| --- |
| license: cc-by-4.0 |
| pretty_name: Blade3DNO Structured CFD WebDataset |
| size_categories: |
| - 1K<n<10K |
| tags: |
| - webdataset |
| - cfd |
| - scientific-machine-learning |
| - neural-operator |
| - turbomachinery |
| configs: |
| - config_name: default |
| data_files: |
| - split: train |
| path: train.tar |
| - split: validation |
| path: val.tar |
| - split: test |
| path: test.tar |
| --- |
| |
| # Blade3DNO Structured CFD WebDataset |
|
|
| This repository provides an ML-ready WebDataset release associated with |
| **Blade3DNO**, a geometry-consistent spectral operator learning framework for |
| three-dimensional transonic compressor flows. |
|
|
| The data contain reconstructed structured tensors derived from steady RANS |
| solutions of multi-circular-arc compressor blade configurations under different |
| operating conditions. Each sample combines geometry, operating-condition |
| features, grid metrics, and three-dimensional flow fields on a logical grid of |
| `256 × 64 × 32`. |
|
|
| The paper associated with this release is: |
|
|
| > Liangrui Wei, Yuxin Zhao, Zhou Du, Quanyong Xu, and Feng Zhou. |
| > [Blade3DNO: Geometry-consistent spectral operator learning for transonic 3D |
| > compressor flows](https://doi.org/10.1016/j.ast.2026.112334). |
| > *Aerospace Science and Technology*, 177:112334, 2026. |
|
|
| ## Dataset summary |
|
|
| The public release contains 1,828 samples: |
|
|
| | Split | Archive | Samples | Design-ID manifest | |
| |---|---:|---:|---| |
| | Train | `train.tar` | 1,279 | `train_design_ids.txt` | |
| | Validation | `val.tar` | 274 | `val_design_ids.txt` | |
| | Test | `test.tar` | 275 | `test_design_ids.txt` | |
| | **Total** | | **1,828** | | |
|
|
| The split manifests define membership in each split. Archive member names such |
| as `000795.npz` are packaging keys rather than design identifiers. Always use |
| the `design_id` stored inside each NPZ sample, or join against |
| `coefficients.csv`. |
|
|
| > **Release note:** the article reports 1,827 samples in its experiment |
| > snapshot, whereas this public package contains 1,828 samples. The archives |
| > and manifests above are authoritative for this release. |
|
|
| ## Repository contents |
|
|
| ```text |
| . |
| ├── train.tar |
| ├── val.tar |
| ├── test.tar |
| ├── coefficients.csv |
| ├── train_design_ids.txt |
| ├── val_design_ids.txt |
| └── test_design_ids.txt |
| ``` |
|
|
| - The three TAR files are WebDataset archives. |
| - Every TAR member is a compressed NumPy archive with an `.npz` extension. |
| - `coefficients.csv` contains one `design_id` column and 30 raw scalar |
| operating/boundary-condition columns. |
| - The three text files contain one `design_id` per line. |
|
|
| ## Sample schema |
|
|
| Unless noted otherwise, arrays are stored as `float32`. |
|
|
| | Field | Shape / type | Description | |
| |---|---|---| |
| | `design_id` | scalar string | Canonical identifier used by the manifests and `coefficients.csv`. | |
| | `features` | scalar Python object containing a dictionary | Min-max-normalized operating and boundary-condition features. | |
| | `coordinates` | `(256, 64, 32, 3)` | Physical-grid coordinates, with Cartesian coordinates in the last dimension. | |
| | `coordinates_centered` | `(256, 64, 32, 3)` | Centered coordinate representation used during preprocessing. | |
| | `density` | `(256, 64, 32)` | Density field. | |
| | `velocity` | `(256, 64, 32)` | Velocity-magnitude field. | |
| | `mach` | `(256, 64, 32)` | Mach-number field. | |
| | `temperature` | `(256, 64, 32)` | Temperature field. | |
| | `pressure` | `(256, 64, 32)` | Pressure field. | |
| | `density_std` | `(256, 64, 32)` | Precomputed normalized density field; the `_std` suffix is retained for compatibility. | |
| | `mach_std` | `(256, 64, 32)` | Precomputed normalized Mach-number field; the `_std` suffix is retained for compatibility. | |
| | `temperature_std` | `(256, 64, 32)` | Precomputed normalized temperature field; the `_std` suffix is retained for compatibility. | |
| | `pressure_std` | `(256, 64, 32)` | Precomputed normalized pressure field; the `_std` suffix is retained for compatibility. | |
| | `sdf` | `(256, 64, 32)` | Signed-distance-function geometry representation. | |
| | `normals_x`, `normals_y`, `normals_z` | `(256, 64, 32)` each | Cartesian components of the stored geometry-normal representation. | |
| | `wall_mask` | `(256, 64, 32)` | Binary wall-region mask stored as `float32`. | |
| | `metrics_dxi_dx`, `metrics_dxi_dy`, `metrics_dxi_dz` | `(256, 64, 32)` each | Stored derivatives of the logical coordinate `xi`. | |
| | `metrics_deta_dx`, `metrics_deta_dy`, `metrics_deta_dz` | `(256, 64, 32)` each | Stored derivatives of the logical coordinate `eta`. | |
| | `metrics_dzeta_dx`, `metrics_dzeta_dy`, `metrics_dzeta_dz` | `(256, 64, 32)` each | Stored derivatives of the logical coordinate `zeta`. | |
|
|
| The directory name used during preprocessing contains `256_32_32`, but the |
| serialized arrays have the verified shape `256 × 64 × 32`. Downstream code |
| should use the array shapes stored in the NPZ files. |
|
|
| ### Scalar coefficients |
|
|
| The `features` dictionary contains normalized forms of the following 30 columns |
| from `coefficients.csv`: |
|
|
| ```text |
| inlet_static_pressure |
| inlet_static_temperature |
| inlet_velocity_x |
| inlet_velocity_y |
| inlet_velocity_z |
| inlet_velocity_magnitude |
| inlet_mach_number |
| inlet_total_pressure |
| inlet_total_temperature |
| inlet_dynamic_pressure |
| inlet_density |
| inlet_mass_flow_rate |
| outlet_static_pressure |
| outlet_static_temperature |
| outlet_velocity_x |
| outlet_velocity_y |
| outlet_velocity_z |
| outlet_velocity_magnitude |
| outlet_mach_number |
| outlet_total_pressure |
| outlet_total_temperature |
| outlet_dynamic_pressure |
| outlet_density |
| outlet_mass_flow_rate |
| inlet_total_pressure_p01 |
| inlet_static_pressure_p1 |
| inlet_temperature_t1 |
| velocity_y |
| velocity_z |
| outlet_static_pressure_p2 |
| ``` |
|
|
| Use `coefficients.csv` when the original, non-normalized scalar values are |
| required. |
|
|
| ## Loading the WebDataset |
|
|
| Install the two lightweight reader dependencies: |
|
|
| ```bash |
| pip install numpy webdataset |
| ``` |
|
|
| The public archives can then be streamed directly: |
|
|
| ```python |
| import io |
| |
| import numpy as np |
| import webdataset as wds |
| |
| url = ( |
| "https://huggingface.co/datasets/lrwei/bladenet/" |
| "resolve/main/train.tar" |
| ) |
| |
| dataset = wds.WebDataset(url, shardshuffle=False) |
| sample = next(iter(dataset)) |
| |
| with np.load(io.BytesIO(sample["npz"]), allow_pickle=True) as data: |
| design_id = str(data["design_id"].item()) |
| coordinates = data["coordinates"] # (256, 64, 32, 3) |
| sdf = data["sdf"] # (256, 64, 32) |
| pressure = data["pressure"] # (256, 64, 32) |
| temperature = data["temperature"] # (256, 64, 32) |
| density = data["density"] # (256, 64, 32) |
| mach = data["mach"] # (256, 64, 32) |
| features = data["features"].item() # dict[str, np.float32] |
| |
| print(design_id) |
| print(features) |
| ``` |
|
|
| `allow_pickle=True` is required because the scalar `features` field stores a |
| Python dictionary. Enable it only for dataset artifacts obtained from a trusted |
| source. |
|
|
| To read another split, replace `train.tar` with `val.tar` or `test.tar`. |
| Because the archives are large, streaming or copying them to fast local storage |
| is recommended. |
|
|
| ## Data generation and processing |
|
|
| The Blade3DNO study constructs a parametric multi-circular-arc compressor-blade |
| design space and samples geometry and operating conditions before running |
| steady RANS simulations. Solver-native multi-block flow fields are then mapped |
| to globally continuous structured tensors suitable for convolutional models |
| and neural operators. |
|
|
| The packaged representation includes: |
|
|
| - blade geometry encoded by coordinates, SDF values, and normal components; |
| - operating and boundary conditions encoded by scalar features; |
| - raw and normalized flow variables; |
| - wall masks and logical-to-physical grid metric components. |
|
|
| Refer to the paper for the CFD setup, geometric parameterization, filtering |
| criteria, reconstruction method, and model experiments. |
|
|
| ## Intended uses |
|
|
| This release is intended for research on: |
|
|
| - three-dimensional compressor-flow surrogate modeling; |
| - neural operators and structured-grid learning; |
| - geometry-aware scientific machine learning; |
| - full-field prediction of pressure, temperature, density, and Mach number; |
| - comparisons with 3D CNN and point-cloud baselines. |
|
|
| The data are numerical RANS results rather than experimental measurements. |
| Models trained on this release should be validated independently before use in |
| safety-critical or production engineering workflows. |
|
|
| ## Limitations |
|
|
| - This is a processed, grid-aligned ML representation rather than the original |
| solver-native multi-block archive. |
| - Interpolation and reconstruction may smooth or alter local flow features. |
| - The release contains one large TAR archive per split, so random access is less |
| efficient than with many smaller shards. |
| - Exact reproduction of paper results also depends on the preprocessing, |
| training code, random seeds, and experiment configuration used in the study. |
|
|
| ## Citation |
|
|
| If you use this dataset, please cite the Blade3DNO paper: |
|
|
| ```bibtex |
| @article{wei2026blade3dno, |
| title = {Blade3DNO: Geometry-consistent spectral operator learning for |
| transonic 3D compressor flows}, |
| author = {Wei, Liangrui and Zhao, Yuxin and Du, Zhou and |
| Xu, Quanyong and Zhou, Feng}, |
| journal = {Aerospace Science and Technology}, |
| volume = {177}, |
| pages = {112334}, |
| year = {2026}, |
| doi = {10.1016/j.ast.2026.112334}, |
| url = {https://doi.org/10.1016/j.ast.2026.112334} |
| } |
| ``` |
|
|
| When referring specifically to this packaged release, also include the |
| repository URL: |
| `https://huggingface.co/datasets/lrwei/bladenet`. |
|
|
| ## License |
|
|
| This dataset is released under the |
| [Creative Commons Attribution 4.0 International license |
| (CC BY 4.0)](https://creativecommons.org/licenses/by/4.0/). |
| Redistribution and adaptation are permitted with appropriate attribution. |
|
|