Internal:Adaptive CDT3D Results: Difference between revisions

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BrainMapping, CNF, HPC, I2MConversion, NDAM, Segmentation, UltraSound3D, Bureaucrats, external, internal, Administrators
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BrainMapping, CNF, HPC, I2MConversion, NDAM, Segmentation, UltraSound3D, Bureaucrats, external, internal, Administrators
2,152 edits
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=OneraM6 Wing =
[[File:Onera m6.png|500px]]


= Delta Wing  (Scitech 2018) =
Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> )
This case comes from the LaRC Turbulent Modeling Resource. For more see  https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html
 
{{Reflist}}
 
[[Internal:CDT3D_OneraM6_adaptation_2020]]
 
= Hemisphere Cylinder =
[[ File:Hemicyl.png ‎ |500px]]
 
'''Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) ''' This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/hc3dnumericspart2_val.html
 
{{Reflist}}
 
[[Internal:CDT3D_Hemicyl_2020]]
 
= Delta Wing =


[[File:Delta_wing_50k_parallel_scitech.png | 500px]]
[[File:Delta_wing_50k_parallel_scitech.png | 500px]]
'''Description (source Scitech 2018) '''  A delta wing constructed of planar facets. A multiscale metric is constructed
based on the Mach field of this subsonic laminar flow.
[[Internal:CDT3D_2019_strong_scaling_delta_wing |  Strong scaling Data (2019)]]
[[Internal:CDT3D_Scitech2019_scalable_complexity| Scalable complexity data (Scitech Journal 2019)]]


[[Internal:ACDT3D_Scitech2018_strong_scaling |  Strong scaling Data (Scitech 2018)]]
[[Internal:ACDT3D_Scitech2018_strong_scaling |  Strong scaling Data (Scitech 2018)]]


[[Internal:ACDT3D_Scitech2018_scalable_complexity| scalable complexity data (Scitech 2018)]]
[[Internal:ACDT3D_Scitech2018_scalable_complexity| Scalable complexity data (Scitech 2018)]]
 
= Cube (polar-2 metric)  =
[[File:Cube_qcircle1.png|300px]]


[[Internal:CDT3D_Scitech2019_scalable_complexity| scalable complexity data (Scitech Journal 2019)]]
'''Description (scitech 2018): '''  A cube with an analytically defined metric field M referred to as polar-2 in the first UGAWG benchmark [https://www.sciencedirect.com/science/article/pii/S1877705817343618].


[[Internal:CDT3D_2019_strong_scaling_delta_wing | Strong scaling Data (2019)]]
[[Internal:CDT3D_Strong_Scaling_cube_case| Strong Scaling Data (2019)]]


= Cube (polar-2 metric)  (Scitech 2018) =
[[File:Cube_qcircle1.png|300px]]


[[Internal:ACDT3D_(Scitech2018)_Strong_Scaling_(Cube_case)| Strong Scaling Data]]
[[Internal:ACDT3D_(Scitech2018)_Strong_Scaling_(Cube_case)| Strong Scaling Data (Scitech 2018)]]


= Spherical Blast =
= Spherical Blast =
[[Image:Blast_banner.png | 500px]]
[[Image:Blast_banner.png | 500px]]
'''Description :''' The metric corresponds to the numerical solution (at one time step) of a spherical blast problem [https://www.sciencedirect.com/science/article/pii/S0010448516301142].
[[Internal:CDT3D 2019 Spherical Blast | Strong Scaling Spherical Blast (2019)]]


= Supersonic missile =
= Supersonic missile =
[[File:Ss missile.png|500px]]
[[File:Ss missile.png|500px]]


[[Internal:ss_missile_comparison_AFLR | Comparison with AFLR ]]
[[Internal:ss_missile_comparison_AFLR | Comparison with AFLR (2018) ]]

Latest revision as of 16:49, 17 February 2020

OneraM6 Wing

Description ([1] ) This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html

Template:Reflist

Internal:CDT3D_OneraM6_adaptation_2020

Hemisphere Cylinder

Description ([2] ) This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/hc3dnumericspart2_val.html

Template:Reflist

Internal:CDT3D_Hemicyl_2020

Delta Wing

Description (source Scitech 2018) A delta wing constructed of planar facets. A multiscale metric is constructed based on the Mach field of this subsonic laminar flow.

Strong scaling Data (2019)

Scalable complexity data (Scitech Journal 2019)

Strong scaling Data (Scitech 2018)

Scalable complexity data (Scitech 2018)

Cube (polar-2 metric)

Description (scitech 2018): A cube with an analytically defined metric field M referred to as polar-2 in the first UGAWG benchmark [1].

Strong Scaling Data (2019)


Strong Scaling Data (Scitech 2018)

Spherical Blast

Description : The metric corresponds to the numerical solution (at one time step) of a spherical blast problem [2].

Strong Scaling Spherical Blast (2019)

Supersonic missile

Comparison with AFLR (2018)

  1. ↑ M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103
  2. ↑ M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103
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