Internal:Adaptive CDT3D Results: Difference between revisions
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[[File:Onera m6.png|500px]] | [[File:Onera m6.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> ) | 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 | |||
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[[Internal:CDT3D_OneraM6_adaptation_2020]] | |||
= Hemisphere Cylinder = | = Hemisphere Cylinder = | ||
[[ File:Hemicyl.png |500px]] | [[ 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 | '''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 | ||
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[[Internal:CDT3D_Hemicyl_2020]] | [[Internal:CDT3D_Hemicyl_2020]] | ||
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
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
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.
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 (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
- ↑ 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
- ↑ 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