“…In the present paper, a rather simple configuration is considered: a single airfoil, between two end plates, with a clearance at the lower end. This simplicity enabled Jacob et al [6,7] to carry out a detailed experimental characterization, on both aerodynamics and acoustics. A zonal large-eddy simulation was also performed on the same configuration and compared very favorably to the experiment, as shown by Boudet et al [8,9] on mean flow, Reynolds stresses, and spectra.…”