Wedge Duct Multi-Resolution Adaptive CFD Dataset
Supersonic/hypersonic inviscid flow over a wedge in a duct, solved with Ansys Fluent on a sequence of anisotropically adapted meshes. Each sample is one set of inflow conditions drawn from a 1750-point sampling plan. For every sample, the dataset provides the volume solution, the derived fields that drive the adaptation (gradients, Hessians, shock flags, size field) and the boundary-surface solution, for each of four adaptation cycles.
Contents
| Samples | 228 (metadata/samples.parquet) |
| Cycles per sample | 4 (cycle0 … cycle3) |
| Mesh | 3D slab, one layer of wedge (prism) cells through the thickness (z) |
Layout
metadata/
samples.parquet one row per sample: inflow conditions
cycles.parquet one row per (sample, cycle): mesh size and file paths
fields.json field names, original solver names, units, descriptions
reflag_summary.parquet shock-flag recomputation statistics
lambda_values.parquet Hessian eigenvalue percentile statistics
geometry/ Parasolid model, Simmetrix model and starter mesh
data/NNNN/cycleK/
volume.vtu flow solution on the cycle-K mesh
supp.vtu adaptation fields on the same mesh
surface.vtm boundary surfaces (multiblock), blocks in surface/<name>.vtu
All .vtu files are VTK XML unstructured grids (binary, zlib), readable with ParaView, VTK,
pyvista or meshio. Fields are point data.
Samples (metadata/samples.parquet)
| column | units | description |
|---|---|---|
| sample_id | four-digit ID, matches data/NNNN/ |
|
| original_id | ID in the original 1750-point sampling plan | |
| T0 | K | total temperature |
| P0 | Pa | total pressure |
| Ts | K | static temperature |
| Ps | Pa | static pressure |
| M | freestream Mach number | |
| altitude_km | km | altitude used for the static conditions |
Adaptation cycles
cycleK holds the solution on the mesh after K adaptations; cycle0 is the starter mesh. Minimum mesh size in adaptation cycle N is
h_min = 0.00651125 / (4 · 2^(N-1)), maximum size h_max = 0.05209448, and maximum requested
aspect ratio 32. The adaptation is driven by the static temperature Hessian, modified at
shocks flagged from the temperature and pressure fields.
Fields
volume.vtu and surface/<block>.vtu: Static_Pressure, Mach_Number, Velocity_Magnitude,
Sound_Speed, Static_Temperature, Density, Dynamic_Pressure, Enthalpy,
Specific_Heat_Ratio__gamma_, Gas_Constant__R_, Velocity (3).
supp.vtu: temperature_gradient (3), temperature_hessian (9), temperature_flag_direction,
temperature_seeds, temperature_flag, pressure_gradient (3), pressure_hessian (9),
pressure_flag_direction, pressure_seeds, pressure_flag, size_field (6).
size_field is the size field prescribed for the next adaptation, stored as two orthogonal
3-component vectors (components 0–2 and 3–5). Each vector gives a direction, and its magnitude is
the requested mesh size in that direction. The cases are 2D, so the third (through-thickness)
direction does not apply and is omitted.
Surface blocks: top, outlet, bottom, wedge, bottom-2, inlet, front, back.
Loading
import meshio, pandas as pd
from huggingface_hub import snapshot_download
root = snapshot_download("sahni-lab/multi-res-wedge-duct-cfd-database", repo_type="dataset",
allow_patterns=["metadata/*", "data/0000/*"])
samples = pd.read_parquet(f"{root}/metadata/samples.parquet")
vol = meshio.read(f"{root}/data/0000/cycle0/volume.vtu")
print(vol.point_data["Mach_Number"].shape)
Citation
A paper describing this dataset is forthcoming at AIAA SciTech 2027. The citation will be added here once it is published.
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