Research Article
Transition Effect on the Flow Dynamics in a Compressor Blade Passage
Table 4
RMS of average shock oscillations and shock amplitude for flow cases with roughness.
| Flow case | A (mm) | RMS (mm) |
| Ref-laminar | 4.37 | 1.21 | X/C = 0.11, Ra = 8 | 4.84 | 1.33 | X/C = 0.11, Ra = 10 | 3.96 | 1.04 | X/C = 0.11, Ra = 12 | 4.84 | 1.07 | X/C = 0.16, Ra = 12 | 4.71 | 1.54 | X/C = 0.16, Ra = 16 | 5.04 | 1.52 | X/C = 0.16, Ra = 20 | 4.45 | 1.20 | X/C = 0.21, Ra = 12 | 5.48 | 1.57 | X/C = 0.21, Ra = 16 | 6.28 | 1.85 | X/C = 0.21, Ra = 20 | 4.63 | 1.24 |
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