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Initial public release
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NASA 2DZP — 2D Zero-Pressure-Gradient Flat Plate

Validation case from the NASA TMR Collaborative Testing Challenge 2022 (turb-prs2022).

Required metrics

  1. Cf vs. x — skin-friction along plate
  2. u⁺ vs. log₁₀(y⁺) at x = 0.97 — boundary-layer profile compared with theory

Folder layout

NASA_2DZP/
├── baseline_komegasst/   k-ω SST RANS integral profiles (.dat + .csv)
├── highfidelity/         Theory + experimental references (.dat + .csv)
└── plots/                Pre-rendered comparison figures + plot_profiles.py

The full OpenFOAM case (mesh, fields, run scripts, extraction code) is hosted separately on the heavy CFD-asset Hugging Face dataset linked in the paper.

Solver / setup

  • Solver: rhoSimpleFoam (compressible steady)
  • Turbulence model: kOmegaSST (baseline, no augmentation)
  • Grid: 545 × 385, finest of NASA TMR sequence
  • Re_L: 5×10⁶ (L = 2)
  • Inflow: M = 0.2

Submission format

Provide two files (CSV or Tecplot .dat) matching the columns of the bundled baseline:

  • 2DZP_cf.csv — columns: zone, x, Cf
  • 2DZP_u+y+.csv — columns: zone, log(y+), u+

Then python plots/plot_profiles.py overlays the baseline + reference + your model.