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@. Fig, Distribution of the local Nusselt number as a function of the local Reynolds number Re r = Re × (r/R ext ) 2 for Re = 5

@. Fig, Axial profiles of the mean radial and tangential velocity components and the corresponding Reynolds stress tensor components at r/R ext = 0.56 and Re = 1.04 × 10 6 in a shrouded rotor-stator cavity of aspect ratio G = 0.036: (a) C w = 0, ) C w = 9881. Comparisons between the present RSM (straight lines), a low-Reynolds number k ? ? model (dashed lines) and the LDV measurements (symbols) of Poncet, 1976.

@. Fig, 5: Streamline patterns obtained by the RSM, from (a) Test case 1 to (i) Test case 9

@. Fig, Streamline patterns obtained by the k ? ? SST, for Test cases (a) 4, (b) 5 and (c) 6

@. Fig, Normalized velocity vectors in the plane (x, y) for Test cases 1 (a,b) and 7 (c,d), in two planes, near the rotor

@. Fig, Radial variation of the core-swirl ratio ? for the 9 test cases: (a) test case 1 . . . (i) test case 9. Comparisons between the experiments (symbols), the RSM (solid black lines), the k-? SST model

@. Fig, Radial variation of the averaged mean radial velocity V r /V for Test case 5 and three axial positions: one near the rotor (z/e = 0.23), at mid-gap (z/e = 0.53) and one close to the stator (z/e = 0.84) Comparisons between the experiments (symbols), the RSM (dashed lines), the k ? ? SST (solid lines), the LDA measurements of Mingawa and Obi

@. Fig, 10: Maps of the turbulence kinetic energy k normalized by its maximum value for Test Case 4 (a,b), 5 (c,d) and 6 (e,f) obtained by the RSM (a,c,e) and the k ? ? SSt model (b,d,f)

@. Fig, Radial variation of three components of the Reynolds stress tensor for Test case 5 and at three axial positions: one near the rotor (z/e = 0.23), at mid-gap (z/e = 0.53) and one close to the stator (z/e = 0.84) Comparisons between the experiments (symbols), p.the RSM