A recent consideration in aircraft design is the use of folding wingtips, 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 wingtips on the aircraft flight dynamics. It is found that a floating wingtip aircraft has similar handling qualities with respect to an aircraft with no wing extension.
Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device
Journal of Aircraft ; 57 , 2 ; 333-341
2020-03-01
Article (Journal)
Electronic Resource
English
Applied Helicopter Aeroelastics - Modelling and Testing
British Library Conference Proceedings | 1996
|Applied helicopter aeroelastics : modelling and testing
TIBKAT | 1996
|