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Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device
- 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.
- Subjects :
- Coupling
020301 aerospace & aeronautics
Lift-induced drag
business.industry
Computer science
Hinge
Aerospace Engineering
aeroelastic analysis
ComputerApplications_COMPUTERSINOTHERSYSTEMS
02 engineering and technology
Flight control surfaces
Aeroelasticity
01 natural sciences
GeneralLiterature_MISCELLANEOUS
Finite element method
010305 fluids & plasmas
folding wing tip
0203 mechanical engineering
Flight dynamics
0103 physical sciences
Aerospace engineering
business
ComputingMethodologies_COMPUTERGRAPHICS
Subjects
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