NASA 2DZP — 2D Zero-Pressure-Gradient Flat Plate
Validation case from the NASA TMR Collaborative Testing Challenge 2022 (turb-prs2022).
Required metrics
- Cf vs. x — skin-friction along plate
- 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,Cf2DZP_u+y+.csv— columns:zone,log(y+),u+
Then python plots/plot_profiles.py overlays the baseline + reference + your model.