Authors Index

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [Q] [R] [S] [T] [V] [W] [X] [Y] [Z]

Author	Manuscripts
Eric Rantet Aviation Design	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Daniella E. Raveh	78 Flight-dynamics aeroelastic coupling in flexible and very flexible wings 110 Estimation of slender body elastic rates and accelerations using a combination of measured data
Bruno Regina Instituto Tecnológico de Aeronáutica (ITA)	226 Comparison between computational and experimental non-stationary pressure distribution on a pitch-oscilating wing
Lars Reimer DLR Institute of Aerodynamics and Flow Technology	141 Assessment of Active Load Control Approaches for Transport Aircraft – Simulation and Wind Tunnel Test
Manuel Reyes Airbus Defence and Space	171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Djamel Rezgui	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? 208 Experimental investigation into the dynamic characteristics of a tilting multirotor system 129 Aeroelastic analysis of distributed electric propulsion flexible wings
Sergio Ricci Politecnico di Milano	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration 231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Luca Riccobene Politecnico di Milano	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
Leif Rieck Hamburg University of Technology	46 Doublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters
Marcello Righi ZHAW and ETHZ	65 Experimental investigation of a highly flexible wing
Antoine Riols-Fonclare ONERA/DAAA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA
Cristina Riso Georgia Institute of Technology	35 Evaluation of Aeroelastic Models for Gust Response Prediction in Very Flexible Wings
Markus Ritter German Aerospace Center (DLR), Institute of Aeroelasticity	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft 106 Design and Experimental Characterization of a Gust-Generator Concept with Rotating-Slotted Cylinders in the Low-Speed Wind Tunnel DNW-NWB 107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
Andrea Da Ronch University of Southampton	168 Model order reduction for nonlinear aeroelastic dynamical system using automatic differentiation
Carlo Rotundo Delft University of Technology	174 Aeroelastic tailoring of dual-role propellers
Serena Russo DREAM INNOVATION	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [Q] [R] [S] [T] [V] [W] [X] [Y] [Z]