Author/Authors :
Boudis, A Laboratory of Thermodynamics and Energy Systems - Faculty of Physics - University of Science and Technology Houari Boumediene (USTHB), Algiers, Algeria , Benzaoui, A Laboratory of Thermodynamics and Energy Systems - Faculty of Physics - University of Science and Technology Houari Boumediene (USTHB), Algiers, Algeria , Oualli, H Laboratory of Fluid Mechanics - Ecole Militaire Polytechnique, Algiers, Algeria , Guerri, O Centre de Développement des Energies Renouvelables - CDER, Bouzaréah, Algiers, Algeria , Bayeul-Lainé, A. C Arts et Métiers ParisTech - LMFL, Lille, France , Coutier Delgosha, O Virginia Tech, Kevin T. Crofton - Dept. of Aerospace & Ocean Eng., Blacksburg, USA
Abstract :
In this study, numerical investigations on the energy extraction performance of a flapping foil device are
carried out by using a modified foil shape. The new foil shape is designed by combining the thick leading
edge of NACA0012 foil and the thin trailing edge of NACA0006 foil. The numerical simulations are based
on the solution of the unsteady and incompressible Navier-Stokes equations that govern the fluid flow around
the flapping foil. These equations are resolved in a two-dimensional domain with a dynamic mesh technique
using the CFD software ANSYS Fluent 16. A User Define Function (UDF) controls the imposed sinusoidal
heaving and pitching motions. First, for a validation study, numerical simulations are performed for a
NACA0012 foil undergoing imposed heaving and pitching motions at a low Reynolds number. The obtained
results are in good agreement with numerical and experimental data available in the literature. Thereafter, the
computations are applied for the new foil shape. The influences of the connecting area location between the
leading and trailing segments, the Strouhal number and the effective angle of attack on the energy extraction
performance are investigated at low Reynolds number (Re = 10 000). Then, the new foil shape performance
was compared to those of both NACA0006 and NACA0012 baseline foils. The results have shown that the
proposed foil shape achieves higher performance compared to the baseline NACA foils. Moreover, the energy
extraction efficiency was improved by 30.60% compared to NACA0006 and by 17.32% compared to
NACA0012. The analysis of the flow field around the flapping foils indicates a change of the vortex structure
and the pressure distribution near the trailing edge of the combined foil compared to the baseline foils.
Keywords :
CFD , Combined foil , Power coefficient , Energy extraction , Flapping foil