Back to Search Start Over

Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device

Authors :
Jonathan E. Cooper
Thomas Wilson
Andrea Castrichini
Franco Mastroddi
N. Viceconti
Francesco Saltari
Source :
Castrichini, A, Wilson, T, Salteri, F, Mastroddi,, F, Viceconti, N & Cooper, J E 2019, ' Aeroelastics Flight Dynamics Coupling Effects of the Semi Aeroelastic Hinge Device ', Journal of Aircraft . https://doi.org/10.2514/1.C035602
Publication Year :
2020
Publisher :
American Institute of Aeronautics and Astronautics (AIAA), 2020.

Abstract

A recent consideration in aircraft design is the use of folding wing-tips with the aim of enabling higher aspect ratio aircraft with less induced drag, but also meeting airport gate limitations. This study investigates the impact of floating folding wing-tips on the aircraft flight dynamics. It is found that a floating wing-tips aircraft has similar handling qualities with respect to an aircraft with no wing extension.

Details

ISSN :
15333868
Volume :
57
Database :
OpenAIRE
Journal :
Journal of Aircraft
Accession number :
edsair.doi.dedup.....c1596811fa350645038caa6a87a93306
Full Text :
https://doi.org/10.2514/1.c035602