Authors Index

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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
Ruslan Nikitin National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”	235 Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
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
Salvatore Nocerino Leoanrdo	95 Ground resonance test and aeroelastic model validation of an innovative regional aircraft fitted with innovative wing tip (IWT) and adaptive morphing winglet (AMW)
Julia Noël Airbus Operations	50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft

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