Authors Index

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Author	Manuscripts
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
Guo Li Chinese Academy of Aerospace Aerodynamics	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
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
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
Jinying Li	32 Stall flutter suppression with active camber morphing based on reinforcement learning
Zhuoneng Li University of Southampton	61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
Gongde Li	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Cedric Liauzun ONERA	34 A modular TSM solver for aeroelastic analysis and optimizations
Cédric Liauzun ONERA/DAAA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
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

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