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Aerodynamic Field Prediction on SuperWing (test)

0.028Rel L2 Error

GeoTransolver

-0.0038680.2112410.426350.641459May 7, 2026
Updated 27d ago

Evaluation Results

MethodLinks
2026.05
0.0280.01460.00960.00440.02770.01260.45
2026.05
0.03090.02250.00970.00550.03060.01750.45
2026.05
0.03240.01820.01110.00550.03210.01570.35
2026.05
0.03580.02690.01120.00660.03540.0210.35
2026.05
0.05290.03740.00760.00370.05390.02590.45
2026.05
0.05480.03020.01860.0090.05430.02610.32
2026.05
0.06060.04590.00870.00460.06120.03160.35
2026.05
0.06440.04730.020.01160.0630.03650.32
2026.05
0.10840.07680.01560.00770.10970.05310.32
2026.05
0.14290.08630.04970.02630.1420.07490.27
2026.05
0.19460.1580.05980.03830.18840.12060.27
2026.05
0.2240.1410.07840.04310.22270.12240.57
2026.05
0.29120.22670.04160.02250.28990.15460.27
2026.05
0.32650.26790.10170.06610.320.20760.57
2026.05
0.35870.23760.12690.07350.35880.20750.45
2026.05
0.38580.27730.1360.08590.3850.24180.35
2026.05
0.45330.35780.14270.08950.45020.28220.45
2026.05
0.48580.41350.15120.10260.47630.32290.35
2026.05
0.49090.39840.06970.03930.48350.27090.57
2026.05
0.6990.61320.09690.05870.6660.40130.45
2026.05
0.82470.73520.11490.0710.79430.48560.35