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Correcting a CFD-trained wing surrogate with wind-tunnel pressure paint

Paper title A Data Fusion Framework for Grounding Aerospace Surrogate Model via Experimental Wind-Tunnel Observations

Kulkarni et al. (Luminary) · Aero & CFD

Paper arXiv 2609.04267PDF

A GeoTransolver surrogate trained on 2,300 CFD runs of the NASA Common Research Model wing-body is frozen; a small correction head on its per-cell latents is trained on wind-tunnel pressure-sensitive paint, registered onto the CFD surface, to learn the gap between CFD and the measurements.

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