External flow over an aircraft wing. The case has around 2 million hexahedral cells and uses the realizable K-e Turbulence model and the coupled implicit solver.
| Number of cells | 2 million |
| Cell type | hexahedral |
| Models | realizable k-eps turbulence |
| Solver | Pressure based coupled solver, Green Gauss Node based, steady |
Last updated: 2019-11-22
| Platform | Cores | Machines | Core Solver Rating | Core Solver Speedup | Core Solver Efficiency |
Intel white box, Xeon 8260L, 48 cores, 2.4 GHz, Omni-Path, using Fluent AVX2 binary
| 48
| 1
| 6400.0000
| 48.000
| 100.00%
|
96
| 2
| 12943.8202
| 97.079
| 101.12%
| |
192
| 4
| 24510.6383
| 183.830
| 95.74%
| |
384
| 8
| 41638.5542
| 312.289
| 81.33%
| |
768
| 16
| 65207.5472
| 489.057
| 63.68%
| |
| 1152 | 24 | 69120.0000 | 518.400 | 45.00% |
