Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
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Authors Index

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Author Manuscripts
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

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