Top: passage-averaged LES fields of the velocity magnitude in the plane (only radial and tangential components) at 77% of the diffuser span from the hub side for the design (a) and off-design (b) conditions, normalized using the tangential velocity of the impeller blades at their trailing edge, u2. Bottom: passage-averaged profiles of the velocity component, ut, tangential to the PS of blade 5 along the line f in Fig. 3 for the design (c) and the off-design (d) conditions (: experiments by Boccazzi et al. [26]; : present computations). The horizontal axis refers to the distance, xn, from the PS of blade 5, scaled by the local width of the diffuser channel, h.