Author |
Manuscripts |
Stephan Adden
IBK Innovation
|
192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
|
Frederico Afonso
Instituto Superior Tecnico
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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-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 Bleecke
Airbus Operations
|
50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft
|
Hans Martin Bleecke
Airbus Operations
|
30 Machine learning to forecast unsteady, motion-induced unsteady forces
|
Brianna Blocher
The University of Texas at Austin
|
185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
|
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
|
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
|
Roeland de Breuker
Delft University of Technology
|
198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
|
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
|
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
|
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
|
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 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
|
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
|
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 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
|
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
|
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
|
Zhiying Chen
|
87 An integrated static/dynamic aerothermoelastic analysis framework for functionally graded structures in hypersonic vehicles
|
Song Chen
|
136 The Design and Analysis of Tensegrity Morphing Wing
|
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 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
|
Jonathan E. Cooper
University of Bristol
|
31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
|
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
|
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
|
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
|
215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
|
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 José González
Technische Universität Berlin
|
42 Aeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study
|
Pedro J. González
TU-Berlin
|
58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
|
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 M. Kier
German Aerospace Center (DLR), Institute of System Dynamics and Control
|
107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible 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
|
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
|
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
|
Gongde Li
|
240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
|
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
|
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
|
Zhuoneng Li
University of Southampton
|
61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
|
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
|
Cédric Liauzun
ONERA/DAAA
|
162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
|
Cedric Liauzun
ONERA
|
34 A modular TSM solver for aeroelastic analysis and optimizations
|
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
|
Yi Liu
Institute of Beijing Mechanics and Electronics
|
5 The simulation and flight verification of active aeroelastic control
|
Dawei Liu
|
11 Wind tunnel test of gust response for distributed propeller-wing system
|
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
|
David Meier
DLR - German Aerospace Center
|
215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
|
Tobias Meier
DLR - German Aerospace Center
|
215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
|
Ana Cristine Meinicke
University of Michigan
|
185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
|
Ana C. Meinicke
University of Michigan
|
105 Investigation on Sensor Selection Applied on a Vehicle-as-a-Sensor Concept in High-Speed Flight
|
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
|
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
|
Mihaly Nagy
HUN-REN SZTAKI
|
116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
|
Misi Nagy
SZTAKI
|
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
|
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
|
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
|
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
|
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 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
|
Martin TANG
DLR
|
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
|
Bela Takarics
SZTAKI
|
103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
|
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
|
Jun Kang Tan
|
108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
|
Martin Tang
German Aerospace Center (DLR), Institute of Aeroelasticity
|
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
|
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
|
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
|
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
|
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
|
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
|
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
|
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
|
Gaozhan Wang
Beihang University
|
92 Hypersonic flutter analysis based on three-dimensional local piston theory
|
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
|
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
|
Peihan Wang
Beihang University
|
45 Dynamic analysis of nonlinear aeroservoelasticity by a modified frequency-time domain method
|
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
|
Zhichun Yang
|
210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
|
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
|
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
|
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
|
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
|
Jian Zhang
|
39 Nonlinear Aeroelasticity Characteristics and Dynamics Response Analysis of Unmanned Multi-Body Aircraft
|
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
|
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
|
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
|
Markus Zimmer
German Aerospace Center (DLR)
|
90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
|