D. Antonelli - Cordoba National University, Cordoba, Cordoba, ۵۰۰۰, Argentina
C. Sacco - Aeronautical University Institute, Cordoba, Cordoba, ۵۰۰۰, Argentina
J. Tamagno - Cordoba National University, Cordoba, Cordoba, ۵۰۰۰, Argentina

Numerical simulations of flow patterns at ultra-low Reynolds numbers over rigid and flexible airfoils are presented, and the influence of flexibility on main aerodynamic properties are discussed. Typical unsteady flights like heaving and flapping are, in terms of Reynolds and Strouhal numbers, reduced frequencies and FSI (Fluid Structure Interaction) factor, are valuated. It has been found that for some flexibility levels, the aerodynamic forces and propulsive efficiency are enhanced if compared with a rigid airfoil. The mathematical technical approach used to solve the laminar-incompressible flow equations coupled with structural algorithms, is described.

Aerodynamic wing sections, CFD, Fluid structure interaction, Low Reynolds, Flexible airfoil, Unsteady flows, Partitioned method, Finite element method