External Flow Over an Aircraft Wing (aircraft_14m)
External Flow over aircraft wing. The case has around 14 million hexahedral cells and uses the realizable K-e Turbulence model and the Pressure based coupled solver, Least Squares cell based, steady solver.
| Number of cells | 14,000,000 |
| Cell type | Hexahedral |
| Models | Realizable K-e Turbulence |
| Solver | Pressure based coupled solver, Least Squares cell 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
|
799.4448
|
48.000
|
100.00%
|
|
96
|
2
|
1600.7411
|
96.111
|
100.12%
|
|
|
192
|
4
|
3197.0398
|
191.956
|
99.98%
|
|
|
384
|
8
|
6620.6897
|
397.517
|
103.52%
|
|
|
768
|
16
|
13447.4708
|
807.409
|
105.13%
|
|
| 1152 | 24 | 19415.7303 | 1165.753 | 101.19% | |
| 1536 | 32 | 22153.8462 | 1330.154 | 86.60% | |
| 2304 | 48 | 34217.8218 | 2054.495 | 89.17% | |
| 4608 | 96 | 44883.1169 | 2694.857 | 58.48% | |
| 6144 | 128 | 53169.2308 | 3192.369 | 51.96% |
