SILVA NETO, O. T.; http://lattes.cnpq.br/8667252478624737; SILVA NETO, Orlando Tomaz da.
Résumé:
The search for increase in the performance of the aircraft has directed, among other things, to the increase of the aspect ratio of the wing and to the use of advanced materials; These solutions led to an increase of flexibility, resulting in aeroelastic problems - aeroelasticity is the science that studies the phenomena arising from the interactions between aerodynamic, elastic and inertial forces. In this area, we highlight the flutter, dynamic stability aeroelastic phenomenon. In this context, this work aims to analyze the behavior of a flexible wing with high aspect ratio with passive actuators of Shape Memory Alloys (SMA) in flutter, submitted to a subsonic flow. For this, the design, construction and testing of an aeroelastic model was carried out to be tested in a wind tunnel, the development of this prototype counted on a numerical-experimental approach; After finished model tests, the thermomechanical selection and characterization of the actuator was done; Finally, the tests were carried out in the wind tunnel. The results showed that, for certain arrangements of the actuators in the wing, the aeroelastic behavior underwent a very significant performance gain as, an increase of approximately 28% in the critical rate of flutter occurrence. With the results analysis, it was possible to conclude that a detailed study of the dynamic behavior of the actuators and of the effect of each arrangement of them on the structure must be carried out so that the desired effect may be achieved.
