Laboratory of Thermodynamics and Energy Systems, Faculty of Physics, University of Science and Technology Houari Boumediene (USTHB), BP 32 El-Alia, Algiers, Algeria
Laboratory of Fluid Mechanics, Ecole Militaire Polytechnique, Bordj El Bahri 16046, Algiers, Algeria
Centre de Développement des Energies Renouvelables, CDER, B.P 62 Route de l’Observatoire, 16340 Bouzaréah, Algiers, Algeria
Arts et Métiers ParisTech, LMFL, 8 boulevard Louis XIV, 59046 Lille, France
Virginia Tech, Kevin T. Crofton, Dept. of Aerospace & Ocean Eng., Blacksburg, 460 Old Turner Street,
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.