunnel model design via eigenvector-based level-set topology optimization
Venkateswaran Narayanaswamy North Carolina State University	81 Limit Cycle Oscillation of a Plate with Piezoelectric Elements in Supersonic Flow
Jan Navrátil Brno University of Technology - FME - Institute of Aerospace Engineering	133 Unified model of sandwich panel core and faces for aeroelastic optimization
Andrew Neely UNSW Canberra	187 Hot-wall shock-wave boundary layer interaction of a compliant cantilever in hypersonic flow
Doug Neill ICME Design	12 Including Gradient-based Transient Gust Optimization in ASTROS
Renata Nepumoceno-Merce Airbus Helicopters	215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
Jens Neumann DLR	66 Design of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics 159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Bing Feng Ng	108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Ruslan Nikitin National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”	235 Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
Jens Nitzsche DLR, Institute of Aeroelasticity	112 A general solver for the prediction of flutter and buffet onset 214 Investigation of vortex-induced vibrations to compare Reynolds-averaged Navier-Stokes and detached-eddy simulations 123 Analysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver
Salvatore Nocerino Leoanrdo	95 Ground resonance test and aeroelastic model validation of an innovative regional aircraft fitted with innovative wing tip (IWT) and adaptive morphing winglet (AMW)
Julia Noël Airbus Operations	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft
Fernando de Oliveira Moreira Embraer S.A.	117 Comparative analysis of flight maneuver loads between flexible and rigid aircraft
Emre Ongut Siemens Digital Industries Software	21 Nonlinear aeroelastic modeling workflow using Simcenter Nastran
Ludovic Onofri Università of Rome “La Sapienza”	65 Experimental investigation of a highly flexible wing
Edoardo Orazi 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)
Pedro Paglione Instituto Tecnológico de Aeronáutica	118 Rayleigh-Ritz method with multibody dynamics for highly flexible structures
Rafael Palacios 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 82 Differentiable Aeroelastic Framework Suitable for Industrial Modelling of Nonlinear Loads on Accelerators 137 Nonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings
Nicola Paletta Airbus Defence and Space	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Asa Palmer University of Dayton Research Institute	13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
Aditya Panigrahi The University of Texas at Austin	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
Alexander Pankonien Air Force Research Lab	13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
Younggeun Park Seoul National University	135 Machine learning-based parametric model order reduction for the gust load analysis
Bálint Patarics HUN-REN Institute for Computer Science and Control	99 Flexible aircraft conceptual co-design based on the RCE framework
Mario Peinado Garcia Sapienza University of Rome - Department of Mechanical and Aerospace Engineering	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device
Alex Pereira do Prado Embraer S. A.	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Amanda Perroni Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Luisa Piccolo Serafim 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
Alberto Pirrera University of Bristol	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Dale Pitt The Boeing Company - Retired	6 Flutter and Gust Response of a Wing with Aerodynamic Gaps
Marco Pizzoli Sapienza University of Rome	161 Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics
Antoine Placzek ONERA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA 150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Charles Poussot-Vassal 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
Beatriz Pulido Airbus Defence and	171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Luca Pustina Sapienza University of Rome	161 Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics
David Quero DLR, Institute of Aeroelasticity	112 A general solver for the prediction of flutter and buffet onset 123 Analysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver
Álvaro A. G. Quesada TU-Berlin	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Eric Rantet Aviation Design	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Daniella E. Raveh	78 Flight-dynamics aeroelastic coupling in flexible and very flexible wings 110 Estimation of slender body elastic rates and accelerations using a combination of measured data
Bruno Regina Instituto Tecnológico de Aeronáutica (ITA)	226 Comparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating wing
Lars Reimer DLR Institute of Aerodynamics and Flow Technology	141 Assessment of Active Load Control Approaches for Transport Aircraft – Simulation and Wind Tunnel Test
Manuel Reyes Airbus Defence and Space	171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Djamel Rezgui	125 Active flutter suppression and gust load alleviation of wings incorporating floating wingtips 122 Wing mounted hydrogen fuel tanks: mitigating the aeroelastic penalties of dry wing configurations? 208 Experimental investigation into the dynamic characteristics of a tilting multirotor system 129 Aeroelastic analysis of distributed electric propulsion flexible wings
Sergio Ricci Politecnico di Milano	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration 231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Luca Riccobene Politecnico di Milano	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
Leif Rieck Hamburg University of Technology	46 Doublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters
Marcello Righi ZHAW and ETHZ	65 Experimental investigation of a highly flexible wing
Antoine Riols-Fonclare ONERA/DAAA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
Cristina Riso Georgia Institute of Technology	35 Evaluation of Aeroelastic Models for Gust Response Prediction in Very Flexible Wings
Markus Ritter German Aerospace Center (DLR), Institute of Aeroelasticity	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft 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
Andrea Da Ronch University of Southampton	168 Model order reduction for nonlinear aeroelastic dynamical system using automatic differentiation
Carlo Rotundo Delft University of Technology	174 Aeroelastic tailoring of dual-role propellers
Serena Russo DREAM INNOVATION	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Francesco Saltari Sapienza University of Rome	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device 161 Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics
Divya Sanghi University of Michigan	35 Evaluation of Aeroelastic Models for Gust Response Prediction in Very Flexible Wings
Emilio Santos Airbus Defence and Space	170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project
Roberto Sbarra Università of Rome “La Sapienza”	65 Experimental investigation of a highly flexible wing
Thomas G. Schmidt German Aerospace Center (DLR), Institute of Aeroelasticity	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
Thomas Schmidt	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
Jean-Sébastien Schotté ONERA	150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Simon Schulz DLR - German Aerospace Center	109 Decentralized Control of Ailerons for Gust Load Alleviation
Matthias Schulze DLR – Institute of Aeroelasticity, Bunsenstrasse 10, 37073 Goettingen, Germany	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft 7 Assessment of aeroelastic stability of high aspect wing aircraft during the preliminary design
Jan Schwochow DLR	119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Andrea Sciacchitano Delft University of Technology	101 Integrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip
Carlos Sebastia Saez Chair of Aircraft Design, Technical University of Munich	24 Experimental and numerical assessment on the aeroelastic behavior of a NLF airfoil with oscillating control surfaces 10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement
Thomas Seren Technical University of Munich	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
Alan Serena Airbus De	170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project
Yali Shao Beihang University	83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
Tanuj Sharma School of Civil, Aerospace and Design Engineering, University of Bristol	208 Experimental investigation into the dynamic characteristics of a tilting multirotor system
Bilal Sharqi University of Michigan	79 Finite element model update of a very flexible wing using ground vibration testing data
Junlin Shen	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Pengtao Shi NPU	210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
SangJoon Shin Seoul National University	135 Machine learning-based parametric model order reduction for the gust load analysis
Roberto Silva Instituto Tecnológico de Aeronáutica (ITA)	226 Comparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating wing
Gefferson Silva Technische Universität Berlin	59 Aeroelastic analysis of a smart SMA-composite wing 195 On the preparation of a flexible real-time aircraft model for a flight simulator
Roberto da Silva Aeronautics Institute of Technology - ITA	70 Application of Shape Memory Alloys for Flutter Suppression in a Propeller-Driven Typical Section
Felipe da Silva Embraer	70 Application of Shape Memory Alloys for Flutter Suppression in a Propeller-Driven Typical Section
Flávio Silvestre	149 Constrained flexible wing with folding wingtip dynamics model based on Lagrange's method
Flávio José Silvestre Technische Universität Berlin	42 Aeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study 98 Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
Flavio Silvestre Technische Universität Berlin	59 Aeroelastic analysis of a smart SMA-composite wing 195 On the preparation of a flexible real-time aircraft model for a flight simulator
Flávio J. Silvestre TU-Berlin	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Magan Singh Indian Institute of Science	176 Transonic shock oscillations in an oscillating finite span wing
Kautuk Sinha	142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction
Tomas Sinnige Delft University of Technology	174 Aeroelastic tailoring of dual-role propellers
Julian Sinske DLR German Aerospace Center	113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter 49 Research shake test on an Airbus helicopter technology demonstrator
Federica Siotto Airbus UK	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Jayant Sirohi The University of Texas at Austin	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle 172 Measurement of Natural Frequency and Damping of a Slender Model in Mach 5 Flow
Miroslav Smid Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Hollis Smith Air Force Research Laboratory	138 A Panel-Free Aeroelastic Solver with Adjoint Sensitivities
Keith Soal DLR German Aerospace Center	113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter 116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV 215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter 49 Research shake test on an Airbus helicopter technology demonstrator
Breno Soares da Costa Vieira Instituto Tecnológico de Aeronáutica	132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
Jurij Sodja Delft University of Technology	133 Unified model of sandwich panel core and faces for aeroelastic optimization 101 Integrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip 114 An Incremental Modal Shape Sensing Method for Geometrically Non-Linear Deformed Wings 57 Continuous parametrisation of wing movable layout for design optimisation 183 Nonlinear analysis of combined rate and acceleration limits effect on actuator performance 207 Application of aeroelastic tailoring for control surface reversal 174 Aeroelastic tailoring of dual-role propellers
Chen Song Beihang University	93 Gust response analysis of supersonic aircraft based on three-dimensional piston theory
Leonardo Soria Politecnico di Bari	199 Application of the unsteady compressible source and doublet panel method to flutter calculations
Aleli Sosa Chavez Siemens Digital Industry Software NV	225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Abraão Ferreira de Sousa Neto Instituto Tecnológico de Aeronáutica	222 Identification of Flexible Aircraft Parameters with Varying Flexibility Configurations: Integrating Elastic Effects and Sensor Data
Cleber Spode	186 Nonlinear analysis of a flexible half-wing model tested in a subsonic wind tunnel with control-surface freeplay and preloading
Felix Stalla German Aerospace Center (DLR), Institute of System Dynamics and Control	121 Design, manufacturing and identification of an active controlled flexible wing for subsonic wind tunnel testing 107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
Bret Stanford NASA LaRC	69 Gradient-based Optimization of the Common Research Model Wing Subject to CFD-based Gust and Flutter Constraints 20 Transonic limit cycle oscillations of the benchmark supercritical wing
Jan Starek Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Nichoas Stathopoulos L3Harris	73 Testing and Analysis of a Simplified Nonlinear Horizontal Stabilator of an Aircraft
Gerrit Stavorinus TU-Berlin	42 Aeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study 149 Constrained flexible wing with folding wingtip dynamics model based on Lagrange's method 58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Gerrit Sybe Stavorinus Technische Universität Berlin	98 Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
Cyrille Stephan ONERA	160 Design and experimental tests of a flexible wing of high-aspect ratio for investigating flutter mechanisms 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Bernd Stickan Airbus Operations GmbH	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft 123 Analysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver
Kilian Streitenberger Institute of Aeroelasticity - German Aerospace Center (DLR)	214 Investigation of vortex-induced vibrations to compare Reynolds-averaged Navier-Stokes and detached-eddy simulations
Till Strothteicher DLR	191 Automated Tuning of a Baseline Flight Control System with Maneuver Load Alleviation for an Energy-Efficient Passenger Airplane
Vitalii Sukhov National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”	235 Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
Afzal Suleman University of Victoria	237 Topology Optimization of Aeroelastically Scaled Wing Models based on Additive Manufacturing
Zhan Sun	84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method
Xiaoyang Sun Airbus UK	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Özge Süelözgen Research Scientist, DLR (German Aerospace Center)	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Martin TANG DLR	119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Béla Takarics HUN-REN Institute for Computer Science and Control	10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement 196 Co-Design of the Aeroelastic Wing Parameters and the Flutter Control Law 99 Flexible aircraft conceptual co-design based on the RCE framework
Bela Takarics SZTAKI	103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
Jun Kang Tan	108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Martin Tang DLR German Aerospace Center	77 A Procedure for Flutter Analysis with Nonlinear Experimental Modal Parameters 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV 107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing 49 Research shake test on an Airbus helicopter technology demonstrator
Ali Tatar Istanbul Technical University	129 Aeroelastic analysis of distributed electric propulsion flexible wings 80 Aeroelastic optimisation of a cantilevered plate with local damping application
Chien Ming, Jonathan Tay	108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Robert Taylor University of Texas Arlington	13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
Daniel Teubl TU Munich	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Andrew Thelen NASA Langley Research Center	69 Gradient-based Optimization of the Common Research Model Wing Subject to CFD-based Gust and Flutter Constraints
Frank Thielecke Hamburg University of Technology	46 Doublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters
Carsten Thiem DLR German Aerospace Center	119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 49 Research shake test on an Airbus helicopter technology demonstrator
Reik Thormann Airbus Operations	30 Machine learning to forecast unsteady, motion-induced unsteady forces
Fabrice Thouverez LTDS	150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Xinhai Tian	210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
Huub Timmermans Netherlands Aerospace Centre	230 Unsteady RANS-based Computational Aeroelastic Simulations of X-56A Flutter for the Third Aeroelastic Prediction Workshop
Branislav Titurus School of Civil, Aerospace and Design Engineering, University of Bristol	166 Analysis of inertial gust load relief characteristics of high aspect ratio wings 208 Experimental investigation into the dynamic characteristics of a tilting multirotor system
Francesco Toffol Politecnico di Milano	167 Passive and active load alleviation technologies for UHARW wings
MIguel Torralba Airbus Defence and Space	171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Szabolcs Toth SZTAKI	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Natsuki Tsushima Japan Aerospace Exploration Agency	85 Elastic wind tunnel model design via eigenvector-based level-set topology optimization 200 Shape Identification of a wing model by additive manufacturing for transonic tunnel testing
Hoang Thien Phu VO	88 Aircraft vibration from React to Predict
Balint Vanek SZTAKI	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Bálint Vanek	196 Co-Design of the Aeroelastic Wing Parameters and the Flutter Control Law 99 Flexible aircraft conceptual co-design based on the RCE framework 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Santosh Varigonda North Carolina State University	81 Limit Cycle Oscillation of a Plate with Piezoelectric Elements in Supersonic Flow
Srikanth Vasudevan Delft University of Technology	164 Mechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators
Kartik Venkatraman Indian Institute of Science	176 Transonic shock oscillations in an oscillating finite span wing 175 Prediction of transonic buffet in an axial flow fan using global stability analysis
Fabio Vetrano Airbus Operations SAS	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device
Silvia Vettori Siemens Digital Industry Software NV	225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Ondrej Vich Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Cyrille Vidy Airbus Defence & Space GmbH	47 From Multivariate Random Loads To Deterministic Load Distributions: An Exact Method For Aeroelastic Design 44 Robust design through identification of main components from multivariate random loads
Coen de Visser Delft University of Technology	198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
Alessandra Vizzaccaro	33 Aeroelastic hybrid testing for industrial applications
Jarmil Vlach Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Robin Volkmar DLR	113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Arne Voß DLR	1 Gust Encounter of a Supersonic Fighter Aircraft using CFD Methods 58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Pierre Vuillemin 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
Christian Wallace DLR (German Aerospace Center)	163 Lidar-based gust load alleviation – increasing the load reduction potential through a two-degree-of-freedom controller architecture
Zhiqiang Wan	87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles 84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method 63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Xiaozhe Wang	87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles 84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method 63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Gaozhan Wang Beihang University	92 Hypersonic flutter analysis based on three-dimensional local piston theory
Peihan Wang Beihang University	45 Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method
Wei Wang	156 Measurement and Control System Design for Propeller-Wing System Experiments
Xuerui Wang Delft University of Technology	181 Nonlinear Incremental Robust Model Predictive Control for a Nonlinear Aeroservoelastic System 183 Nonlinear analysis of combined rate and acceleration limits effect on actuator performance 164 Mechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators
Guido Weber Liebherr-Aerospace Lindenberg	109 Decentralized Control of Ailerons for Gust Load Alleviation
Zsombor Wermeser	196 Co-Design of the Aeroelastic Wing Parameters and the Flutter Control Law
Michelle Westin Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Viresh Wickramasinghe NRC	73 Testing and Analysis of a Simplified Nonlinear Horizontal Stabilator of an Aircraft
Hannes Wilke Technische Universität Berlin	195 On the preparation of a flexible real-time aircraft model for a flight simulator
Thomas Wilson Airbus Operations Ltd.	96 Parametric nonlinear flutter analysis of the semi-aeroelastic hinges during manoeuvres and gust encounters 137 Nonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings
Kristoffer Wingstedt SAAB	218 Adaptive Euler - efficient and predictive aerodynamics: validation and prototype development toward aeroelasticity
Benjamin King Sutton Woods University of Bristol	166 Analysis of inertial gust load relief characteristics of high aspect ratio wings
Zhigang Wu Beihang University	102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test 45 Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method
Matthias Wuestenhagen DLR - Institute of System Dynamics and Control	99 Flexible aircraft conceptual co-design based on the RCE framework
Matthias Wüstenhagen	103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Wei Xiao	102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test
Changchuan Xie	93 Gust response analysis of supersonic aircraft based on three-dimensional piston theory 92 Hypersonic flutter analysis based on three-dimensional local piston theory 94 IMU-based deformation reconstruction for highly flexible wings 83 Reduced order modeling analysis for flexible wing using a co-rotational beam element 41 Aerodynamic analysis of aircraft wings using a coupled PM-BL approach 27 Nonlinear aeroelastic analysis of large wind turbine blades 11 Wind tunnel test of gust response for distributed propeller-wing system 156 Measurement and Control System Design for Propeller-Wing System Experiments
Italo Ximenes Aeronautics Institute of Technology - ITA	70 Application of Shape Memory Alloys for Flutter Suppression in a Propeller-Driven Typical Section
Pu Xing	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Chao Yang	102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test 32 Stall flutter suppression with active camber morphing based on reinforcement learning 87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles 45 Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method 156 Measurement and Control System Design for Propeller-Wing System Experiments 64 Aeroelastic optimization of commercial aircraft considering high-precision aerodynamic performance
Zhichun Yang	210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
Zhuolin Ying	38 Deep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities 37 Nonlinear Aeroelastic Response Analysis of Unmanned Multi-body Aircraft with Free Play 39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Tomohiro Yokozeki	85 Elastic wind tunnel model design via eigenvector-based level-set topology optimization
Fanglin Yu Technical University of Munich	10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement 116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 99 Flexible aircraft conceptual co-design based on the RCE framework
Changkun Yu	102 Modeling of shaker-structure coupling system and its application in ground aeroelastic stability test
Jie Yu	136 The Design and Analysis of Tensegrity Morphing Wing
Kaihua Yuan Institute of Beijing Mechanics and Electronics	5 The simulation and flight verification of active aeroelastic control
Ni Zao	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Jian Zhang	39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Zhitao Zhang	11 Wind tunnel test of gust response for distributed propeller-wing system 156 Measurement and Control System Design for Propeller-Wing System Experiments
Yuhui Zhang	94 IMU-based deformation reconstruction for highly flexible wings 83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
Tingyu Zhang TUDelft	181 Nonlinear Incremental Robust Model Predictive Control for a Nonlinear Aeroservoelastic System
Duoyao Zhang	83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
Zou Zhicheng	68 Efficient and high-precision nonlinear static aeroelastic load analysis method based on vortex lattice method acceleration
Zijian Zhu	38 Deep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities 37 Nonlinear Aeroelastic Response Analysis of Unmanned Multi-body Aircraft with Free Play 39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Lipeng Zhu	41 Aerodynamic analysis of aircraft wings using a coupled PM-BL approach
Chen Zhu	38 Deep Reinforcement Learning for Aeroservoelastic Control of Unmanned Multi-Body Aircraft with Geometric Nonlinearities 37 Nonlinear Aeroelastic Response Analysis of Unmanned Multi-body Aircraft with Free Play 39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
Markus Zimmer German Aerospace Center (DLR)	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft

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