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
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 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
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
Flávio J. Silvestre
TU-Berlin
58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
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 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
Flávio Silvestre
149 Constrained flexible wing with folding wingtip dynamics model based on Lagrange's method
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-Institute of Aeroelasticity
113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter
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
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
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 Sybe Stavorinus
Technische Universität Berlin
98 Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
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
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

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