Internal:Adaptive CDT3D Results

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Hemisphere Cylinder

Description ([1] )

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