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Mach number field prediction on Airfoil NACA-0012 (test)

59.6Error (%)

eDAFNO

42.156159.903277.65395.397Apr 30, 2023
Updated 4d ago

Evaluation Results

MethodLinks
2023.04
59.6
2023.04
64.2
2023.04
65.9
2023.04
79.4
2023.04
165
2023.04
372.5
2023.04
495.7