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SHIFT-Wing

Benchmarks

Task NameDataset NameSOTA ResultTrend
Aerodynamic SimulationSHIFT-Wing full-resolution (test)
Relative L2 Error (Surface)0.0559
7
Aerodynamic SimulationSHIFT-Wing full-resolution
Relative L2 Error (Surface)0.0559
7
Aerodynamic flow field predictionSHIFT-WING Ma = 0.85 (test)
Static Pressure (ps)1.88
4
Aerodynamic flow field predictionSHIFT-WING (Ma = 0.5) geometries (test)
Static Pressure Coefficient (ps)0.468
4
Aerodynamic Coefficient PredictionSHIFT-WING (test)
Drag Coefficient (Ma=0.5)1
4
Showing 5 of 5 rows