Conceptual

Parametric Neural-Network Surrogate Solver for Laminar Airfoil Flows

A physics-informed solver that computes all laminar flows around airfoils at once by combining the Time-Stepping-Oriented Neural Network reformulation with a body-fitted mesh transformation. Trains a single label-free surrogate model spanning a high-dimensional space of airfoil shapes, Reynolds numbers, and angles of attack, overcoming the ill-conditioning that limits standard physics-informed neural networks on viscous flows.