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 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
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
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
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
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
Flávio Silvestre	149 Constrained flexible wing with folding wingtip dynamics model based on Lagrange's method
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
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
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 DLR	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 147 Design of a High Aspect Ratio Windtunnel Model for Transonic Gust Load Alleviation
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	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 169 Linearized CFD-and CSM based flutter process for very flexible aircraft
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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