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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.

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This page is a summary of: Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device, Journal of Aircraft, March 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035602.
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