Author |
Manuscripts |
Yasser M. Meddaikar
DLR - Institute of Aeroelasticity
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99 Flexible aircraft conceptual co-design based on the RCE framework
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Liang Ma
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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
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Xiaoping Ma
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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
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Terence Macquart
University of Bristol
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31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
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Holger Mai
German Aerospace Center (DLR) - Institute of Aeroelasticity
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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
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Jyoti Majhi
Indian Institute of Science
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175 Prediction of transonic buffet in an axial flow fan using global stability analysis
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Vadim Maltsev
University of Southampton
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61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
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William Mansey
University of Bristol
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125 Active flutter suppression and gust load alleviation of wings incorporating floating wingtips
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Paolo Mantegazza
Politecnico di Milano
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192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
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Luca Marchetti
Politecnico di Milano
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192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
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Luca Marino
TU Delft
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183 Nonlinear analysis of combined rate and acceleration limits effect on actuator performance
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Sylvie Marquier
Airbus Operations SAS
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25 Control surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria
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Pier Marzocca
RMIT University Melbourne
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89 The Effect of Aerodynamic Interactions on Aeroelastic Stability in Wing-Propeller Systems
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Paolo Mastracci
Airbus UK
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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
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Franco Mastroddi
Sapienza University of Rome
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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
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Davide Mastrodicasa
Siemens Digital Industry Software NV
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225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
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Kevin McHugh
United States Air Force Research Laboratory
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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
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Yasser Meddaikar
DLR
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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
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David Meier
DLR - German Aerospace Center
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215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
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Tobias Meier
DLR - German Aerospace Center
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215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
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Ana Cristine Meinicke
University of Michigan
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185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
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Ana C. Meinicke
University of Michigan
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105 Investigation on Sensor Selection Applied on a Vehicle-as-a-Sensor Concept in High-Speed Flight
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Eduardo de Melo Pinto
Instituto Tecnológico de Aeronáutica
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117 Comparative analysis of flight maneuver loads between flexible and rigid aircraft
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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
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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
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Kolja Michel
German Aerospace Center (DLR), Institute of System Dynamics and Control
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109 Decentralized Control of Ailerons for Gust Load Alleviation
107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
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Boris Micheli
DLR Institut für Aeroelastik
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66 Design of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics
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Francesco M. A. Mitrotta
University of Bristol
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31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
|
Amir Hossein Modarres Aval
University of Southampton
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61 Investigation of multibody flight dynamic modes of an aircraft with flexible folding wing tips
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Eduardo Molina
Embraer S.A.
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226 Comparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating wing
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Charly Mollet
ONERA/DAAA
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162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
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Reza Moosavi
University of Hertfordshire, UK
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139 Aeroelasticity of smart wing in supersonic flow
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Joseph Morlier
ISAE-Supaero
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25 Control surface sizing and design through integrated MDO approach: Enhancing load alleviation while preserving handling quality criteria
|
Breno Moura Castro
Embraer S.A.
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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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Daniel Muradas Odriozola
Airbus Operations SAS
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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
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Thulasi Mylvaganam
Imperial College London
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29 Modelling complex actuator and sensor architectures for gust alleviation systems of flexible aircraft
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Martin Müller
|
202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
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Florian Müller
German Aerospace Center (DLR)
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90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
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