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% |
