Author |
Manuscripts |
Francesco Saltari
Sapienza University of Rome
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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
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Divya Sanghi
University of Michigan
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35 Evaluation of Aeroelastic Models for Gust Response Prediction in Very Flexible Wings
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Emilio Santos
Airbus Defence and Space
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170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project
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Roberto Sbarra
Università of Rome “La Sapienza”
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65 Experimental investigation of a highly flexible wing
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Thomas G. Schmidt
German Aerospace Center (DLR), Institute of Aeroelasticity
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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
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Thomas Schmidt
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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
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Jean-Sébastien Schotté
ONERA
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150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
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Simon Schulz
DLR - German Aerospace Center
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109 Decentralized Control of Ailerons for Gust Load Alleviation
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Matthias Schulze
DLR – Institute of Aeroelasticity, Bunsenstrasse 10, 37073 Goettingen, Germany
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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
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Jan Schwochow
DLR
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119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
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Andrea Sciacchitano
Delft University of Technology
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101 Integrated Aerodynamic and Structural Measurements of the Gust Response of a Hinged Folding Wingtip
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Carlos Sebastia Saez
Chair of Aircraft Design, Technical University of Munich
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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
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Thomas Seren
Technical University of Munich
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116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
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Alan Serena
Airbus De
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170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project
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Yali Shao
Beihang University
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83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
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Tanuj Sharma
School of Civil, Aerospace and Design Engineering, University of Bristol
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208 Experimental investigation into the dynamic characteristics of a tilting multirotor system
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Bilal Sharqi
University of Michigan
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79 Finite element model update of a very flexible wing using ground vibration testing data
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Junlin Shen
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240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
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Pengtao Shi
NPU
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210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
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SangJoon Shin
Seoul National University
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135 Machine learning-based parametric model order reduction for the gust load analysis
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Roberto da Silva
Aeronautics Institute of Technology - ITA
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70 Application of Shape Memory Alloys for Flutter Suppression in a Propeller-Driven Typical Section
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Felipe da Silva
Embraer
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70 Application of Shape Memory Alloys for Flutter Suppression in a Propeller-Driven Typical Section
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Roberto Silva
Instituto Tecnológico de Aeronáutica (ITA)
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226 Comparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating wing
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Gefferson Silva
Technische Universität Berlin
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59 Aeroelastic analysis of a smart SMA-composite wing
195 On the preparation of a flexible real-time aircraft model for a flight simulator
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Flávio J. Silvestre
TU-Berlin
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58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
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Flavio Silvestre
Technische Universität Berlin
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59 Aeroelastic analysis of a smart SMA-composite wing
195 On the preparation of a flexible real-time aircraft model for a flight simulator
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Flávio José Silvestre
Technische Universität Berlin
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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
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Flávio Silvestre
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149 Constrained flexible wing with folding wingtip dynamics model based on Lagrange's method
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Magan Singh
Indian Institute of Science
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176 Transonic shock oscillations in an oscillating finite span wing
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Kautuk Sinha
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142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction
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Tomas Sinnige
Delft University of Technology
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174 Aeroelastic tailoring of dual-role propellers
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Julian Sinske
DLR-Institute of Aeroelasticity
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113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter
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Federica Siotto
Airbus UK
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26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
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Jayant Sirohi
The University of Texas at Austin
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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
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Miroslav Smid
Czech Aerospace Research Centre (VZLU)
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56 New Design of Whirl Flutter Aeroelastic Demonstrator
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Hollis Smith
Air Force Research Laboratory
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138 A Panel-Free Aeroelastic Solver with Adjoint Sensitivities
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Keith Soal
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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
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Breno Soares da Costa Vieira
Instituto Tecnológico de Aeronáutica
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132 Surrogate Modeling of Highly Flexible Structures and Aerodynamics Using Neural Networks
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Jurij Sodja
Delft University of Technology
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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
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Chen Song
Beihang University
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93 Gust response analysis of supersonic aircraft based on three-dimensional piston theory
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Leonardo Soria
Politecnico di Bari
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199 Application of the unsteady compressible source and doublet panel method to flutter calculations
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Aleli Sosa Chavez
Siemens Digital Industry Software NV
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225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
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Abraão Ferreira de Sousa Neto
Instituto Tecnológico de Aeronáutica
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222 Identification of Flexible Aircraft Parameters with Varying Flexibility Configurations: Integrating Elastic Effects and Sensor Data
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Cleber Spode
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186 Nonlinear analysis of a flexible half-wing model tested in a subsonic wind tunnel with control-surface freeplay and preloading
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Felix Stalla
German Aerospace Center (DLR), Institute of System Dynamics and Control
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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
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Bret Stanford
NASA LaRC
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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
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Jan Starek
Czech Aerospace Research Centre (VZLU)
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56 New Design of Whirl Flutter Aeroelastic Demonstrator
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Nichoas Stathopoulos
L3Harris
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73 Testing and Analysis of a Simplified Nonlinear Horizontal Stabilator of an Aircraft
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Gerrit Sybe Stavorinus
Technische Universität Berlin
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98 Influence of nonlinear aerodynamic effects on high aspect ratio aircraft model
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Gerrit Stavorinus
TU-Berlin
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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
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Cyrille Stephan
ONERA
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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
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Bernd Stickan
Airbus Operations GmbH
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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
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Kilian Streitenberger
Institute of Aeroelasticity - German Aerospace Center (DLR)
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214 Investigation of vortex-induced vibrations to compare Reynolds-averaged Navier-Stokes and detached-eddy simulations
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Till Strothteicher
DLR
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191 Automated Tuning of a Baseline Flight Control System with Maneuver Load Alleviation for an Energy-Efficient Passenger Airplane
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Vitalii Sukhov
National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”
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235 Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
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Afzal Suleman
University of Victoria
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237 Topology Optimization of Aeroelastically Scaled Wing Models based on Additive Manufacturing
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Zhan Sun
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84 Aerothermoelasticity analysis of hypersonic vehicle based on meshfree method
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Xiaoyang Sun
Airbus UK
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26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
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Özge Süelözgen
Research Scientist, DLR (German Aerospace Center)
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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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