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| = Delta Wing 50k Complexity (Scitech 2018) = | | <span id="Contents"></span> |
| | = Data = |
| | [[Internal:Adaptive CDT3D Results | Adaptive CDT3D Results ]] |
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| [[File:Delta_wing_50k_parallel_scitech.png| 500px]]
| | = Integration with SU2 = |
| ==Preliminary data ==
| | * SU2 + refine + CDT3D pipeline [http://www.cs.odu.edu/crtc/SU2/SU2_pipeline.svg] |
| {| class="wikitable" style="text-align: right;"
| | * SU2 + refine + CDT3D, ONERAM6 invicid [http://www.cs.odu.edu/crtc/SU2/onera_invicid.pdf] |
| |+ All time data are given in seconds.
| |
| ! rowspan="2" | # Threads
| |
| ! rowspan="2" | # Tetrahedra
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| ! rowspan="2" | # Vertices
| |
| ! rowspan="2" | Intitialize Bg Mesh
| |
| ! rowspan="2" | Boundary Adaptation (MMGS)
| |
| ! rowspan="2" | Boundary Recovery
| |
| ! colspan="6" style="text-align: center;" | Mesh Refinement
| |
| ! rowspan="2" | Total Time
| |
| (without MMGS)
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| ! rowspan="2" | Memory (GB)
| |
| |-
| |
| ! # Iterations
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| ! Par. Deactivation
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| ! Par. Vertex Creation
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| ! Vertex Insertion
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| ! Partition
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| ! Par. Reconnection
| |
| |-
| |
| | 12
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| | 363278
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| | 63198
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| | 1.41
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| | 6.27
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| | 0.33
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| | 22
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| | 0.32
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| | 1.55
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| | 0.11
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| | 1.62
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| | 8.24
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| | 19.99
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| | 0.86
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| |-
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| | 24
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| | 363756
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| | 63270
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| | 1.49
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| | 6.26
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| | 0.33
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| | 22
| |
| | 0.2
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| | 0.88
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| | 0.11
| |
| | 1.6
| |
| | 5.13
| |
| | 16.15
| |
| | 1.31
| |
| |}
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| |
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| == Notes ==
| | * SU2 + refine + CDT3D, steady laminar flow low mach number over delta wing |
| * according to Mike's email mesh should be around 100k vertices | | ** meshes [http://www.cs.odu.edu/crtc/SU2/delta_wing.pdf] |
| * Metric Input Data available at [https://github.com/UGAWG/parallel-adapt-results/tree/master/delta-wing/fun3d-fv-lp2 https://github.com/UGAWG/parallel-adapt-results ] | | ** solution cuts of the vortex [http://www.cs.odu.edu/crtc/SU2/delta_vortex.pdf] |
| * Input surface is the coase mesh available at [https://github.com/UGAWG/solution-adapt-cases/delta-wing/initial-grid/delta01.meshb https://github.com/UGAWG/solution-adapt-cases] | | ** video [http://www.cs.odu.edu/crtc/SU2/delta_wing_005.ogv] |
| * The experiments performed on a DELL workstation with Linux Red Hat Enterprise, 24 hardware cores Intel® Xeon® CPU E5-2697v2@2.70 GHz, and 757 GB RAM
| | |
| * Memory is measured at the end of Mesh refinement and thus it may reach a slightly higher value before the point of measurement
| | = Improvements = |
| * parameters <code> --brec=2 --met=1 --meval=3 --mrecm2=1 --mrec4=1 --nadapt=2 --malign=0 --mpp=2 --ndfs=0 --nthreads=$THREADS --nbuckets=20*$THREADS --nthreadsaf=20*$THREADS --nbucketsaf=20*${THREADS} --blockmul=500000 --nqual=0 --nminpts=30 --ordt=0 --pardeact=1 --mdse=0 </code>
| | [[Internal:Adaptive CDT3D - Smoothing | Metric Adaptive Smoothing ]] |
| | |
| | = General Notes = |
| | * [[Internal:ACDT3D_Quality_Criteria | Comparison for quality criteria for ACDT3D]] |
| | * [[Internal:ACDT3D_(Scitech2018)_stability_data | Stability Data for 500k]] |
| | [[#Contents | Back To Top]] |
Data
Adaptive CDT3D Results
Integration with SU2
- SU2 + refine + CDT3D pipeline [1]
- SU2 + refine + CDT3D, ONERAM6 invicid [2]
- SU2 + refine + CDT3D, steady laminar flow low mach number over delta wing
- meshes [3]
- solution cuts of the vortex [4]
- video [5]
Improvements
Metric Adaptive Smoothing
General Notes
Back To Top