Circulating fluidized bed (fluidized_bed_2m)

External flow over an aircraft wing. The case has around 2 million mixed cells and uses the Laminar, Eulerian Multiphase model and the Pressure based segregated solver, Least Squares cell based, unsteady solver.

Number of cells 2,000,000
Cell type Mixed
Models Laminar, Eulerian Multiphase
Solver Pressure based segregated solver, Least Squares cell based, unsteady

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Results

Results are listed alphabetically by platform. Download

Last updated: 2016-03-09
Platform Cores Machines Core Solver
Rating		 Core Solver
Speedup		 Core Solver
Efficiency
cray-xc40-intel_e5_2698v3,2300,cle52up04,sles11sp3,aries

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32
1
1811.3
N/A
N/A
64
2
3692.3
N/A
N/A
128
4
7480.5
N/A
N/A
256
8
14222.2
N/A
N/A
384
12
19525.4
N/A
N/A
512
16
23510.2
N/A
N/A
768
24
28800.0
N/A
N/A
hp_proliant_xl170r_gen9-intel_e5_2697v3,2600,rhel65,infiniband,fdr

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1
1
51.5
1.0
100%
2
1
107.8
2.1
105%
4
1
229.4
4.5
111%
6
1
344.9
6.7
112%
8
1
464.9
9.0
113%
10
1
586.0
11.4
114%
12
1
709.8
13.8
115%
14
1
813.0
15.8
113%
16
1
942.7
18.3
114%
18
1
1042.5
20.2
112%
20
1
1135.0
22.0
110%
22
1
1249.5
24.3
110%
24
1
1342.7
26.1
109%
26
1
1431.1
27.8
107%
28
1
1507.9
29.3
105%
56
2
2916.5
56.6
101%
112
4
5674.9
110.2
98%
224
8
9762.7
189.6
85%
448
16
14582.3
283.2
63%
896
32
16457.1
319.6
36%
3584
128
17194.0
333.9
9%