Research Article
Numerical Investigation of the Wake Vortex-Related Flow Mechanisms in Transonic Turbines
Table 2
Boundary conditions of research objects.
| Flow conditions | (K) | (Pa) | (degree) | (Pa) | |
| VKI LS89: MUR129 | 409.2 | 184900 | 0 | 116500 | 0.840 | VKI LS89: MUR235 | 413.3 | 182800 | 0 | 104900 | 0.927 | CNRC: Mach 1 | 293.0 | 101300 | 0 | 67000 | 0.80 | CNRC: Mach 2 | 293.0 | 101300 | 0 | 54602 | 1.00 | CNRC: Mach 3 | 293.0 | 101300 | 0 | 43600 | 1.16 |
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