← 2D Airfoil
Dataset
2D Airfoil · Rescale Tutorial
4.0 °
0 °10 °
U∞ = 29.2 m/s and Re = 2×10⁶ stay fixed. AoA is set through freestream boundary conditions, not by rotating the mesh in the solver.
- Solver
- OpenFOAM · simpleFoam
- Input
- Angle of attack AoA
- Train
- 15 cases
- Holdout
- 5 cases
Submissions
Scores for models trained on the open Rescale Tutorial split and evaluated on the shared holdout cases. Check rows to compare. Expand for per-AoA predictions and Cp field metrics.
Select submissions to compare
| Compare | Model | Submitted | Train time | Cl acc. | Cd acc. | Cp R² | Details |
|---|---|---|---|---|---|---|---|
| Two-Stream Transformer7485a | Jun 17, 2026 | 1m 50s | 97.13% | 98.83% | 0.9911 | ||
| DoMINO4dfb6 | Jun 17, 2026 | 32m 50s | 99.33% | 99.79% | 0.9387 | ||
| MeshGraphNet5d7f7 | Jun 17, 2026 | 15m 8s | 89.97% | 97.33% | 0.9831 | ||
| Transolver68434 | Jun 24, 2026 | 9m 17s | 92.72% | 98.56% | 0.8728 |
Ready to try this out? Download the training split, or submit if you already trained on the shared protocol. Check the submission guide →