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Compressible Airfoil Flow Modeling on NACA2412 (test)
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3.92
Relative L1 Error (Test)
TNO/HTNO (Best of ours)
3.6636
5.3943
7.125
8.8557
Jun 8, 2026
Relative L1 Error (Test)
Updated 1mo ago
Evaluation Results
Method
Method
Links
Relative L1 Error (Test)
TNO/HTNO (Best of ours)
2026.06
3.92
HOGNN
2026.06
10.33
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