25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-10.2.4


NON LINEAR AEROELASTIC BEHAVIOR OF HIGHLY FLEXIBLE HALE WINGS

G. Romeo, G. Frulla, E. Cestino, P. Marzocca*
Politecnico di Torino, Italy; *Clarkson University NY

Keywords: HALE Flutter Behaviour, Non-Linear Aeroelasticity, Limit Cycle Oscillations

A time simulation of a nonlinear aeroelastic model is proposed as a design/diagnostic analysis tool for highly flexible HALE aircrafts. Large structure deformations and static and dynamic aeroelastic responses are accounted for. Analytical, computational results are presented along with experiments on a high aspect-ratio wing model.


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