Authors Index

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Author	Manuscripts
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

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