SHIFT-Wing
Adapted-mesh simulations of parametric NASA CRM wing-body variants for transonic aerodynamics
Data
luminary-shift/
Simulations of thousands of parametric variants of the NASA Common Research Model, with the wing re-lofted from six spanwise sections and the fuselage tube varied in diameter and length, across a range of flow conditions, with surface and volume fields.
- Licence
- CC BY-NC 4.0
- Access
- Gated on Hugging Face: access is granted on request
- Cases
- Thousands of parametric NASA CRM wing-body variants, each with its own flow condition (one parameterization, OnShape Luminary DPW4)
- Solver
- Luminary Cloud, with Luminary Mesh Adaptation
- Mesh
- Adapted, a default sequence of 13 meshes from about 250,000 to 30 million cells
- Fields
- Surface pressure and wall shear stress; volume pressure, velocity, eddy viscosity, density and temperature; forces and moments; geometry and flow parameters
- Size
- 10.2 TB
Used by
- Paper · TransformersTransolver without attention — Does Transolver really need a Transformer?
- Paper · PretrainingGeometry meets physics — Data-efficient pre-training for unstructured neural PDE solvers
- Paper · TransformersSMART — Mesh-free aerodynamic surrogates from raw geometry
- Paper · TransformersGeoTransolver — Transolver that keeps the geometry in every layer
- Paper · Latent modelsD-JEPA — One geometry latent, reused across flow conditions and physics
- News · ReleaseLuminary attaches calibrated 90% error bars to trained large physics models with a 166,000-parameter companion network
- News · ReleaseLuminary reports an out-of-distribution confidence score on SHIFT-Wing: 0.99 in distribution, 0.13 for an SUV
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