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.
Quantification of airfoil geometry-induced aerodynamic uncertainties— comparison of approaches.SIAM/ASA Journal on Uncertainty Quan- tification, 5(1):334–352, 2017
1 Pith paper cite this work. Polarity classification is still indexing.
1
Pith paper citing it
fields
physics.flu-dyn 1years
2026 1verdicts
UNVERDICTED 1representative citing papers
citing papers explorer
-
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.