A progressive Euler-PINN with geometry-aware loss weighting achieves CFD-comparable pressure and velocity fields for ten NACA6 blades across 30 operating points while cutting computational cost for family-wide screening.
Physics-informed neural network compression mechanism for airfoil flow field prediction.Physics of Fluids, 37(3), 2025
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A fast Physics-Informed Neural Networks based approach to the 2D design of turbine blades
A progressive Euler-PINN with geometry-aware loss weighting achieves CFD-comparable pressure and velocity fields for ten NACA6 blades across 30 operating points while cutting computational cost for family-wide screening.