Reference : Nonlinear dynamic analysis of an F-16 aircraft using GVT data
Scientific congresses and symposiums : Paper published in a book
Engineering, computing & technology : Aerospace & aeronautics engineering
http://hdl.handle.net/2268/151122
Nonlinear dynamic analysis of an F-16 aircraft using GVT data
English
Noël, Jean-Philippe mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux >]
Renson, Ludovic [Université de Liège - ULg > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux >]
Kerschen, Gaëtan [Université de Liège - ULg > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux >]
Peeters, Bart [LMS International > > > >]
Manzato, Simone [LMS International > > > >]
Debille, Jan [LMS International > > > >]
Jun-2013
Proceedings of the International Forum on Aeroelasticity and Structural Dynamics
No
No
International
International Forum on Aeroelasticity and Structural Dynamics
24 - 26 June 2013
Bristol
UK
[en] Characterisation of structural nonlinearities ; F-16 aircraft ; GVT data
[en] This paper aims at investigating the nonlinear dynamics of an F-16 aircraft, based upon sine-sweep data collected during a ground vibration test (GVT) campaign. Various analysis techniques, including the mere visual inspection of the time series, the wavelet transform and the restoring force surface method, are utilised and reveal that the F-16 wing-to-payload mounting interfaces exhibit both softening and hardening nonlinearities.
Fonds pour la formation à la Recherche dans l'Industrie et dans l'Agriculture (Communauté française de Belgique) - FRIA
Researchers ; Professionals ; Students
http://hdl.handle.net/2268/151122

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