Airfoil pressure coefficient prediction on Airfoil (test)
0.0095RMSEFluidFlow
Evaluation results
| Method | Links | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| FluidFlowArchitecture=DiT2026.03 | 0.0095 | 0.0001 | 0.0025 | 3.4372 | 0.0076 | 0.0325 | 0.9998 | 0.0131 | — | |
| FluidFlowArchitecture=U-Net2026.03 | 0.0096 | 0.0001 | 0.0024 | 4.4881 | 0.0076 | 0.0318 | 0.9998 | 0.0133 | — | |
| GNNSource=this work2026.06 | 0.029 | 8.4 | 0.0065 | — | 0.0204 | 0.1195 | 0.9965 | — | 0.1142 | |
| MLPSource=this work2026.06 | 0.0311 | 9.7 | 0.0085 | — | 0.0305 | 0.1359 | 0.996 | — | 0.1158 | |
| MLPSource=DLR [21]2026.06 | 0.0335 | — | 0.0068 | — | 0.0225 | 0.1164 | 0.9954 | — | — | |
| KANSource=this work2026.06 | 0.0346 | 1.2 | 0.0137 | — | 0.0566 | 0.1667 | 0.9951 | — | 0.1457 | |
| Vanilla MLPArchitecture=Multilayer Perceptron2026.03 | 0.036 | 0.0013 | 0.0176 | 16.8522 | 0.0572 | 0.1418 | 0.9973 | 0.0491 | — | |
| GNNSource=DLR [21]2026.06 | 0.2876 | — | 0.0061 | — | 0.0202 | 0.1176 | 0.9966 | — | — |