Airfoil
Benchmarks
| Task Name | Dataset Name | SOTA Result | Trend | |
|---|---|---|---|---|
| Forward PDE solving | Airfoil | Relative L20.46 | 21 | |
| Regression | Airfoil UCIrvine (5-fold cross-validation) | 1-RAE0.2201 | 16 | |
| Operator Learning | Airfoil (Structured Mesh) (test) | Relative L2 Error0.0051 | 15 | |
| PDE Solving | Airfoil Structured Mesh (test) | Relative L2 Error0.0052 | 15 | |
| Regression | Airfoil | RMSE2.717 | 14 | |
| Regression | Airfoil UCIrvine | 1-RAE0.463 | 9 | |
| Regression | Airfoil 5-fold CV | RMSE1.54 | 7 | |
| Regression | Airfoil (3 train-test splits) | LPPD-0.176 | 7 | |
| Mach number field prediction | Airfoil NACA-0012 (test) | Error (%)59.6 | 7 | |
| Mach number field prediction | Airfoil NACA-0012 (train) | Error (%)32.9 | 7 | |
| Regression | Airfoil (test) | NLL0.0837 | 6 | |
| Meta-regression | Airfoil (test) | RMSE0.0936 | 4 | |
| Regression | Airfoil | MSE- | 0 | |
| Initial Value Problem | Airfoil (test) | Metric- | 0 |
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