Release 13.0 Test Cases Benchmarks - External Flow Over an Aircraft Wing


External flow over an aircraft wing. The case has around 1.8 million hexahedral cells and uses the realizable k-epsilon model and the coupled implicit solver.

Number of cells 1,800,000
Cell type hexahedral
Models realizable k-eps turbulence
Solver coupled implicit

Plots


Results

Results are listed alphabetically by platform. Download

Last updated: 2011-12-01

 

Platform Cores Machines Core Solver
Rating
Core Solver
Speedup
Core Solver
Efficiency
cisco-ucs_c200-intel_x5670,2930,rhel55,10gige

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12
1
1060.8
N/A
N/A
24
2
2080.7
N/A
N/A
48
4
3940.7
N/A
N/A
96
8
6620.7
N/A
N/A
192
16
9653.6
N/A
N/A
384
32
8150.9
N/A
N/A
ibm-dx360_M3-intel_x5670,2930,rhel55,ib,qlogic,qdr

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12
1
1061.4
N/A
N/A
24
2
2084.4
N/A
N/A
48
4
3954.2
N/A
N/A
96
8
7291.1
N/A
N/A
192
16
11443.7
N/A
N/A
ibm-dx360_M3-intel_x5670,2930,rhel61,ib,mellanox,qdr

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12
1
1079.3
N/A
N/A
24
2
2121.5
N/A
N/A
48
4
4046.8
N/A
N/A
96
8
7464.4
N/A
N/A
192
16
11715.3
N/A
N/A
384
32
10666.7
N/A
N/A
sgi-altix_ice_8400-amd_6180,2500,sles11,ib,qdr

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1
1
82.2
1.0
100%
2
1
148.6
1.8
90%
4
1
256.2
3.1
78%
8
1
451.9
5.5
69%
12
1
659.4
8.0
67%
24
1
1209.7
14.7
61%
48
2
2435.5
29.6
62%
96
4
3034.2
36.9
38%
192
8
6697.7
81.5
42%
sgi-altix_ice_8400ex-intel_x5690,3470,sles11,ib

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1
1
157.1
1.0
100%
2
1
305.7
1.9
97%
4
1
539.4
3.4
86%
8
1
838.6
5.3
67%
12
1
1119.5
7.1
59%
24
2
2204.1
14.0
58%
48
4
4214.6
26.8
56%
96
8
7260.5
46.2
48%
192
16
11294.1
71.9
37%
sgi-uv_1000-intel_e7_8837,2670,sles11,numalink5

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1
1
98.0
1.0
100%
2
1
187.3
1.9
96%
4
1
341.8
3.5
87%
8
1
614.2
6.3
78%
16
1
1162.1
11.9
74%
32
1
2308.6
23.6
74%
64
1
3445.7
35.2
55%
128
1
4874.5
49.7
39%
256
1
11006.4
112.3
44%