“…The polar curves ( C L = C L ( , Re L ) , and C D = C D ( , Re L ) ) as a function of attack angle, , and local Reynolds number, Re L , are computed employed the XFOIL tool at the low Reynolds number ( ∼ 10 4 ) for the model, and high Reynolds number ( ∼ 10 6 ) for full-size prototype turbine. In order to compute the local Reynolds number in each blade section, it is necessary to calculate the rotational velocity of the rotor, the tangential velocity in the blade radial position and the induction factors, involving polar curves, in an iterative process [8,9]. The BEM method applied to a rotor geometry under specific operating conditions can estimate, beside hydrodynamical forces and moments, the power coefficient as in Eq.…”