Authors Index

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Author	Manuscripts
Alberto Gallego Pozo Universidad Carlos III of Madrid	182 Flight dynamic-aeroelastic response of highly flexible aircraft with distributed propellers
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 J. González TU-Berlin	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Pedro José González Technische Universität Berlin	42 Aeroservoelastic Analysis and Load Alleviation Control for Very Flexible Aircraft: TU-Flex Study
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
Yingsong Gu NPU	210 Body freedom flutter of scaled vehicles: From blended wing body to conventional configuration
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?
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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