An SDF-embedded RANS-PINN predicts turbulent flow fields for unseen NACA 4-digit airfoil geometries and Reynolds numbers with a few percent normalized error.
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Geometry-aware PINNs for Turbulent Flow Prediction
An SDF-embedded RANS-PINN predicts turbulent flow fields for unseen NACA 4-digit airfoil geometries and Reynolds numbers with a few percent normalized error.