HiLiftAeroML: A High-Fidelity Computational Fluid Dynamics Dataset for High-Lift Aircraft Aerodynamics
Ashton et al.
What it does
1,800 wall-modelled LES runs of 180 variants of the NASA Common Research Model high-lift configuration, at ten angles of attack from 4° to 22°, on 300–500 million-cell grids, released under CC BY 4.0.
Why it matters
The first open high-fidelity dataset for high-lift aerodynamics. Its GeoTransolver and Transolver baselines reconstruct fields well but struggle with separated flow at high angle of attack and with regime shifts.