Aeroelasticity & Structural Dynamics in a Fast Changing World
17 – 21 June 2024, The Hague, The Netherlands
Home Program Author Index Search

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
Dor Naftaly
78 Flight-dynamics aeroelastic coupling in flexible and very flexible wings
Mihaly Nagy
HUN-REN SZTAKI
116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
Misi Nagy
SZTAKI
119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
Eisuke Nakagawa
University of Tokyo
85 Elastic wind tunnel model design via eigenvector-based level-set topology optimization
Venkateswaran Narayanaswamy
North Carolina State University
81 Limit Cycle Oscillation of a Plate with Piezoelectric Elements in Supersonic Flow
Jan Navrátil
Brno University of Technology - FME - Institute of Aerospace Engineering
133 Unified model of sandwich panel core and faces for aeroelastic optimization
Andrew Neely
UNSW Canberra
187 Hot-wall shock-wave boundary layer interaction of a compliant cantilever in hypersonic flow
Doug Neill
ICME Design
12 Including Gradient-based Transient Gust Optimization in ASTROS
Renata Nepumoceno-Merce
Airbus Helicopters
215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
Jens Neumann
DLR
66 Design of flutter suppression controllers for a wing in compressible flow based on high-fidelity aerodynamics
159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Bing Feng Ng
108 Wind tunnel experiment for body freedom flutter of flying wing unmanned aerial vehicle
Jens Nitzsche
DLR, Institute of Aeroelasticity
112 A general solver for the prediction of flutter and buffet onset
214 Investigation of vortex-induced vibrations to compare Reynolds-averaged Navier-Stokes and detached-eddy simulations
123 Analysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver
Julia Noël
Airbus Operations
50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft

[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]