External Flow Over an Aircraft Wing (aircraft_2m) 2019 R1

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
 

Results

Results are listed alphabetically by platform. Download

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%

Contattaci

* = Required Field

Thank you for reaching out!

We’re here to answer your questions and look forward to speaking with you. A member of our Ansys sales team will contact you shortly.