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Benchmarks
Compressible Airfoil Flow Modeling on NACA0012 (test)
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3.77
Relative L1 Error
TNO/HTNO (Best of ours)
3.5464
5.0557
6.565
8.0743
Jun 8, 2026
Relative L1 Error
Updated 1mo ago
Evaluation Results
Method
Method
Links
Relative L1 Error
TNO/HTNO (Best of ours)
2026.06
3.77
HOGNN
2026.06
9.36
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