Reference : Aeroelastic and Structural Design of an All-Moveable Aircraft Fin
Scientific congresses and symposiums : Paper published in a book
Engineering, computing & technology : Aerospace & aeronautics engineering
http://hdl.handle.net/2268/25504
Aeroelastic and Structural Design of an All-Moveable Aircraft Fin
English
Cooper, J. E. [University of Manchester > School of Engineering > > >]
Bureerat, S. [University of Manchester > School of Engineering > > >]
Sensberg, O. [University of Manchester > School of Engineering > > >]
Dimitriadis, Grigorios mailto [Université de Liège - ULiège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale >]
Jun-2001
Proceedings of the CEAS Conference on Multidisciplinary Aircraft Design and Optimization
Hönlinger, Heinz
177-184
No
No
International
CEAS Conference on Multidisciplinary Aircraft Design and Optimization
du 25 juin 2001 au 26 juin 2001
CEAS Council of European Aerospace Societies
Cologne
Germany
[en] Multi-Disciplinary Design Optimisation ; All-movable aircraft fin ; Control effectiveness
[en] The Lagrange Multi-Disciplinary Design Optimisation (MDO) code is used for the preliminary
study into design aspects of a generic all-movable aircraft fin. It is shown how the control
effectiveness at high speeds can be increased through variation of the attachment position and
stiffness, whilst still meeting strength and aeroelastic stability constraints.
Researchers ; Professionals
http://hdl.handle.net/2268/25504

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