Reference : Online Flight Flutter Testing
Scientific congresses and symposiums : Paper published in a book
Engineering, computing & technology : Aerospace & aeronautics engineering
http://hdl.handle.net/2268/24706
Online Flight Flutter Testing
English
Dimitriadis, Grigorios mailto [Université de Liège - ULiège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale >]
Cooper, Jonathan E [University of Manchester > School of Engineering > > >]
Sep-2001
Proceedings of the International Conference on Structural System Identification
Link, M.
Universitätsbibliothek Kassel
583-592
No
No
International
3-89792-055-7
Kassel
Germany
International Conference on Structural System Identification
du 5 septembre 2001 au 7 septembre 2001
COST F3, Universität Gesamthochschule Kassel
Kassel
Germany
[en] Aeroelasticity ; Flight Flutter Testing ; System identification ; On-line Identification Methods ; Time-Frequency Methods
[en] A number of different identification methods are considered as candidate
approaches to undertake online flight flutter testing. Rather than flying the test aircraft to a
new flight condition and then performing a data analysis at a constant flight condition, it is
shown how it is feasible to track changes in frequencies and damping ratios as the flight
speed is increased. It is also possible to provide an updated estimate of the predicted flutter
speed, giving the flight engineers added confidence in the margin of safety. Both frequency
and time domain methods are evaluated on a simulated 3 DOF aeroelastic system. These
preliminary results show that such an approach is feasible although further work is required
to determine the best testing and analysis approach.
Researchers ; Professionals
http://hdl.handle.net/2268/24706

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