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
Stephan Adden IBK Innovation	192 Gust load alleviation wind tunnel tests of a folding wing tip configuration
Frederico Afonso Instituto Superior Tecnico	237 Topology Optimization of Aeroelastically Scaled Wing Models based on Additive Manufacturing
Majid Ahmadi	14 Gust load alleviation efficiency in an optimized composite wing through the integration of wingtip devices: Incorporating folding and twist strategies 15 Optimizing high aspect ratio composite wings through geometrically nonlinear aeroelastic tailoring
Rafic Ajaj Khalifa University	145 Gust load alleviation of electric aircraft with distributed propulsors using thrust vectoring 100 On the aeroelasticity of high aspect ratio strut-braced wings: A parametric study
Farbod Alijani	142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction
Hamad Almarzooqi Khalifa University	100 On the aeroelasticity of high aspect ratio strut-braced wings: A parametric study
Anna Altkuckatz German Aerospace Center (DLR) - Institute of Aeroelasticity	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
Muhittin-Nami Altug Airbus Helicopters	215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
Xavier Amandolese CNAM	160 Design and experimental tests of a flexible wing of high-aspect ratio for investigating flutter mechanisms
Mohammadreza Amoozgar	145 Gust load alleviation of electric aircraft with distributed propulsors using thrust vectoring
Chao An	92 Hypersonic flutter analysis based on three-dimensional local piston theory 83 Reduced order modeling analysis for flexible wing using a co-rotational beam element
Hao Wei, Elijah Ang	108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Carlo Aquilini Airbus Defence & Space GmbH	47 From Multivariate Random Loads To Deterministic Load Distributions: An Exact Method For Aeroelastic Design 44 Robust design through identification of main components from multivariate random loads
Felix Arevalo 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
Jürgen Arnold DLR Institut für Aeroelastik	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft 66 Design of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics

[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]