BWhat changed
Generated roughly30thousand wing-geometry/inflow RANS simulations with surface and volume fields and evaluated learned surrogates for held-out geometry/condition lift-drag tradeoffs.
Scientific scope
Generated roughly30thousand wing-geometry/inflow RANS simulations with surface and volume fields and evaluated learned surrogates for held-out geometry/condition lift-drag tradeoffs. Inherits OpenFOAM RANS, Transolver and AB-UPT. Simulated high-fidelity labels are not direct numerical resolution of all turbulence or wind-tunnel truth. Specific NACA-profile parameter ranges and held-out splits do not imply arbitrary aircraft generalization or certified optimal design.
Evidence
The linked original sources describe the stated contribution and its evidence limits. WRS has not independently rerun the experiments or certified a proof. Inherits OpenFOAM RANS, Transolver and AB-UPT. Simulated high-fidelity labels are not direct numerical resolution of all turbulence or wind-tunnel truth. Specific NACA-profile parameter ranges and held-out splits do not imply arbitrary aircraft generalization or certified optimal design.
Contributors
- Source-listed authors and technical contributors · SCIENCE: Source-listed authors or explicitly credited technical contributors for the cited versions. Family entries retain source-specific attribution; a combined list is not one original-paper byline or equal individual work. Names alone do not establish resolved identities.
- Going with the Speed of Sound: Pushing Neural Surrogates into Highly-turbulent Transonic Regimes
- Mistral research publications index
Provisional WRS assessment, edition 2026-10-16.1. Independent expert calibration is pending. This grade does not certify correctness or assign ownership.
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