Authors Index

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Author	Manuscripts
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

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