Session: Self-excited vibrations
SEV1 - Monday 20 September, 2010
| 16:20 | Application of PVDF foils for the measurements
of unsteady pressures on wind tunnel models for the prediction of
aircraft vibrations (ID 382) Wolfgang Luber, J. Becker, AEDS-MAS (Military Air System), Germany |
|
| 16:45 | Damping identification in an non-linear
aeroelastic structure (ID 127) Gareth Vio, Marco Prandina, University of Liverpool, United Kingdom Grigorios Dimitriadis, University of Liège, Belgium |
|
| 17:10 | Effect of damping on the propensity of squeal
instability: A numerical investigation (ID 18) Francesco Cantone, Francesco Massi, INSA Lyon, France |
|
| 17:35 | Bifurcation analysis of an airfoil undergoing
plunge stall flutter oscillations in a wind tunnel (ID
307) Norizham Abdul Razak, Universite of Liège, Belgium Thomas Andrianne, Grigorios Dimitriadis, University of Liège, Belgium |
|
| 18:00 | Flight Flutter Testing and Clearance of the
baseline Configuration of a Developmental Combat Aircraft (ID
321) R.V. Vaidyanathan, Aeronautical Development Agency, India E. Hemalatha, Aeronautical Developement Agency, India |
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