pith:F6VZU2KV
A fast Physics-Informed Neural Networks based approach to the 2D design of turbine blades
A progressive PINN framework screens turbine blade families at CFD-comparable accuracy across many conditions with one workflow.
arxiv:2605.07131 v2 · 2026-05-08 · physics.flu-dyn
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Claims
To the best of our knowledge, this is the first study to deploy a single PINN workflow for large-scale, engineering-grade screening of turbomachinery blade families across multiple operating conditions, covering ten NACA6 variants and 30 subsonic operating points. The proposed framework achieves CFD-comparable accuracy for pressure and velocity fields while reducing the computational cost required for family-wide blade screening.
That gradually relaxing boundary conditions from tunnel flow to full outlet static pressure, combined with a geometry-aware dynamic loss-weighting scheme, will ensure reliable convergence and accuracy for complex blade geometries and off-design flows where standard PINNs often struggle.
A progressive Euler-PINN with geometry-aware dynamic loss weighting delivers CFD-comparable pressure and velocity fields for ten NACA6 blade variants across thirty subsonic points at lower computational cost than traditional methods.
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| First computed | 2026-05-25T02:01:22.557276Z |
|---|---|
| Builder | pith-number-builder-2026-05-17-v1 |
| Signature | Pith Ed25519
(pith-v1-2026-05) · public key |
| Schema | pith-number/v1.0 |
Canonical hash
2fab9a6955ed997f45fd68d5cb65ef8d9117af03c815ddc03ab2a6b9e7c6ece1
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curl -sH 'Accept: application/ld+json' https://pith.science/pith/F6VZU2KV5WMX6RP5NDK4WZPPRW \
| jq -c '.canonical_record' \
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# expect: 2fab9a6955ed997f45fd68d5cb65ef8d9117af03c815ddc03ab2a6b9e7c6ece1
Canonical record JSON
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